Shock absorber for a landing gear leg of an aircraft and landing gear of an aircraft with such a

DE102025103641B3Undetermined Publication Date: 2026-07-23LIEBHERR AEROSPACE LINDENBERG GMBH
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Patent Information

Application Number
DE102025103641
Authority / Receiving Office
DE · DE
Patent Type
Patents
Current Assignee / Owner
Filing Date
2025-01-31
Publication Date
2026-07-23
Estimated Expiration
2045-01-31

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Abstract

The invention relates to a shock absorber for a landing gear leg of an aircraft, in particular an airplane, comprising a housing, a thrust tube that is retractable into and out of the housing, and a first damping device that exerts a first preload force acting in the extension direction of the thrust tube to dampen movement of the thrust tube in the retraction direction. The invention is characterized in that the first damping device is arranged to be reciprocally movable in the housing in the extension and retraction direction of the thrust tube between a rear stop and a front stop.
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Citation Information

Patent Citations

  • Aircraft landing gear shock absorber strut

    WO2024028573A1