Invention Grant
US09126690B2 Nacelle for an aircraft engine with cascade-type thrust reverser and variable-geometry nozzle
有权
用于具有级联式推力反向器和可变几何喷嘴的飞机发动机的机舱
- Patent Title: Nacelle for an aircraft engine with cascade-type thrust reverser and variable-geometry nozzle
- Patent Title (中): 用于具有级联式推力反向器和可变几何喷嘴的飞机发动机的机舱
-
Application No.: US13662872Application Date: 2012-10-29
-
Publication No.: US09126690B2Publication Date: 2015-09-08
- Inventor: Pierre Moradell-Casellas
- Applicant: AIRCELLE
- Applicant Address: FR Gonfreville L'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: FR Gonfreville L'Orcher
- Agency: Brinks Gilson & Lione
- Priority: FR1053282 20100428
- Main IPC: F02K1/76
- IPC: F02K1/76 ; B64D29/06 ; F02K1/09 ; F02K3/075 ; F01D15/10

Abstract:
An aircraft engine nacelle is provided that includes a fixed front frame, a thrust reverser cowling mounted to slide with respect to the front frame between a direct-jet position and a reversed-jet position, a variable-geometry nozzle positioned in a downstream continuation of the reverser cowling, thrust-reversal jacks interposed between the front frame and the thrust-reverser cowling, adaptive nozzle jacks interposed between said thrust reverser cowling and the variable-geometry nozzle, drive shafts mounted on the front frame, transmission shafts extending along the thrust reverser cowling as far as the variable-geometry nozzle jacks, and mechanical means for coupling said transmission shafts to said drive shafts, and means for locking rotation of said transmission shafts before decoupling of the transmission shafts from their respective drive shafts, and when the decoupling is completed.
Public/Granted literature
- US20130062435A1 NACELLE FOR AN AIRCRAFT ENGINE WITH CASCADE-TYPE THRUST REVERSER AND VARIABLE-GEOMETRY NOZZLE Public/Granted day:2013-03-14
Information query