Invention Application
- Patent Title: LANDING GEAR
- Patent Title (中): 起落架
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Application No.: US13333249Application Date: 2011-12-21
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Publication No.: US20120091271A1Publication Date: 2012-04-19
- Inventor: Ian BENNETT , Richard C. LANG , Robert A. MENEZES
- Applicant: Ian BENNETT , Richard C. LANG , Robert A. MENEZES
- Applicant Address: GB Gloucester
- Assignee: MESSIER-DOWTY LIMITED
- Current Assignee: MESSIER-DOWTY LIMITED
- Current Assignee Address: GB Gloucester
- Priority: GBGB0516030.4 20050804
- Main IPC: B64C25/20
- IPC: B64C25/20

Abstract:
A semi-levered landing gear for an aircraft includes a main shock absorber strut, a bogie beam and an auxiliary actuator mechanism. The bogie beam extends fore and aft of an airframe of the aircraft with forward and aft axles for respective forward and aft wheels, and a main pivot between the forward and aft axle pivotally connected to the lower portion of the main shock absorber strut. The auxiliary actuator mechanism includes a spring unit pivotally connected at a lower end to an auxiliary pivot on the bogie forward of the main pivot, and at an upper end to an anchor point offset from the pivot connection of the upper portion to the aircraft fuselage. During stowing the strut and spring unit pivot together about different pivot points, causing a relative longitudinal movement between the main pivot and auxiliary pivot that further tilts the bogie beam to a stowing position.
Public/Granted literature
- US08382032B2 Landing gear Public/Granted day:2013-02-26
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