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US 2015/0308381 A1Published application
Drag link assembly including buried drag link fitting
AssigneeRohr, Inc.
InventorStuart J. Byrne
Life of this patent
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AssigneeRohr, Inc.
InventorStuart J. Byrne
Estimating the term…
A drag link assembly for use in a thrust reverser of a propulsion system is provided. The thrust reverser includes a fixed structure and a translating structure that at least partially define an annular airstream bypass duct there between. The translating structure is moveable relative to the fixed structure. The translating structure includes a blocker door disposed at least partially within the airstream bypass duct. The drag link assembly includes a drag link fitting and a drag link. The drag link fitting is fastened to the fixed structure of the thrust reverser. The drag link includes a first end portion and an opposing second end portion. The first end portion is pivotably connected to the blocker door. The second end portion is pivotably connected to the drag link fitting. The second end portion includes a curved section.
A drag link assembly for use in a thrust reverser of a propulsion system, the thrust reverser including a fixed structure and a translating structure that at least partially define an annular airstream bypass duct there between, the translating structure being moveable relative to the fixed structure, the translating structure including a blocker door disposed at least partially within the airstream bypass duct, the drag link assembly comprising:
A thrust reverser of a gas turbine propulsion system for an aircraft, comprising:
Dependencies are inferred from the claim text.