A damper for an aircraft landing gear includes a housing with an internal cavity. A weight is slidingly disposed within the cavity and positioned between and engages a first pneumatic spring and a second pneumatic spring. The shimmy damper includes at least one mounting feature to fixedly mount the housing to a component of the aircraft landing gear.
ADJUSTABLE LANDING GEAR VIBRATION SUPPRESSION
2017-05-04
Patent
Electronic Resource
English
LANDING GEAR VIBRATION ABSORBER AND METHOD OF OPERATING SAID LANDING GEAR VIBRATION ABSORBER
European Patent Office | 2016
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