Title:
AIRCRAFT LANDING GEAR WITH INTEGRATED EXTENSION, RETRACTION, AND LEVELING FEATURE
Document Type and Number:
WIPO Patent Application WO2008060338
Kind Code:
A9
Abstract:
Electrically controlled and/or actuated landing gear mechanisms are presented that allow for adjustment of aircraft attitude on the ground as well as for retraction and extension of the landing gear in a single unit. Most preferably, the electric actuator is positioned within the diameter of the strut to thereby form a compact and load bearing structure.
Inventors:
WAIDE WILLIAM MARTIN (US)
Application Number:
PCT/US2007/014563
Publication Date:
August 14, 2008
Filing Date:
June 22, 2007
Export Citation:
Assignee:
KAREM AIRCRAFT INC (US)
WAIDE WILLIAM MARTIN (US)
WAIDE WILLIAM MARTIN (US)
International Classes:
B64C25/00
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