ADJUSTABLE LANDING GEAR VIBRATION SUPPRESSION
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United States of America Patent
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Issued Date -
May 4, 2017
app pub date -
Nov 4, 2015
filing date -
Nov 4, 2015
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Abstract
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.
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