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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Мониторинг СМИ

Мониторинг СМИ и социальных сетей. Сканирование интернета, новостных сайтов, специализированных контентных площадок на базе мессенджеров. Гибкие настройки фильтров и первоначальных источников.

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Поддерживает ввод нескольких поисковых фраз (по одной на строку). При поиске обеспечивает поддержку морфологии русского и английского языка
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Применить Всего найдено 571. Отображено 100.
31-01-2013 дата публикации

Rotary internal combustion engine with phasing gear

Номер: US20130028774A1
Принадлежит: Pratt and Whitney Canada Corp

In one aspect, described is a rotor of a rotary internal combustion engine, including a phasing gear with an annular meshing section including a plurality of radially inwardly oriented teeth and an annular attachment section connected to the meshing section and coaxial therewith, the attachment section being offset axially inwardly from the teeth and having at least a portion thereof located radially inwardly of the teeth, and a fastener apparatus connecting the phasing gear to the rotor body, the fastener apparatus engaging the rotor body radially inwardly of the teeth.

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31-01-2013 дата публикации

Apex and face seals with rotary internal combustion engine

Номер: US20130028776A1
Принадлежит: Pratt and Whitney Canada Corp

In one aspect, described is a rotor for a rotary internal combustion engine where a first face seal biased axially outwardly away from the first end face has opposed curled ends abutting a first seal element of a respective one of the adjacent apex seal assemblies, and a second face seal biased axially outwardly away from the second end face has opposed curled ends abutting a second seal element of a respective one of the adjacent apex seal assemblies.

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18-07-2013 дата публикации

Seal for the rotor of rotary piston machines

Номер: US20130183186A1
Принадлежит: EN3 GmbH

The parting line or groove between the piston halves of the rotor of a rotary piston engine are sealed by means of fools which conform to the configuration of a peripheral portion of the rotor and cover the parting line or joint.

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07-01-2021 дата публикации

ROTARY ENGINE

Номер: US20210003011A1
Принадлежит:

Disclosed herein is a rotary engine a supply flow passage provided in the housing to allow the lubricating oil to move therethrough, a sealing part arranged to contact the rotor to selectively close the supply flow passage, and an elastic part configured to press the sealing part toward the combustion chamber. 1. A rotary engine , comprising:a housing having a chamber in which a fuel is provided and a supply flow passage through which a lubricating oil supplied to the chamber flows;a rotor provided in the chamber and configured to be rotated to compress the provided fuel; andan oil supplier provided in the housing to supply the lubricating oil to the supply flow passage, a plug configured to contact a portion of the rotor to selectively close the supply flow passage; and', 'an elastic member configured to press the plug toward the chamber., 'wherein the oil supplier includes2. The rotary engine of claim 1 , wherein the housing comprises:a rotor housing having a side surface configured to be in contact with at least one surface of the rotor, the side surface defining an inner side surface of the chamber;a first housing coupled to the rotor housing and defining a first side of the chamber; anda second housing coupled to the rotor housing and defining a second side of the chamber, the second side being opposite to the first side, wherein the supply flow passage is provided in at least one of the first housing or the second housing.3. The rotary engine of claim 2 , wherein the supply flow passage comprises:a flow passage provided in at least one of the first housing or the second housing through which lubricating oil is provided; andan inflow hole formed through the at least one of the first housing or the second housing and communicating with the transport flow passage,wherein the plug is inserted in the inflow hole such that, when the rotor contacts the plug, the plug is moved to open the inflow hole.4. The rotary engine of claim 3 , wherein:the supply flow passage ...

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09-01-2020 дата публикации

METHODS AND SYSTEMS FOR SEALING ROTATING EQUIPMENT SUCH AS EXPANDERS OR COMPRESSORS

Номер: US20200011426A1
Автор: Juchymenko Victor
Принадлежит:

A method and system is provided for pressure balancing one or more seals in machines such as expanders and/or compressors using the process fluid which is being expanded or compressed to provide the pressure for pressure balancing the other side of the one or more seals. The one or more seals may be part of a pressure containing chamber which may comprise a seal, a bearing and/or a gear on a rotating shaft common to the seal. An amount of pressure to be supplied to housing(s) for a machine so as to create a pressure cascade, and thereby dropping the pressure in each subsequent chamber as pressure approaches atmosphere. Pressure differentials may be directed to leak process fluid to the chamber into the process. Pressurized lube oil systems may be employed for balancing pressure and delivering lubricant to the seals, bearings and gears. 1. A system for distributing pressure across seals , comprising:a machine, configured to handle process fluid, the machine comprising a higher pressure process pipe and a lower pressure process pipe;a first pressure chamber, operatively coupled to one portion of the machine, wherein the first pressure chamber is configured to be pressurized by the process fluid, the first pressure chamber comprising one or more first chamber seals; anda second pressure chamber, operatively coupled to another portion of the machine, wherein the second pressure chamber is configured to be pressurized by the process fluid, the second pressure chamber comprising one or more second chamber seals;wherein the machine is configured to direct process fluid, via the one or more of the first chamber seals and second chamber seals,wherein at least one of the first chambers and/or second chambers is connected via a pressure balancing line to a point in the machine that is at a lower pressure than the pressure at the seal.2. The system of claim 1 , wherein the pressure balancing line is operative to assist in directing the process fluid from the first pressure ...

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06-02-2020 дата публикации

ROTARY ENGINE CASING

Номер: US20200040813A1
Принадлежит:

A rotary engine casing having at least one end wall of an internal cavity for a rotor including a seal-engaging plate sealingly engaging the peripheral wall to partially seal the internal cavity and a member mounted adjacent the seal-engaging plate outside of the internal cavity. The member and seal-engaging plate having abutting mating surfaces which cooperate to define between them at least one fluid cavity communicating with a source of liquid coolant. When the casing includes a plurality of rotor housings, the end wall may be between rotor housings. A method of manufacturing a rotary engine casing is also discussed. 1. A method of manufacturing a rotary engine casing , the method comprising:manufacturing two end-casing sections including a first part of a fluid path for circulating a cooling fluid;manufacturing a central-casing section defining at least one internal cavity for receiving a rotor and a second part of the fluid path; manufacturing a member having a first mating surface,', 'manufacturing a seal-engaging plate having a second mating surface, and', 'machining at least one surface depression on at least one of the first and second mating surfaces, the at least one surface depression in fluid communication with the fluid path; and, 'wherein at least one of the manufacturing of the two end-casing sections and of the manufacturing of the central-casing section includesassembling the central-casing section between the two end-casing sections, including connecting the first and second parts of the fluid path, and assembling the member with the seal-engaging plate by abutting the first and second mating surfaces such that the at least one surface depression defines a fluid cavity in communication with the fluid path for circulating a cooling fluid therein.2. The method as defined in claim 1 , wherein machining the at least one surface depression on at least one of the first and second mating surfaces includes machining complementary depressions on the first ...

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15-03-2018 дата публикации

Prime Mover Assemblies and Methods

Номер: US20180073364A1
Принадлежит: Regi US Inc USA

Prime movers are provided that can include: a pair of cylindrical members about a center rod, a fixed member about the center rod between the pair of cylindrical members; wherein the pair of cylindrical members rotate with the center rod in relation to the fixed member; a housing extending between the cylindrical members; and a plurality of chambers between the opposing bases of the cylindrical members and the fixed member. Methods for rotating members in relation to a fixed member are also provided. The methods can include rotating a pair of cylindrical members in relation to a fixed member about a center rod along a shared axis within a housing extending between the pair of cylindrical members.

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12-03-2020 дата публикации

ROTARY DEVICE

Номер: US20200080421A1
Принадлежит:

A rotor can comprise a body having arcuate voids each presenting away from a rotation axis and, for each void, a vane. The vane is mounted to the body for pivotal movement between retracted and extended positions; is adapted to sweep the void in the manner in which a piston sweeps a cylinder during movement between the positions; and terminates in a tip. A stator defines the rotation axis; and has an annular surface which, in use, is swept by the tips during rotation of the body. The surface is positioned such that, in each rotation, each vane cycles between its extended and retracted positions. A sealing arrangement defines a pair of ports and, in combination with the rotor and stator, defines, in use, chambers that increase in volume when in communication with one of the ports and that decrease in volume when in communication with the other of the ports. 1. Apparatus comprising: a body having defined therein a plurality of arcuate voids each presenting away from the rotation axis; and', 'for each of the voids of the plurality, a vane, the vane: being pivotally mounted to the body for movement between a retracted position and an extended position; being adapted to sweep the void in the manner in which a piston sweeps a cylinder during movement between the retracted and extended positions; and terminating in a tip;, 'a rotor which, in use, rotates about a rotation axis, the rotor havinga stator: defining the rotation axis; and having an annular surface which, in use, is swept by the tips of the vanes during rotation of the body, the annular surface being positioned such that, in each rotation, each vane makes a cycle between the extended position and the retracted position thereof;a sealing arrangement defining a pair of ports and adapted, in combination with the rotor and the stator, to define, in use, chambers that increase in volume when in communication with one of the pair of ports and that decrease in volume when in communication with the other of the pair of ...

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30-03-2017 дата публикации

HYBRID PNEUMATIC / INTERNAL COMBUSTION ROTARY ENGINE

Номер: US20170089201A1
Автор: Farazifard Rasoul
Принадлежит:

A hybrid engine comprises a housing and at least one rotor. The engine employs tongue and groove system to generate rotational movement. As the rotor pivots, reciprocating tongues slide into and out of the grooves. In pneumatic mode, introduction of compressed air forwardly into the grooves drives the rotor. Meanwhile, the air exhaust is cleared from the grooves rearwardly. In internal combustion mode, compression and air intake strokes start and end at the same time in a groove. Combustion and exhaust strokes occur simultaneously in the next groove arriving at the combustion chamber. 1. A rotary engine able to produce mechanical energy from internal combustion and from pneumatic , steam and pressurized fluid flow , comprising:a housing having an internal cylindrical contour wall, including at least one side plate connected to the housing;at least one rotor positioned in and movable in the housing, having an axis of rotation, and having at least one pressure groove cut in said rotor;at least one central shaft coaxial with the housing axis, connecting to the rotor and extending out of the housing, supported by at least one bearing in at least one of the side plates, and rotating with the rotor;at least one slot cut through the housing contour wall, accepting a tongue reciprocating in sealing relationship to and within said slot;at least one intake passage in the housing; andat least one exhaust passage in the housing.2. A rotary engine as defined in claim 1 , wherein when used as pneumatic claim 1 , steam and pressurized fluid engine claim 1 , wherein the intake passages are located in the front of the slots and the exhaust passages are located at the rear of the slots.3. A rotary engine as described in claim 1 , wherein when used as internal combustion engine claim 1 , further comprising:at least one combustion chamber cut into the internal housing contour wall;at least one compression slot located at the front of each of the combustion chamber, accepting a ...

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27-04-2017 дата публикации

SEALING SLEEVE FOR GEARED SHAFT OF GEARMOTOR ASSEMBLY

Номер: US20170114640A1
Принадлежит: NIDEC MOTOR CORPORATION

A motor includes a shaft rotatable about an axis, an engaged component engaged by the shaft, a sleeve fixed to the shaft to rotate therewith, and a seal at least partly circumscribing the shaft. The shaft includes an engagement region presenting a substantially variable outer shaft surface that at least in part engages the engaged component. The sleeve includes a first section that at least partly circumscribes and engages the engagement region of the shaft. The first section of the sleeve presents an outer seal-engaging surface and an outer bearing-engaging surface. The seal and the bearing each at least partly circumscribe the engagement region of the shaft and the first section of the sleeve to engage the seal-engaging surface and the bearing-engaging surfaces, respectively, of the sleeve. 1. A motor comprising:a shaft rotatable about an axis;an engaged component engaged by the shaft;a sleeve fixed to the shaft to rotate therewith; anda seal at least partly circumscribing the shaft,said shaft including an engagement region presenting a substantially variable outer shaft surface that at least in part engages the engaged component,said sleeve including a first section that at least partly circumscribes and engages the engagement region of the shaft,said first section of the sleeve presenting an outer seal-engaging surface,said seal at least partly circumscribing the engagement region of the shaft and the first section of the sleeve to sealingly engage the seal-engaging surface of the sleeve.2. The motor of claim 1 ,said variable outer shaft surface comprising a plurality of teeth.3. The motor of claim 2 ,said engaged component comprising a gear,said shaft rotatably engaging said gear.4. The motor of claim 1 ,said shaft including a second region adjacent the engagement region,said sleeve including a second section that at least partly circumscribes the second region.5. The motor of claim 4 ,said second region of the shaft and said engagement region of the shaft ...

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18-06-2015 дата публикации

APEX AND FACE SEALS WITH ROTARY INTERNAL COMBUSTION ENGINE

Номер: US20150167465A1
Принадлежит:

A rotor for a rotary internal combustion engine with a first face seal biased axially outwardly away from the first end face has opposed curled ends abutting a first end seal of a respective one of the adjacent apex portions, and a second face seal biased axially outwardly away from the second end face has opposed curled ends abutting a second end seal of a respective one of the adjacent apex portions. A rotary internal combustion engine and a method of sealing chambers of a Wankel engine are also discussed. 1. A rotor for a rotary internal combustion engine comprising:a body having first and second axially spaced apart end faces, and a peripheral face extending between the end faces and defining at least three circumferentially spaced apex portions, the first and second end faces each having a groove defined therein between each of the apex portions and each adjacent one of the apex portions, the grooves of the first and second end faces being disposed adjacent to and radially inwardly of the peripheral surface of the rotor; an apex seal protruding radially from the peripheral face of the body and being biased radially away therefrom, and', 'first and second end seals received in a corresponding recess defined in the first and second end face, respectively, the first end seal protruding axially from the first end face and being biased axially outwardly away therefrom, and the second end seal protruding axially from the second end face and being biased axially outwardly away therefrom, the apex seal being engaged with the first and second end seals;, 'at each of the apex portionsa first face seal located in each groove of the first end face and extending between adjacent ones of the apex portions, each first face seal being biased axially outwardly away from the first end face, each first face seal having opposed curled ends each abutting the first end seal of a respective one of the adjacent apex portions; anda second face seal located in each groove of the second ...

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14-06-2018 дата публикации

HYDRAULIC DEVICE COMPRISING A SEALING ELEMENT

Номер: US20180163542A1
Автор: Baur Dominik, Meinig Uwe
Принадлежит:

A hydraulic device for an internal combustion engine or a gearing system, the hydraulic device including a housing featuring a chamber wall structure which delineates a pressure chamber for a pressurised hydraulic fluid; an actuating member which can be adjusted in the housing relative to the chamber wall structure in an actuating direction and in an actuating counter direction opposite to the actuating direction in order to adjust the delivery volume or phase position; and a sealing element including a sealing structure and a spring structure which is supported or moulded on one of the chamber wall structure and the actuating member, preferably the actuating member, and presses the sealing structure into sealing contact with the other of the chamber wall structure and the actuating member with a spring force in order to seal off the pressure chamber. The sealing structure and the spring structure are moulded in one piece. 1. A hydraulic device for an internal combustion engine or a gearing system , the hydraulic device comprising:(a) a housing featuring a chamber wall structure which delineates a pressure chamber for a pressurised hydraulic fluid;(b) an actuating member which can be adjusted in the housing relative to the chamber wall structure in an actuating direction and in an actuating counter direction which is opposite to the actuating direction in order to adjust the delivery volume or phase position;(c) and a sealing element comprising a sealing structure and a spring structure which is supported or moulded on one of the chamber wall structure and the actuating member and presses the sealing structure into a sealing contact with the other of the chamber wall structure and the actuating member with a spring force in order to seal off the pressure chamber;(d) wherein the sealing structure and the spring structure are moulded in one piece.2. The hydraulic device according to claim 1 , wherein the sealing structure is a sealing strip which extends in the ...

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06-06-2019 дата публикации

SEALING DEVICE

Номер: US20190169988A1
Принадлежит:

An oil seal member is provided at an outside surface of a member performing whirling motion such as a rotary engine rotor. A sliding face of the oil seal member that slides relatively to a stationary-side member is provided with a step extending circumferentially, and has a relatively high surface formed on one radial side with respect to the step and a relatively low surface on the other radial side. The high surface is provided with pumping grooves to pump oil tending to leak from the high surface side into the low surface side, into the high surface side by sliding relatively to the stationary-side member. 1. A sealing device that seals a gap between an outside surface of a member performing whirling motion such as a rotary engine rotor and a stationary-side member , the device comprising:an oil seal member provided at the outside surface of the member performing whirling motion,the oil seal member having a sliding face that slides relatively to the stationary-side member, the sliding face being provided with a step extending circumferentially, and having a relatively high surface formed on one radial side with respect to the step and a relatively low surface on the other radial side, the high surface being provided with pumping grooves to pump oil tending to leak from the high surface side into the low surface side, into the high surface side by sliding relatively to the stationary-side member.2. The sealing device according to claim 1 , wherein the step is provided circumferentially continuously.3. The sealing device according to claim 1 , wherein the step is provided circumferentially intermittently claim 1 , and a portion not provided with the step is provided with a dam formed by the high surface protruding to the low surface side.4. The sealing device according to claim 3 , wherein the dam is provided at an angle from the low surface side to the high surface side so that the high surface side is located downstream.5. The sealing device according to claim 1 ...

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27-06-2019 дата публикации

ROTARY PISTON AND CYLINDER DEVICE

Номер: US20190195071A1
Принадлежит:

A rotary piston and cylinder device () comprising a rotor (), a stator () and a rotatable shutter (), the rotor comprising a piston () which extends from the rotor into a working chamber, the rotor and the stator together defining a working chamber, the shutter arranged to extend through the working chamber and forming a partition therein, and the shutter comprising a slot which allows passage of the piston therethrough, a bearing () which mounts the rotor relative to the stator, the rotor comprising a formation () which extends substantially axially away from the chamber, and the formation being radially outward of the bearing and extending around the axis of rotation, and the formation comprising a surface which at least in part defines a space between the rotor and the stator, and at least part of that space and/or the formation overlaps in an axial direction with the bearing. 1. A rotary piston and cylinder device comprising a rotor , a stator and a rotatable shutter ,the rotor including a piston which extends from the rotor into a working chamber, the rotor and the stator together defining a working chamber,the shutter arranged to extend through the working chamber and forming a partition therein, and the shutter including a slot which allows passage of the piston therethrough,a bearing which mounts the rotor relative to the stator,the rotor including a formation which extends substantially axially away from the chamber, and the formation being radially outward of the bearing and extending around the axis of rotation, and the formation including a surface which at least in part defines a space between the rotor and the stator, and at least part of that space and/or the formation overlaps in an axial direction with the bearing.2. The device as claimed in in which the formation comprises an annular or cylindrical formation.3. The device as claimed in in which the annular or cylindrical formation is provided rearwardly of the chamber.4. The device as claimed in in ...

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25-06-2020 дата публикации

ROTARY ENGINE WITH HOUSING HAVING SILICON CARBIDE PLATE

Номер: US20200200009A1
Принадлежит:

A rotary internal combustion engine has: a rotor; a housing circumscribing a rotor cavity, the rotor received within the rotor cavity, the housing having a peripheral wall and a side housing assembly secured to the peripheral wall, the side housing assembly having plates located at spaced apart ends of the peripheral wall, the plates defining seal running surfaces in sealing engagement with opposed end faces of the rotor, the plates made of silicon carbide. 1. A rotary internal combustion engine comprising: a rotor; a housing circumscribing a rotor cavity , the rotor received within the rotor cavity , the housing having a peripheral wall and a side housing assembly secured to the peripheral wall , the side housing assembly having plates located at spaced apart ends of the peripheral wall , the plates defining seal running surfaces in sealing engagement with opposed end faces of the rotor , the plates made of silicon carbide.2. The rotary internal combustion engine of claim 1 , wherein the side housing assembly includes two end walls secured at opposed ends of the peripheral wall claim 1 , the plates located on inner sides of the end walls claim 1 , peripheries of the plates sandwiched between the end walls and the peripheral wall.3. The rotary internal combustion engine of claim 2 , wherein the end walls define recesses at the inner sides thereof claim 2 , the plates received within the recesses.4. The rotary internal combustion engine of claim 3 , wherein the end walls define abutment surfaces at the recesses and oriented toward the plates claim 3 , the plates spaced apart from the abutment surfaces.5. The rotary internal combustion engine of claim 2 , wherein the end walls are made of a material different than that of the plates.6. The rotary internal combustion engine of claim 2 , wherein the side housing assembly defines pockets between the end walls and the plates claim 2 , the pockets configured for circulating a liquid coolant.7. The rotary internal ...

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19-08-2021 дата публикации

SCROLL TYPE EXPANDER

Номер: US20210254466A1
Автор: Nakamura Shinji
Принадлежит:

A housing of a scroll type expansion machine includes: a suction port formed at a position on the opposite side to a drive shaft with a fixed scroll interposed therebetween; a discharge port formed on the side of a drive-side bearing closer to the tip end of the drive shaft; a low pressure chamber formed on the outer side of an orbiting-side scroll portion when viewed from the axial direction of the drive shaft; and a tip end-side low-pressure space being a space in which a sealing member is disposed, and has: a partition wall partitioning the tip end-side low-pressure space and the low-pressure chamber from each other; and a communication space communicating the tip end-side low-pressure space with the low-pressure chamber. 1. A scroll type expander used in a Rankine cycle in which a working fluid circulates , comprising:a housing;a drive shaft a base end of which is housed in the housing and a tip end of which projects out of the housing;a fixed scroll fixed to a side closer to the base end of the drive shaft rather than to the tip end of the drive shaft inside the housing;an orbiting scroll arranged on a side of the fixed scroll closer to the tip end of the drive shaft in a rotatable structure inside the housing;a bearing arranged on a side of the orbiting scroll closer to the tip end of the drive shaft inside the housing and configured to support the drive shaft in a rotatable structure with respect to the housing via a plurality of rolling elements; anda sealing member arranged on a side of the bearing closer to the tip end of the drive shaft inside the housing and configured to surround an outer peripheral surface of the drive shaft, whereinthe fixed scroll has a fixed-side scroll portion formed in a spiral shape when viewed from an axial direction of the drive shaft,the orbiting scroll has an orbiting-side scroll portion formed in a spiral shape when viewed from the axial direction of the drive shaft and meshing with the fixed-side scroll portion,the housing ...

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04-12-2014 дата публикации

EXPANDER

Номер: US20140356208A1
Автор: TSUBOI Noboru

In order to suppress the damage and the degradation in durability of a bearing of an expander, simplify the configuration of the expander, and reduce the manufacturing cost thereof, an expander of the present invention includes an expander rotor that is rotationally driven by an expanding force transmitted from vapor of a working medium introduced into an expansion chamber and a first bearing that supports a first rotation shaft of the expander rotor to a vapor inlet, a casing includes therein first bearing chambers that have a pressure lower than that of the vapor inlet and accommodate the first bearing, and a passage that leads lubricant to a low-pressure portion having a pressure lower than that of the first bearing chamber is connected to a position above the lowermost portion of the first bearing in the first bearing chamber. 1. An expander , comprising:a casing that includes therein an expansion chamber into which lubricant and vapor of a working medium are introduced;an expander rotor that is rotationally driven by an expanding force transmitted from the vapor of the working medium introduced into the expansion chamber;a first bearing that supports a rotation shaft of the expander rotor to a working medium feeding port of the expansion chamber so that the expander rotor is rotatable;a second bearing that supports the rotation shaft of the expander rotor to a working medium lead-out port of the expansion chamber so that the expander rotor is rotatable;a first bearing chamber that is provided inside the casing and accommodates the first bearing, the pressure inside the first bearing chamber being lower than that of the feeding port of the expansion chamber; anda lubricant passage that connects a position above a lowermost portion of the first bearing in the first bearing chamber to a low-pressure portion having a pressure lower than that of the first bearing chamber.2. The expander according to claim 1 , whereina shaft seal that seals the outer periphery of the ...

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15-10-2020 дата публикации

APEX SEAL ARRANGEMENT FOR ROTARY INTERNAL COMBUSTION ENGINE

Номер: US20200325777A1
Принадлежит:

A rotor assembly for a rotary internal combustion engine is provided. The rotor assembly includes a rotor having a radial groove defined radially in a peripheral surface of the rotor. The groove has a depth and an intermediate shoulder at an intermediate depth. The groove has a first width therealong that is narrower than an intermediate width at the shoulder. An apex seal is received in the groove and protrudes from the peripheral face of the rotor. The apex seal is configured to move radially between a first position and a second position outward of the first position. A biasing member biases the apex seal toward the second position. A platform is disposed in the groove between the apex seal and the biasing member and has a width greater than the first width. 1. A rotor assembly for a rotary internal combustion engine , the rotor assembly comprising:a rotor having a radial groove defined radially in a peripheral surface of the rotor, the groove having a depth and an intermediate shoulder at an intermediate depth, the groove having a first width therealong that is narrower than an intermediate width at the shoulder; andan apex seal received in the groove and protruding from the peripheral face of the rotor, the apex seal configured to move radially between a first position and a second position outward of the first position, a biasing member biasing the apex seal toward the second position, and a platform disposed in the groove between the apex seal and the biasing member, the platform having a width greater than the first width.2. The rotor assembly as defined in claim 1 , wherein the platform has a first and a second surface defined on opposed sides thereof claim 1 , the first surface interfacing with the biasing member and the second surface interfacing with an underside surface of the apex seal.3. The rotor assembly as defined in claim 2 , wherein the second surface of the platform and the underside surface of the apex seal have a corresponding relief.4. The ...

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06-12-2018 дата публикации

ROTARY ENGINE CASING

Номер: US20180347457A1
Принадлежит:

A rotary engine casing having at least one end wall of an internal cavity for a rotor including a seal-engaging plate sealingly engaging the peripheral wall to partially seal the internal cavity and a member mounted adjacent the seal-engaging plate outside of the internal cavity. The member and seal-engaging plate having abutting mating surfaces which cooperate to define between them at least one fluid cavity communicating with a source of liquid coolant. When the casing includes a plurality of rotor housings, the end wall may be between rotor housings. A method of manufacturing a rotary engine casing is also discussed. 1. A method of manufacturing a rotary engine casing , the method comprising:manufacturing two end-casing sections including a first part of a fluid path for circulating a cooling fluid;manufacturing a central-casing section defining at least one internal cavity for receiving a rotor and a second part of the fluid path; manufacturing a member having a first mating surface,', 'manufacturing a seal-engaging plate having a second mating surface, and', 'machining at least one surface depression on at least one of the first and second mating surfaces, the at least one surface depression in fluid communication with the fluid path; and, 'wherein at least one of the manufacturing of the two end-casing sections and of the manufacturing of the central-casing section includesassembling the central-casing section between the two end-casing sections, including connecting the first and second parts of the fluid path, and assembling the member with the seal-engaging plate by abutting the first and second mating surfaces such that the at least one surface depression defines a fluid cavity in communication with the fluid path for circulating a cooling fluid therein.2. The method as defined in claim 1 , wherein machining the at least one surface depression on at least one of the first and second mating surfaces includes machining complementary depressions on the first ...

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27-12-2018 дата публикации

CONTINUOUSLY VARIABLE TURBINE

Номер: US20180371910A1
Принадлежит:

A continuously variable turbine includes a case assembly with a case body defining a chamber, a rotor assembly positioned in the chamber, and a pair of valve assemblies. The rotor assembly includes a ring piston and a rotor body positioned within the ring piston. The rotor body is connected to a shaft, and the rotor body rotates concentrically about an axis extending through the shaft while the ring piston rotates eccentrically about the axis. Each valve assembly is positioned outside of the ring piston relative to the rotor assembly and includes a valve body and a seal component attached to the valve body. Each seal component has a surface with a curvature that matches the outer curvature of the ring piston to form a continuous surface seal between the seal component and the ring piston as the ring piston rotates eccentrically about the axis. The position of the continuous surface seals in the chamber defining a first sub-chamber and a second sub-chamber between the surface seals. The case body includes an intake port and an exhaust port for each sub-chamber. 1. A continuously variable turbine comprising:a case assembly with a case body defining a chamber;a rotor assembly positioned in the chamber and including a ring piston and a rotor body positioned within the ring piston, the rotor body being connected to a shaft, the rotor body rotating concentrically about an axis extending through the shaft while the ring piston rotates eccentrically about the axis; anda pair of valve assemblies, each valve assembly being positioned outside of the ring piston relative to the rotor assembly, each valve assembly including a valve body and a seal component attached to the valve body, each seal component having a surface with a curvature that matches the outer curvature of the ring piston to form a continuous surface seal between the seal component and the ring piston as the ring piston rotates eccentrically about the axis, the position of the continuous surface seals in the ...

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27-08-2013 дата публикации

Роторно-поршневая машина объемного расширения "турбомотор" (варианты)

Номер: RU2012101836A

1. Роторно-поршневая машина объемного расширения «ТурбоМотор» включающая:а) корпус, имеющий круговую рабочую полость и впускные и выпускные каналы;б) по меньшей мере два рабочих вала, которые соосны круговой поверхности рабочей полости и оснащены с одной стороны лопастными поршнями и с другой стороны рычагами;в) по меньшей мере одно центральное неподвижное зубчатое колесо, которое соосно поверхности рабочей полости и рабочим валам;г) соосный рабочим валам выходной вал имеет эксцентрик, на котором установлены водило и планетарное зубчатое колесо, при этомд) планетарное зубчатое колесо находится в зацеплении с центральным неподвижным зубчатым колесом с внутренним зубчатым зацеплением с передаточным отношением i=n/(n+1) (где n=1, 2, 3, 4, 5… - ряд целых чисел),ж) водило шарнирно соединено шатунами с рычагами обоих рабочих валов, аз) количество лопастных поршней, установленных на каждом рабочем валу, равно n+1,отличающаяся тем, чтои) круговая рабочая полость корпуса (1) имеет впускные (18) и выпускные (19) каналы и/или выходные (27) и входные (28) каналы объема(ов) перетока, вынесенного(ных) за пределы рабочей полости,к) при этом эти каналы (18 и 19, 27 и 28) имеют последовательно смежно-расположенное подключение к круговой рабочей полости корпуса (1) по ходу движения лопастных поршней (5 и 6),л) причем как впускные (18) и выпускные (19) каналы, так и выходные (27) и входные (28) каналы расположены по обе стороны относительно мест смыкания граней лопастных поршней (5 и 6),м) а сами грани лопастных поршней (5 и 6) имеют угловую ширину, достаточную для одновременного перекрытия выходного (27) и входного (28) каналов.2. Роторно-поршневая машина по п.1, отличающаяся т РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (51) МПК F01C 1/07 (11) (13) 2012 101 836 A (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ЗАЯВКА НА ИЗОБРЕТЕНИЕ (21)(22) Заявка: 2012101836/06, 06.11.2009 (71) Заявитель(и): Драчко Евгений Федорович (UA) Приоритет(ы): (30) Конвенционный приоритет: (72) Автор(ы ...

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03-01-2017 дата публикации

Rotary piston machine, especially rotary engine

Номер: US9534594B2
Принадлежит: AVL List GmbH

A rotary piston machine is disclosed. In one aspect, the machine includes a piston chamber that is defined in a housing by a first sidewall, a second sidewall and a peripheral wall interconnecting these sidewalls and a rotary piston that is rotatably arranged in the piston chamber and has a first face and a second face. The first face of the rotary piston faces an interior of the first sidewall of the piston chamber and the second face of the rotary piston faces an interior of the second sidewall of the piston chamber. at least one ventilation bore is provided in the first and/or the second sidewall of the piston chamber and connected to at least one ventilation channel, wherein the at least one ventilation bore is arranged at a location that radially lies within at least one first lateral seal.

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19-03-1963 дата публикации

Gas seal for rotary mechanisms

Номер: US3081745A
Автор: Roy T Hurley
Принадлежит: Curtiss Wright Corp

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14-03-1967 дата публикации

Seal construction for rotary combustion engine

Номер: US3309011A
Принадлежит: Toyo Kogyo Co Ltd

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28-10-1975 дата публикации

Structure for preventing leakage of lubricating oil in rotary-piston internal combustion engines

Номер: US3915599A
Автор: Kazuhiro Kawamura
Принадлежит: Toyota Motor Corp

Disclosed herein is a structure for preventing leakage of lubricating oil in rotary-piston internal combustion engines. The structure comprises passages formed in the side walls of a rotor to allow a rotary shaft to rotatably extend therethrough, each passage having a counter-tapered opening, which diverges toward a combustion chamber. Oil seal rings are interposed between the rotary shaft and the passages.

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29-03-2017 дата публикации

Rotary piston machine, especially rotary engine

Номер: EP2643553B1
Принадлежит: AVL List GmbH

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11-09-1974 дата публикации

Rotary piston internal combustion engine

Номер: GB1366214A
Автор:
Принадлежит: Nissan Motor Co Ltd

1366214 Rotary I C engines NISSAN MOTOR CO Ltd 30 Oct 1972 [13 Nov 1971] 49950/72 Heading F1F A rotary piston internal combustion engine of the trochoidal type comprises apertures 12a, 24 in facing surfaces of the housing end wall 12 and rotor wall 26, an annular plate 60 fixed to eccentric 34 and having grooves 64, 72 which receive seals 66, 74 engaging the peripheries of apertures 12a, 24, and a gas source 80 for supplying pressurized gas via flow control valve 82, inlet 84 and passage 86 into the space 70 between plate 60 and the end wall, thus maintaining the seal 74 urged against the axially inner side wall of groove 72 in all conditions of the engine. This sealing prevents coolant from leaking out of rotor cavity 22. Blow-by gases from the opposite side of the rotor pass through passages 78, 76 in the eccentric 34 and plate 60 to space 70 to assist the pressurized gas in its sealing function. However, upon braking of the engine, the blow-by gas pressure would not be sufficient, and the pressurized gas source 80 is particularly needed in this situation.

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10-09-2014 дата публикации

Rotary piston machine of volumetric expansion

Номер: RU2528221C2

FIELD: machine building. SUBSTANCE: invention relates to the rotary piston machine comprising a housing, two working shafts, central fixed toothed gear wheel and output shaft with an eccentric. The working shafts are fitted with vane pistons and levers. The eccentric has a spider with a planetary pinion engaged with the central sprocket with internal gearing with a reduction ratio i=n/(n+1) (where n=1, 2, 3, 4, 5… - series of integers). The spider has an articulated connection of connecting rods with levers of both working shafts. The amount of vane pistons on each working shaft is equal to n+1. The circumferential working cavity of the housing (1) has inlet (18) and outlet (19) bores, and also output (27) and input (28) bores of cross-flow volumes, provisioned outside the working cavity. The passages (18 and 19, 27 and 28) have series adjoining connection to a circumferential working cavity of the housing (1) towards the motion of vane pistons (5 and 6). Both inlet (18) and outlet (19) bores, and output (27) and input (28) passages are located from both sides with reference to the places of contacts of fractures of edges of vane pistons (5 and 6). Edges of vane pistons (5 and 6) have angular width, sufficient for simultaneous overlapping of output (27) and input (28) passages. EFFECT: increased cost effectiveness and reliability of machinery operation. 10 cl, 45 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 528 221 C2 (51) МПК F01C 1/07 (2006.01) F01C 1/077 (2006.01) F02G 1/044 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ (21)(22) Заявка: ИЗОБРЕТЕНИЯ К ПАТЕНТУ 2012101836/06, 06.11.2009 (24) Дата начала отсчета срока действия патента: 06.11.2009 (72) Автор(ы): Драчко Евгений Федорович (UA) (73) Патентообладатель(и): Драчко Евгений Федорович (UA) Приоритет(ы): (30) Конвенционный приоритет: (43) Дата публикации заявки: 27.08.2013 Бюл. № 24 R U 20.07.2009 UA A200907575 (45) Опубликовано: 10.09.2014 Бюл. № 25 2146009 C1, 27.02.2000. US ...

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21-05-2018 дата публикации

Sixty-rock rotary-pulse internal combustion engine

Номер: RU2654555C1

FIELD: motors and pumps. SUBSTANCE: invention relates to engine construction, namely to rotary-blade internal combustion engine (ICE), which can be used for water, air and land transport. Essence of invention lies in the fact that six-stroke rotary-blade internal combustion engine contains stator rigidly fixed to shaft by cylindrical rotor with longitudinal grooves in which blades are placed, side walls, front and rear bearing shields. In this case, side walls of all working chambers of engine are formed by parts rigidly and hermetically fastened to stator, and in grooves made at rotor ends, there are composite prismatic parts, springs pressed by ends to adjacent blades, and lateral side to side walls of working chambers. EFFECT: technical result is reduction of fuel-air mixture leaks outside working space, as well as inter-chamber leaks. 1 cl, 5 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 654 555 C1 (51) МПК F02B 53/02 (2006.01) F01C 1/356 (2006.01) F01C 19/10 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК F02B 53/02 (2018.02); F01C 1/356 (2018.02); F01C 19/10 (2018.02) (21)(22) Заявка: 2017124969, 13.07.2017 (24) Дата начала отсчета срока действия патента: (73) Патентообладатель(и): Кривко Николай Михайлович (RU) Дата регистрации: 21.05.2018 (56) Список документов, цитированных в отчете о поиске: RU 2416032 C1, 10.04.2011. RU 2397327 C2, 20.08.2010. RU 2426898 C2, 20.08.2011. US 4168941 A, 25.09.1979. US 2011165007 A1, 07.07.2011. RU 2386823 C1, 20.04.2010. (45) Опубликовано: 21.05.2018 Бюл. № 15 R U (54) ШЕСТИТАКТНЫЙ РОТОРНО-ЛОПАСТНОЙ ДВИГАТЕЛЬ ВНУТРЕННЕГО СГОРАНИЯ (57) Реферат: Изобретение относится к области ротор с продольными пазами, в которых двигателестроения, а именно к роторноразмещены лопатки, боковые стенки, передний лопастному двигателю внутреннего сгорания и задний подшипниковые щиты. При этом (ДВС), который может быть использован на боковые стенки всех рабочих камер двигателя водном, ...

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16-02-2016 дата публикации

Power generator

Номер: JP5860435B2
Автор: 昇 壷井
Принадлежит: Kobe Steel Ltd

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10-10-2012 дата публикации

Engine with swing pistons and sealing system

Номер: RU2463457C2
Принадлежит: Арнольд ВАГНЕР

FIELD: engines and pumps. SUBSTANCE: pistons are coupled with rotary swing shaft. Said shaft runs about rotational axis. Pistons swing about swing axis perpendicular to rotational axis. Guide elements are arranged on pistons. Guide elements fit in, at least, one guide groove in housing. Cantilever elements of two pistons are arranged to make four intermediate spaces. Each of said two intermediate spaces makes working chamber while each of the other two intermediate spaces makes forechamber. Engine comprises zones of clearances between its parts that displace relative to each other in piston rotation and swinging. Sealing system incorporates sealing elements made up of seal strips or rings to cover gap zones and comprises sealing element lubricator. Sealing elements are arranged nearby swing piston edges relative to guide elements, adequate guide groove, forechambers and working chambers to cover zone of gaps so that pressure drop in said chambers is ruled out as well as ingress of lubricant therein. EFFECT: production of engine with swing pistons with sealing system. 20 cl, 9 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) 2 463 457 (13) C2 (51) МПК F01C 9/00 (2006.01) F01C 19/02 (2006.01) F01C 19/12 (2006.01) F01C 21/04 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (21)(22) Заявка: 2008137659/06, 19.02.2007 (24) Дата начала отсчета срока действия патента: 19.02.2007 (73) Патентообладатель(и): ВАГНЕР Арнольд (CH) R U Приоритет(ы): (30) Конвенционный приоритет: 22.02.2006 CH 277/06 (72) Автор(ы): ВАГНЕР Арнольд (CH) (43) Дата публикации заявки: 27.03.2010 Бюл. № 9 2 4 6 3 4 5 7 (45) Опубликовано: 10.10.2012 Бюл. № 28 (56) Список документов, цитированных в отчете о поиске: WO 2005/098202 A1, 20.10.2005. RU 2080452 C1, 27.05.1997. RU 2062327 C1, 20.06.1996. RU 2239068 C2, 27.10.2004. WO 84/00997 A1, 15.03.1984. WO 02/33238 A1, 25.04.2002. 2 4 6 3 4 5 7 R U (86) Заявка PCT: CH 2007/000088 (19.02.2007) C 2 C 2 (85) Дата начала ...

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10-02-2006 дата публикации

VARIABLE COMPRESSION ENGINE

Номер: RU2005124929A

ÐÎÑÑÈÉÑÊÀß ÔÅÄÅÐÀÖÈß (19) RU (11) 2005 124 929 (13) A (51) ÌÏÊ F01C 1/20 (2006.01) ÔÅÄÅÐÀËÜÍÀß ÑËÓÆÁÀ ÏÎ ÈÍÒÅËËÅÊÒÓÀËÜÍÎÉ ÑÎÁÑÒÂÅÍÍÎÑÒÈ, ÏÀÒÅÍÒÀÌ È ÒÎÂÀÐÍÛÌ ÇÍÀÊÀÌ (12) ÇÀßÂÊÀ ÍÀ ÈÇÎÁÐÅÒÅÍÈÅ (21), (22) Çà âêà: 2005124929/06, 30.12.2003 (71) Çà âèòåëü(è): Ðåâîëþøí Ýíäæèí Êîðïîðåéøí (CA) (30) Ïðèîðèòåò: 09.01.2003 US 60/438,764 (72) Àâòîð(û): ÊÎÍÍÅÐÇ Äæåéìñ Ì. (CA) (85) Äàòà ïåðåâîäà çà âêè PCT íà íàöèîíàëüíóþ ôàçó: 09.08.2005 (74) Ïàòåíòíûé ïîâåðåííûé: Ïîëèêàðïîâ Àëåêñàíäð Âèêòîðîâè÷ (86) Çà âêà PCT: CA 03/02031 (30.12.2003) Àäðåñ äë ïåðåïèñêè: 191036, Ñàíêò-Ïåòåðáóðã, à/ 24, "ÍÅÂÈÍÏÀÒ", ïàò.ïîâ. À.Â.Ïîëèêàðïîâó R U Ôîðìóëà èçîáðåòåíè 1. Äâèãàòåëü (400) äë èñïîëüçîâàíè ñ íàãðóçêîé, ñîäåðæàùèé êîìïðåññîð (428), âûïîëíåííûé ñ âîçìîæíîñòüþ ïðèåìà ýíåðãèè è, ïîñëå åå ïðèåìà, ïåðèîäè÷åñêîãî îãðàíè÷åíè êàìåðû, çàïîëíåíè êàìåðû îêðóæàþùèì âîçäóõîì è îñóùåñòâëåíè ïðîöåññà ñæàòè , ïðè êîòîðîì ïðîèñõîäèò óìåíüøåíèå îáúåìà êàìåðû äë ñîçäàíè ñæàòîãî âîçäóõà; ðàäèàòîð (414), âûïîëíåííûé ñ âîçìîæíîñòüþ ïðèåìà ñæàòîãî âîçäóõà èç êîìïðåññîðà (428) è îõëàæäåíè ïðèí òîãî ñæàòîãî âîçäóõà; ñðåäñòâî (426) ñæèãàíè , ïðåäíàçíà÷åííîå äë ïðèåìà òîïëèâà è åãî ñæèãàíè â ïðîöåññå ñãîðàíè ñî ñæàòûì âîçäóõîì äë ñîçäàíè ïåðâè÷íûõ ïðîäóêòîâ âûõëîïà; îáúåìíûé ïíåâìàòè÷åñêèé äâèãàòåëü (408), âûïîëíåííûé ñ âîçìîæíîñòüþ ïðèâåäåíè â äåéñòâèå ïåðâè÷íûìè ïðîäóêòàìè âûõëîïà äë ñîçäàíè ýíåðãèè è âòîðè÷íûõ ïðîäóêòîâ âûõëîïà; îáúåìíûé ðàñøèðèòåëü (410) ãàçà, ïðåäíàçíà÷åííûé äë ïðèåìà âòîðè÷íûõ ïðîäóêòîâ âûõëîïà è èõ ïî ñóùåñòâó àäèàáàòè÷åñêîãî ðàñøèðåíè äë ñîçäàíè òðåòè÷íûõ ïðîäóêòîâ âûõëîïà è ýíåðãèè; è ñðåäñòâî (314) ïåðåäà÷è ýíåðãèè, ïðåäíàçíà÷åííîå äë íàïðàâëåíè ýíåðãèè, ñîçäàâàåìîé ïðè ðàáîòå ïíåâìàòè÷åñêèì äâèãàòåëåì (408) è ðàñøèðèòåëåì (410) ãàçà, äë ïðèâåäåíè â äåéñòâèå êîìïðåññîðà (428) è íàãðóçêè; ïðè÷åì ñðåäñòâî (426) ñæèãàíè âûïîëíåíî ñ âîçìîæíîñòüþ ïðèåìà ïåðåìåííûõ îáúåìîâ òîïëèâà äë òîãî, ÷òîáû ïðè ðàáîòå ïîáóäèòü ñðåäñòâî (314) ïåðåäà÷è ýíåðãèè ïåðåìåííûìè îáúåìàìè ýíåðãèè ïðèâîäèòü â ...

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15-12-1978 дата публикации

Rotary-piston positive-displacement engine

Номер: SU638276A3
Принадлежит: Ванкель Гмбх (Фирма)

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28-03-1983 дата публикации

SEAL FOR USE BETWEEN THREE RELATED MOVING BODIES, PRELIMINARY TO ROTATING STAMP MACHINES

Номер: DK145881B
Автор: P B Kathmann
Принадлежит: Rotary Motor Co Ag Rmc

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19-06-1998 дата публикации

INTERNAL COMBUSTION ENGINE WITH ROTARY PISTON.

Номер: FR2657919B1
Автор: Eiermann Dankwart
Принадлежит: Wankel GmbH

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21-12-1973 дата публикации

Seals for a rotary motor - comprising a cover or coating of soft and opt self lubricating material on the rotor

Номер: FR2183836A1
Автор: [UNK]
Принадлежит: Nissan Motor Co Ltd

Method comprises providing a seal between a rotor and the walls confining and beside the peaks of the rotor profile by using a relatively soft layer on at least the leading edges and sides of the rotor peaks, pref. the whole external surface of the rotor. Pref. the cover is of aluminium or Ni aluminide (contg. 4.5% Al); Pb; Sn; Cu; or a heat resistant plastic, esp. polyamide, polyimide, phenolic, silicone rubber, or PTFE. Pref. seal layer incorporates a solid lubricant, pref. carbon fibres, graphite or powdered polyimide. Pref. layer also incorporates a combustion catalyst, pref. Pt of Cu oxide to convert combustion products to non toxic residues. Partic suitable for multilobal rotors turning in a flat diepitrochoid chamber such as a Wankel (RTM) engine. Reduces gas losses and mech. play between the rotor and the side walls, improves motor power and smoothness at low rpm.

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04-09-1970 дата публикации

Patent FR2024912A1

Номер: FR2024912A1
Автор:
Принадлежит: Daimler Benz AG

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14-12-1962 дата публикации

Internal combustion engine with rotary piston

Номер: FR1312340A
Автор:
Принадлежит: N S U MOTORENWERKE AG, Wankel GmbH

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31-01-1975 дата публикации

Oil seal for piston of rotary engine - uses oil press. to keep scraper rings on inner ring pressed against rotor

Номер: FR2236379A5
Автор: [UNK]
Принадлежит: Fives Lille Cail

The scraper rings (16) are located in grooves in a ring (14) containing grooves for 0-rings (20) and (24). The annular space (22) communicates with a hole (26) to which high pressure oil is supplied. The oil pressure forces the ring (14) against the scraper rings (16) which prevent oil leaking into the compression chamber. To remove oil which seeps past the 0-rings a hole is bored through the ring (14) and a pipe fitted to lead the oil away through a hole similar to the hole (26) but in a different part of the ring. Sealing load can be increased by compression springs which maintain the load in the event of oil pressure failure.

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27-12-1963 дата публикации

Radial seal for rotary piston machine

Номер: FR1347541A
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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25-11-1966 дата публикации

Rotary piston engine

Номер: FR1460260A
Автор:
Принадлежит: Beteiligungs und Patentverwaltungs GmbH

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24-12-1964 дата публикации

Radial seal for rotor

Номер: FR1383289A
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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05-09-1922 дата публикации

Improvements in rotary engines

Номер: FR543599A
Принадлежит:

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09-08-1991 дата публикации

INTERNAL COMBUSTION ENGINE WITH ROTARY PISTON.

Номер: FR2657919A1
Автор: Dankwart Eiermann
Принадлежит: Wankel GmbH

Moteur à combustion interne à piston rotatif dans lequel il est prévu sur l'excentrique (9), entre la roue à denture intérieure (12) et le pignon (13) du mécanisme de synchronisation (14), un élément de garniture (22) recouvrant celui-ci, qui est rendu étanche, dans son coulissement par rapport aux autres volumes du carter (1), par une bague d'étanchéité (23) coaxiale à l'arbre d'excentrique (6), disposée sur un épaulement (28) de l'alésage d'arbre (29), dans la partie latérale (2) adjacente ainsi que par une bague d'étanchéité (24), excentrée par rapport à l'arbre d'excentrique (6), placée dans le piston (10), sur un épaulement (27) du siège de la roue à denture intérieure (12) et en ce qu'en outre le palier d'excentrique (11) est rendu étanche, sur le côté opposé au mécanisme de synchronisation (14), par une bague d'étanchéité située entre l'excentrique (9) et le piston (10). Internal combustion engine with rotary piston in which there is provided on the eccentric (9), between the internal toothed wheel (12) and the pinion (13) of the synchronization mechanism (14), a packing element (22) covering the latter, which is sealed, in its sliding relative to the other volumes of the casing (1), by a sealing ring (23) coaxial with the eccentric shaft (6), arranged on a shoulder ( 28) of the shaft bore (29), in the adjacent side part (2) as well as by a sealing ring (24), eccentric with respect to the eccentric shaft (6), placed in the piston (10), on a shoulder (27) of the seat of the internally toothed wheel (12) and in that in addition the eccentric bearing (11) is sealed, on the side opposite to the synchronization mechanism ( 14), by a sealing ring located between the eccentric (9) and the piston (10).

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25-09-1964 дата публикации

Radial sealing ring for rotary piston machine

Номер: FR1373473A
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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25-02-1966 дата публикации

Radial sealing device for rotary piston machine

Номер: FR86541E
Автор:
Принадлежит: NSU Motorenwerke AG, Wankel GmbH

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30-06-1967 дата публикации

Rotary piston engine

Номер: FR1487213A
Автор:
Принадлежит: Sachsenring Automobilwerke VEB

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15-12-1961 дата публикации

Rotary piston machine, in particular internal combustion engine

Номер: FR1279051A
Автор:
Принадлежит: Curtiss Wright Corp

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18-03-1977 дата публикации

TURBOMACHINE

Номер: FR2321585A1
Автор: [UNK]
Принадлежит: Applied Power Inc

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03-11-1962 дата публикации

Sealing device for the rotating piston of a rotating piston machine

Номер: FR1308283A
Автор:

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25-09-1964 дата публикации

Internal combustion engine with rotary piston according to a trochoidal embodiment

Номер: FR1373378A
Автор: Wolf Dieter Bensinger
Принадлежит: Daimler Benz AG

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15-02-1963 дата публикации

Sealing device for rotary type piston machines

Номер: FR1318277A
Автор:
Принадлежит: NSU Motorenwerke AG, Wankel GmbH

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09-11-1962 дата публикации

Rotary piston engine

Номер: FR1309111A
Автор: Wolf Dieter Bensinger
Принадлежит: Daimler Benz AG

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29-06-1962 дата публикации

Improvements to rotary engine segments

Номер: FR1297241A
Автор:

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11-07-1980 дата публикации

DEVICE FOR SEALING BETWEEN THREE MOVABLE PARTS IN RELATION TO THE OTHERS, PARTICULARLY FOR ROTARY PISTON ENGINES

Номер: FR2444165A1
Автор: [UNK]
Принадлежит: Rotary Motor Co Ag Rmc

Sur une première pièce 7 susceptible de tourner, il est prévu un premier ensemble d'éléments d'étanchéité 1, 4 qui suivent la circonférence de cette pièce et sont reliés de maniere étanche à un deuxième ensemble d'éléments d'étanchéité 3 s'étendant transversalement aux premiers éléments d'étanchéité, et un troisième ensemble d'éléments d'étanchéité 2 sont prévus aux extrémités d'une deuxième pièce 8 animée d'un mouvement de va-et-vient à travers la première pièce, les éléments d'étanchéité du troisième ensemble étant en contact étanche avec ceux du deuxième ensemble et tous les éléments d'étanchéité prenant appui contre une troisième pièce formant carter. On a first part 7 capable of turning, there is provided a first set of sealing elements 1, 4 which follow the circumference of this part and are connected in a leaktight manner to a second set of sealing elements 3 s' extending transversely to the first sealing elements, and a third set of sealing elements 2 are provided at the ends of a second part 8 driven back and forth through the first part, the elements d sealing of the third assembly being in leaktight contact with those of the second assembly and all the sealing elements bearing against a third part forming a casing.

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30-08-1968 дата публикации

Rotary piston combustion engine

Номер: FR1538269A
Автор:

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26-08-1983 дата публикации

GAS SEALING STRUCTURE FOR PALLET-TYPE INTERNAL COMBUSTION ENGINES.

Номер: FR2522068A1
Принадлежит: ORBITAL ENG Pty

An orbital engine has vanes (70) supported by the engine housing and piston member (40) to reciprocate radially in the housing as the piston member (40) orbits. Vane legs (72) extending along the end faces (42) of the piston member (40) slide relative thereto in a direction at right angles to the reciprocating movement of the vane (70). A seal assembly mounted in each vane leg (72) has a seal pad (86) directed towards and co-operating with a seal ring (60) carried in a groove in the end face (42) of the piston member (40) and a base portion (85) which engages a face in the end wall of the housing so that the vane (70) may move in the axial direction of the piston member axis relative to the seal assembly and independently thereof. Springs are provided to urge the seal pad (86) radially outward to engage the transverse face (80a) of the vane (70) which slides on the outer periphery of the piston member (40) to maintain sealing between the external corner of the piston member (40) and the internal corner of the vane (70) at the junction of the vane transverse face (80a) and the vane leg (72).

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13-09-1963 дата публикации

Device forming a rotary piston machine and in particular a combustion engine or the like

Номер: FR1337601A
Автор:
Принадлежит: NSU Motorenwerke AG, Wankel GmbH

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01-12-1961 дата публикации

Internal combustion engine with rotary piston

Номер: FR1277873A
Автор:
Принадлежит: Curtiss Wright Corp

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26-03-1965 дата публикации

Radial seal for rotary piston machine

Номер: FR1393877A
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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23-10-1964 дата публикации

sealing for pistons

Номер: FR83850E
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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10-09-2009 дата публикации

System for sealing the piston of rotary piston machines

Номер: KR20090096497A
Автор: 에께르트 균타
Принадлежит: 에께르트 균타

본 발명은 로터리 피스톤 엔진의 밀봉 시스템에 관한 것으로서, 회전자는 회전자 디스크(1, 2)를 포함하고, 상기 회전자 디스크는 서로 나란히 배열되고 회전자의 동축에 배열되고 상기 디스크들 사이의 간격(11)에 스프링 및/또는 가스 힘을 작용함으로써 서로를 밀어 바깥쪽으로 압착되고, 이로 인해 하우징의 측벽을 향하는 상기 디스크(1, 2)의 단부면(6, 8)이 상기 하우징에 밀봉 방식으로 지지되어 작동 매체가 축에 접근하는 것을 방지하는 것을 특징으로 하는 로터리 엔진의 밀봉 시스템에 관한 것이다. 또한, 본 발명은 조립체에 관한 것으로서, 이동가능한 라멜라 형상부(3, 4)로 구성된 조립체가 상기 디스크(1, 2) 사이의 간격에 배열되고, 상기 라멜라 형상부는 간격의 폭에 변화에 따라 변화하여 회전자 주위로 내부 유동이 발생하지 않도록 하는 조립체에 관한 것이다. 로터리 엔진, 밀봉 시스템, 래버린스 밀봉부, F.반켈, 라멜라 형상부, 케이싱, 회전자

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21-07-2017 дата публикации

DEVICE FOR SEALING BETWEEN A HYDRAULIC PUMP BODY AND A TRANSMISSION ELEMENT

Номер: FR3046818A1
Принадлежит: RENAULT SAS

Dispositif d'étanchéité (12) entre l'intérieur d'un corps de pompe hydraulique (3) renfermant un premier fluide hydraulique et un arbre relais (6) tournant l'intérieur d'un arbre creux (9) s'étendant au travers du corps de pompe en y étant lubrifié par un deuxième fluide hydraulique distinct du premier, caractérisé en ce qu'il est composé d'une bague rigide (11) fixée sur l'arbre creux (9) et de deux joints d'étanchéité dynamiques (12a, 12b) disposés sur deux faces opposées de celle-ci, prenant appui sur la bague (11) et le carter (3c) du corps de pompe d'une part, et sur la bague (11) et l'arbre relais (9) d'autre part. Sealing device (12) between the inside of a hydraulic pump body (3) enclosing a first hydraulic fluid and a relay shaft (6) rotating inside a hollow shaft (9) extending through the pump body is lubricated by a second hydraulic fluid distinct from the first, characterized in that it is composed of a rigid ring (11) fixed on the hollow shaft (9) and two dynamic sealing seals (12a, 12b) disposed on two opposite faces thereof, bearing on the ring (11) and the casing (3c) of the pump body on the one hand, and on the ring (11) and the relay shaft (9) secondly.

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07-01-1966 дата публикации

Rotary piston engine

Номер: FR1424140A
Автор:
Принадлежит: Toyo Kogyo Co Ltd

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24-05-1963 дата публикации

Sealing device for piston machines, rotary type

Номер: FR1328140A
Автор:
Принадлежит: NSU Motorenwerke AG, Wankel GmbH

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14-05-1965 дата публикации

Internal seal for rotary piston machine

Номер: FR1399278A
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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01-02-1974 дата публикации

Patent FR2191615A5

Номер: FR2191615A5
Автор: [UNK]
Принадлежит: Wankel GmbH

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11-03-1966 дата публикации

Improvements to radial sealing rings for rotary motors

Номер: FR1431008A
Автор:

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04-02-1966 дата публикации

Seal, in particular piston seal for rotary engines or compressors

Номер: FR1427411A
Автор:
Принадлежит: Ustav Pro Vyzkum Motorovych Vozidel

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02-02-1968 дата публикации

Piston for a rotary piston internal combustion engine

Номер: FR1511594A
Автор: Wolf-Dieter Bensinger
Принадлежит: Daimler Benz AG

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24-07-1964 дата публикации

Sealing device for rotary piston explosion machines

Номер: FR1367929A
Автор:
Принадлежит: ZSCHOPAU MOTORRAD VEB

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15-10-1965 дата публикации

Axial seal for internal combustion rotary piston engines

Номер: FR1414440A
Принадлежит: Daimler Benz AG

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24-05-1963 дата публикации

Improvements to rotary engines or similar machines

Номер: FR1327899A
Автор: Louis Henri Vesseron
Принадлежит:

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21-12-1962 дата публикации

Sealing strip for rotary piston machines

Номер: FR1312659A
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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10-06-1960 дата публикации

Sealing device for rotary piston machines and machines equipped with this device

Номер: FR1222462A
Автор: Felix Wankel
Принадлежит: NSU Werke AG

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19-01-1962 дата публикации

Segments for rotary engines

Номер: FR1281913A
Автор:

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20-12-1963 дата публикации

Sealing device for rotary piston internal combustion engine

Номер: FR1346659A
Автор:
Принадлежит: Fichtel and Sachs AG

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20-12-1963 дата публикации

Radial seal for rotary piston machine

Номер: FR1346949A
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

Подробнее
15-02-1963 дата публикации

Internal combustion engine

Номер: FR1318197A
Автор: Hermann Papst
Принадлежит:

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16-04-1982 дата публикации

Rotary piston steam engine - has oscillating mass on piston to balance forces to prevent distortion and maintain sealing

Номер: FR2491995A1
Автор: [UNK]
Принадлежит: Blaise Jean Yves

The engine has a toroidal stator chamber (1). A rotor (4) carries a piston (3) which travels round the chamber. The chamber has inlet and exhaust ports and is divided by radial vanes which move back to allow the piston to pass. The piston has a sealing strip (11) round it, and has a recess in which there is a mass (12) which can move radially. The mass is connected to the sealing strip by two levers (13) pivoted on the piston. The arms of the levers are arranged so that the moments of the forces produced by the kinetic energies of the strip and mass are equal.

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25-06-1976 дата публикации

ROTARY PISTON RING

Номер: FR2292870A1
Автор: [UNK]
Принадлежит: Sealed Power Corp

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30-08-1972 дата публикации

Oil seal construction for rotary internal combustion engine

Номер: IL39641A0
Автор: [UNK]
Принадлежит: Toyo Kogyo Co

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01-01-1974 дата публикации

Housing sealing means for rotary engines

Номер: CA939271A
Автор: Charles Jones
Принадлежит: Curtiss Wright Corp

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30-07-2009 дата публикации

Sealing System For An Oscillating-Piston Engine

Номер: US20090188460A1
Автор: Arnold Wagner
Принадлежит: Peraves AG

The sealing system for oscillating-piston engines, comprising at least two oscillating pistons ( 15 ) which revolve together in a spherical housing ( 24 ) about an axis ( 45 ) of revolution provided in the housing centre and which each have two opposite piston arms, which, when revolving, perform reciprocating oscillating movements in opposite directions about an oscillation axis ( 46 ) perpendicular to the axis ( 45 ) of revolution, wherein guide members ( 47 ) are provided on at least two pistons, said guide members ( 47 ) engaging in at least one guide groove ( 39 ) formed in the housing ( 24 ) for controlling the oscillating movements, has sealing elements ( 1, 2, 12, 14, 26, 33 ) on or in the vicinity of all moving edges surrounding the working chambers ( 17 ) and prechambers ( 30 ), which sealing elements ( 1, 2, 12, 14, 26, 33 ) close in a sealing manner all the gap regions present between machine parts displaced relative to one another by revolving and/or oscillating movements and not in direct contact, and has additional sealing elements ( 60 ) which prevent the excessive penetration of lubricating fluid into inlet ( 40 ) and outlet openings ( 41 ) in the housing ( 24 ).

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01-11-1977 дата публикации

Rotary piston engine

Номер: US4056338A
Автор: Dankwart Eiermann
Принадлежит: Wankel GmbH

A rotary piston engine in which the housing has an opening in at least one end wall that is controlled by the piston. The end seals on the piston and the sealing bolts at the juncture thereof are located radially inwardly from the opening, while the corner seals of the piston have legs at the ends of the piston extending to the sealing bolts. The corner seals are disposed in planes which in the radially inward direction diverge from the radial planes of the piston passing through the corners of the piston.

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22-04-2004 дата публикации

A rotary engine

Номер: WO2004033856A1
Автор: Barry Hudson
Принадлежит: Barry Hudson

A rotary engine (2) comprises a housing (16) having a male rotor (4) having a plurality of projecting lobes (12) and a female rotor (8) having a plurality of cavities (14). The male (4) and female rotors (8) are mounted for synchronous rotation about parallel axes such that during rotation successive lobes (12) on the male rotor (4) mate with successive cavities (14) on the female rotor (8) to define therewith a combustion chamber (26) in which a mixture of air and fuel is compressed by the interaction of the lobe (12) and the cavity (14) during rotor rotation. At least one exhaust port (78, 80) leads out of the housing (16) for discharge of exhaust gases from the cavity (14) of the female rotor (8) following combustion and from the space (74) between adjacent lobes (12) of the male rotor (4) following combustion. Respective purge ports (44, 46) lead out of the housing (16) downstream of the exhaust port (78, 80) in the direction of rotor rotation to facilitate discharge of residual exhaust gases from the cavity (14) and inter-lobe space (74), the purge ports (44, 46) being associated with air inlet ports (48, 50) to admit air into the cavity (14) and inter-lobe space (74) in preparation for the subsequent combustion cycle.

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19-01-1966 дата публикации

Rotary piston machines

Номер: GB1017568A
Автор:
Принадлежит: NSU Motorenwerke AG, Wankel GmbH

1,017,568. Rotary-piston engines. NSU MOTORENWERKE A.G. and WANKEL G.m.b.H. Oct. 10, 1963 [Oct. 13, 1962], No. 39975/63. Heading F1F. In a rotary-piston I.C. engine of the trochoidal n and n+1 lobe type annular members 14, 15 are attached to end faces of an eccentric 7 on which the piston 8 is rotatably mounted, and metallic sealing-rings 16 are lodged between said members and the end walls of the piston to prevent lubricant entering the working chambers. A rubber ring 17<SP>1</SP> is provided in each sealing ring to effect sealing between the ring and an adjacent flange 19 on the periphery of the associated annular member, the ring being biased in the direction of the piston by a leafspring 17. Each of the annular members has a central tubular hub 22, or 23, in engagement with an aperture in the adjacent side wall 3, or 4, of the engine housing, spiral grooves 23 being formed in said hubs to seal a clearance gap 24. Cooling of the piston is accomplished by circulation of lubricant through passages 30, 31 in the annular members and a cavity 13 in the piston, the lubricant also serving to lubricate gearing 10, 11 for controlling the planetary motion of the pistons, a bearing 9 supporting the piston on the eccentric, and bearings for a power-output shaft 6. Each of the rings 16 may be replaced by a ring 16<SP>1</SP> (Fig. 3, not shown) which is pressed by springs against a ring 25 attached to the piston and having a flange 25 mating with a groove in the associated annular member. An outwardly-inclined gap 27 between each annular member and the corresponding ring 25 serves to return lubricant by centrifugal action to cavity 13. Alternatively, sealing between the annular members and the piston is effected by the provision of a narrow gap between each ring 25 and the associated annular member (Fig. 4, not shown), or each ring 25 has axially-extending flanges mating with grooves in the adjacent annular member to form a labyrinth seal (Fig. 5, not ...

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26-03-1965 дата публикации

Radial seal for rotary piston engine

Номер: FR1393878A
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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17-10-2012 дата публикации

Rotating piston machine

Номер: JP5053637B2
Принадлежит: ROBERT BOSCH GMBH

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25-07-2013 дата публикации

Sealing element for a planetary rotation machine

Номер: WO2012107279A3
Принадлежит: ELRINGKLINGER AG

The invention relates to a sealing element for a planetary rotation machine for sealing a lever which is guided in an annular gap and can be rotated about a rotational axis, wherein the sealing element is rotationally symmetrical relative to the rotational axis. The sealing element comprises a dynamic region and a static region, wherein the dynamic region has an axial sealing face which faces the annular gap, and a radial sealing face which faces the interior of an annular channel of the planetary rotation machine, which channel surrounds the annular gap, and wherein the static region is used to fix the sealing element to the planetary rotation machine, and wherein a channel, to which fluid can be supplied, is formed in the static region.

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23-07-1974 дата публикации

Fluid seal for piston of rotary piston mechanism

Номер: CA951757A
Принадлежит: Curtiss Wright Corp

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15-05-1981 дата публикации

Patent JPS5620482Y2

Номер: JPS5620482Y2
Автор: [UNK]
Принадлежит: [UNK]

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22-11-1966 дата публикации

Radial sealing device for rotary piston engine

Номер: US3286699A
Автор: Frenzel Manfred
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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16-04-1965 дата публикации

Improvements to sealing rings for rotary engines

Номер: FR1395747A
Автор:

Подробнее
23-04-1965 дата публикации

Radial seal for rotary piston

Номер: FR1396939A
Автор:
Принадлежит: GOETZEWERKE FRIEDRICH GOETZE AG

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07-05-2015 дата публикации

Positive displacement blower with a sealing system

Номер: WO2015063252A1
Автор: Hubert Hamm
Принадлежит: ENVA Systems GmbH

Vorrichtung (1) zur Umwandlung von in einem Fluid enthaltener Energie mit einem Gehäuse (2), das einen Arbeitsraum (7), wenigstens einen Ölraum (21), eine Eintrittsöffnung (5) und eine Austrittsöffnung (6) aufweist, wenigstens zwei im Gehäuse (2) drehbar gelagerten Rotoren (8), die jeweils wenigstens zwei Flügel (10) aufweisen, wobei die Drehachsen (9) der Rotoren (8) achsparallel zueinander angeordnet sind, und wobei die Rotoren (8) gegenläufig und mit gleicher Drehzahl betreibbar sind. Um zu erreichen, dass sich die Vorrichtung (1) als Strömungsmaschine zur Energiegewinnung, insbesondere als Turbine, eignet, wird zwischen dem Arbeitsraum (7) und dem Ölraum (21) wenigstens ein Dichtsystem (20) angeordnet.

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17-09-1991 дата публикации

Rotary piston internal combustion engine

Номер: US5049049A
Автор: Dankwart Eiermann
Принадлежит: Wankel GmbH

A rotary piston internal combustion engine of trochoidal-type of construction with a slidably journalled piston controlled by a synchronous transmission gear drive unit, with which the synchronous transmission gear drive unit is covered coinciding with an insert part threaded with respect to the remaining machine parts adjacent to the eccentric. The insert part has a hollow cylinder covering the hollow gear of the synchronous transmission gear drive unit eccentric to the eccentric shaft, which hollow cylinder is sealed-off with a sealing ring relative to one shoulder of the piston, as well as a further hollow cylinder coaxial to the eccentric shaft surrounding the holding part for the pinion with a gap or space therebetween, which further hollow cylinder projects into a shaft bore in the side part and is sealed-off relative thereto by a sealing ring. Upon another bearing side there is provided an annular chamber sealed-off relative to the remaining machining spaces or chambers and from which annular chamber the oil discharging from the bearing is conveyed through the cooling chambers of the piston to the synchronous transmission gear drive unit. The oil is discharged through a gap space in a discharge passage or channel in the sidewall formed by the coaxial hollow cylinder.

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22-04-1988 дата публикации

CAPSULISM WITH PALLETS CONTROLLED ON BEARINGS FOR MOTORS AND PUMPS

Номер: FR2571779B1
Автор:
Принадлежит: SZLOSARCZYK JEAN

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