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
04.05.2017
Patent
Elektronische Ressource
Englisch
LANDING GEAR VIBRATION ABSORBER AND METHOD OF OPERATING SAID LANDING GEAR VIBRATION ABSORBER
Europäisches Patentamt | 2016
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