Blade for a rotating bladed disk for an aircraft turbine engine comprising a sealing lip having an optimized non-constant cross section

09-01-2024 дата публикации

Номер:

US0011867065B2

Автор: Edouard Emmanuel Garreau, Josserand Jacques André BASSERY, Lucas Geoffrey Desbois, Etienne Léon FRANCOIS, Samuel Laurent Noel Mathieu Juge, Elsa Maxime, Ba-Phuc Tang, Denis Gabriel TRAHOT, Thomas Tsassis

Принадлежит: SAFRAN AIRCRAFT ENGINES

Контакты:

Номер заявки: 69-03-1776

Дата заявки: 11-02-2021

CPC - классификация

F F0 F01 F01D F01D1 F01D11 F01D11/F01D11/0 F01D11/00 F01D11/001 F05 F05D F05D2 F05D22 F05D222 F05D2220 F05D2220/F05D2220/3 F05D2220/32 F05D2220/321 F05D2220/3215 F05D2220/323 F05D224 F05D2240 F05D2240/F05D2240/8 F05D2240/80 F05D225 F05D2250 F05D2250/F05D2250/1 F05D2250/14 F05D2250/141 F05D2250/18 F05D2250/184 F05D2250/6 F05D2250/61 F05D2250/611 F05D2250/7 F05D2250/71 F05D2250/711 F05D2250/712 F05D2250/713 F05D226 F05D2260 F05D2260/F05D2260/9 F05D2260/94 F05D2260/941 Y Y0 Y02 Y02T Y02T5 Y02T50 Y02T50/Y02T50/6 Y02T50/60

IPC - классификация

F F0 F01 F01D F01D1 F01D11 F01D11/F01D11/0 F01D11/00 F01D11/005 F01D11/02 F1 F16 F16J F16J1 F16J15 F16J15/F16J15/3 F16J15/32 F16J15/329 F16J15/3292

Цитирование НПИ

416/193A
416/223A
International Search Report dated May 17, 2021 in PCT/FR2021/050247 filed on Feb. 11, 2021.
Preliminary French Search Report dated Sep. 25, 2020 in French Application 2001640 filed on Feb. 19, 2020.