Semi-levered landing gear and associated method
AssigneeThe Boeing Company
InventorsMitchell L. Mellor, Michael A. Long, Richard B. Odell
Life of this patent
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AssigneeThe Boeing Company
InventorsMitchell L. Mellor, Michael A. Long, Richard B. Odell
Estimating the term…
A semi-levered landing gear is provided that includes a shock strut, a truck beam pivotally connected to the shock strut and a semi-levered landing gear mechanism including at least three links configured to angularly orient the truck beam and a truck pitch actuation system operatively connected to at least one of the three links. The landing gear mechanism may be configured to cooperate with an extension of a shock strut by positioning the truck pitch actuator in a retracted position, thereby positioning a forward end of the truck beam in a raised position relative to the aft end of the truck beam. The landing gear mechanism may also be configured to cooperate with a retraction of the shock strut into the wheel well by extending the truck pitch actuator to position a forward end of the truck beam in a lower position relative to the aft end of the truck beam.
A semi-levered landing gear comprising:
A semi-levered landing gear comprising:
Dependencies are inferred from the claim text.