Invention Grant
- Patent Title: Actuating assembly for a thrust reverser of an aircraft engine
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Application No.: US14133327Application Date: 2013-12-18
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Publication No.: US09874268B2Publication Date: 2018-01-23
- Inventor: Pierre Moradell-Casellas , Franck Delnaud
- Applicant: AIRCELLE , SAGEM DEFENSE SECURITE
- Applicant Address: FR Gonfreville l'Orcher
- Assignee: AIRCELLE
- Current Assignee: AIRCELLE
- Current Assignee Address: FR Gonfreville l'Orcher
- Agency: Burris Law, PLLC
- Priority: FR1155402 20110620
- Main IPC: F16H25/22
- IPC: F16H25/22 ; F02K1/76 ; F16H25/24 ; F02K1/56 ; F16H25/20

Abstract:
An actuating assembly for an aircraft engine thrust reverser includes a drive shaft bearing a master pinion; a ball screw bearing a slave pinion engaging with the master pinion; a nut capable of translating over the ball screw as a result of the rotation of the ball screw; an extension tube rigidly secured to the nut and a lock assembly to block the rotation of the drive shaft in a so-called direct jet position of the reverser. The extension tube includes, at its free end, a member for connecting to a portion of the reverser prior to being actuated. In particular, the lock assembly includes an abutment secured to the drive shaft, and a cotter moveable between a locking position and an unlocking position. The reduction ratio (R) between the slave and master pinions is even.
Public/Granted literature
- US20140234089A1 ACTUATING ASSEMBLY FOR A THRUST REVERSER OF AN AIRCRAFT ENGINE Public/Granted day:2014-08-21
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