AIRCRAFT NOSE LANDING GEAR

A front aircraft landing gear built into an electric control including: a landing gear leg to be pivotably mounted on a structure of the aircraft between a retracted position and an extended position; an actuating cylinder moving the landing gear leg from the retracted position to the extended posit...

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Bibliographic Details
Main Author REYNES, DIDIER
Format Patent
LanguageEnglish
French
German
Published 07.11.2012
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:A front aircraft landing gear built into an electric control including: a landing gear leg to be pivotably mounted on a structure of the aircraft between a retracted position and an extended position; an actuating cylinder moving the landing gear leg from the retracted position to the extended position; a strut that maintains the landing gear leg in the extended position thereof; an uplock housing that maintains the landing gear leg in the retracted position thereof; an uplock housing an operating mode control and a backup mode for the same housing; and four stress-adding points adding stress to the aircraft structure, namely two points for the pivotal movement of the landing gear leg and two points for the pivotal movement of the strut.
Bibliography:Application Number: EP20090769485