Title:
音響処理を含む逆推力装置カスケード
Document Type and Number:
Japanese Patent JP7417632
Kind Code:
B2
Abstract:
A cascade for a thrust reverser device intended to be mounted on a turbomachine of an aircraft, the cascade including first partitions extending in a first direction, seconds partitions extending in a second direction orthogonal to the first direction, the second partitions extending in a third direction secant to a plane comprising first and second directions between a first and a second end. Each second partition forms, with reference planes parallel to the second direction and to the third direction, a plurality of different angles at positions distinct from the height of the second partitions separating the first end from the second end of the second partitions, each angle being formed between a reference plane and the tangent to the second partition taken at the intersection between said corresponding reference plane and the second partition at the position of the height of the corresponding second partition.
Inventors:
Jode, Norman Bruno Andre
Gonzales, Jeremy Paul Francisco
Gonzales, Jeremy Paul Francisco
Application Number:
JP2021564991A
Publication Date:
January 18, 2024
Filing Date:
April 03, 2020
Export Citation:
Assignee:
Saffron Aircraft Engines
International Classes:
F02K1/72; B64D27/10; B64D29/06; B64D33/00; F01D25/00; F02C7/24; F02K1/44
Domestic Patent References:
| JP2017078415A | ||||
| JP2009062977A | ||||
| JP2002167290A |
Foreign References:
| US20160326985 | ||||
| US20080072571 | ||||
| US20140027536 | ||||
| US20170058829 | ||||
| US20160273488 | ||||
| US20150285184 | ||||
| US20160263820 |
Attorney, Agent or Firm:
Kawaguchi International Patent Office