Invention Grant
- Patent Title: Landing gear door damping mechanism for aircraft
- Patent Title (中): 飞机起落架门阻尼机构
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Application No.: US13800220Application Date: 2013-03-13
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Publication No.: US09334040B2Publication Date: 2016-05-10
- Inventor: Karounen Veerabadran
- Applicant: AIRBUS OPERATIONS (SAS)
- Applicant Address: FR Toulouse
- Assignee: AIRBUS OPERATIONS (S.A.S.)
- Current Assignee: AIRBUS OPERATIONS (S.A.S.)
- Current Assignee Address: FR Toulouse
- Agency: Jenkins, Wilson, Taylor & Hunt, P.A.
- Priority: EP12161567 20120327
- Main IPC: B64C1/14
- IPC: B64C1/14 ; B64C25/16 ; E05B77/00

Abstract:
The invention provides a damping mechanism which comprises a damper; and a coupling mechanism. The coupling mechanism comprises a coupling member which is pivotally attached to the damper and has a pivot bearing for pivotally connecting the coupling member to a structure when in use; and a fitting which can be engaged with the coupling member to couple the fitting with the damper and disengaged with the coupling member to decouple the fitting from the damper. More, the coupling member has a pair of parallel planar faces which taper outwardly from the pivot bearing to a convex curved edge, an upper edge and a lower edge; and a first and a second recess formed in the convex curved edge, a rib between the first and the second recesses and, a third recess formed in the lower edge.
Public/Granted literature
- US20130249152A1 LANDING GEAR DOOR DAMPING MECHANISM FOR AIRCRAFT Public/Granted day:2013-09-26
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