AIRCRAFT LANDING GEAR PROVIDED WITH A LEAF SPRING LOCKING DEVICE
An aircraft undercarriage comprising: a leg connected to an aircraft structure to be movable between a deployed position and a retracted position; a brace member for holding the leg in its deployed position and comprising a first rod hinged to the aircraft structure and a second rod hinged to the fi...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | An aircraft undercarriage comprising: a leg connected to an aircraft structure to be movable between a deployed position and a retracted position; a brace member for holding the leg in its deployed position and comprising a first rod hinged to the aircraft structure and a second rod hinged to the first link and to the leg; a stabilizer member for holding the first and second rods in an aligned position and comprising a first link and a second link that are hinged to each other, with at least one of them being hinged to the brace member; and a spring for elastically urging the hinges of the first and second links into a generally aligned position.The spring comprises at least one spring blade arranged to be subjected to an axial compression force when the first and second links leave the generally aligned position. |
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