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US 2012/0256050 A1Published application
Bogie stop block
AssigneeMessier-Dowty Limited
InventorsMatthew Hilliard, Ian Bennett
Life of this patent
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Abstract
An aircraft landing gear assembly including a bogie beam, a landing gear strut having a first end arranged to be pivotally coupled to an aircraft and a second end pivotally coupled to the bogie beam, and a stop arranged to limit pivotal movement of the bogie beam relative to the landing gear strut, wherein the stop comprises at least one elongate member arranged to be deflectable in bending when the bogie beam reaches a pivotal limit.
Claims16
An aircraft landing gear assembly comprising:
- a bogie beam;
- a landing gear strut having a first end arranged to be pivotally coupled to an aircraft and a second end pivotally coupled to the bogie beam;
- and
- a stop arranged to limit pivotal movement of the bogie beam relative to the landing gear strut,
- wherein the stop comprises an one elongate member arranged to be deflectable in bending when the bogie beam reaches a pivotal limit.
2 more elements
Dependencies are inferred from the claim text.