Invention Grant
- Patent Title: Aircraft flight control surface actuator
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Application No.: US15517325Application Date: 2015-11-19
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Publication No.: US10399669B2Publication Date: 2019-09-03
- Inventor: Severin Viennot , Thierry Cartry , Marc Lebrun
- Applicant: Safran Electronics & Defense
- Applicant Address: FR Boulogne-Billancourt
- Assignee: SAFRAN ELECTRONICS & DEFENSE
- Current Assignee: SAFRAN ELECTRONICS & DEFENSE
- Current Assignee Address: FR Boulogne-Billancourt
- Agency: Womble Bond Dickinson (US) LLP
- Priority: FR1461246 20141120
- International Application: PCT/EP2015/077165 WO 20151119
- International Announcement: WO2016/079270 WO 20160526
- Main IPC: F16H35/10
- IPC: F16H35/10 ; B64C13/34 ; F16H1/46 ; F16H1/28

Abstract:
An actuator for a flight control surface of an aircraft, including: a fixed annulus for fixing to the fuselage, an rotatable annulus with respect to the fixed annulus about an axis of rotation, an output ring which can be fixed to the control surface, and a coupling mechanism having a disc with translational mobility with respect to the mobile annulus in a direction parallel to the axis of rotation, the disc able to move between an engaged position, and a disengaged position, in which the disc is disengaged from the mobile annulus to disconnect the output ring from the mobile annulus. A retaining piece keeps the disc in the engaged position, and a rupture member activates to break the retaining piece to allow the disc to move into the disengaged position.
Public/Granted literature
- US20170305533A1 AIRCRAFT FLIGHT CONTROL SURFACE ACTUATOR Public/Granted day:2017-10-26
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