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US 4,541,673 AGranted
Removable slider shoe for a translating sleeve used on a jet engine cowl and duct
AssigneeThe Boeing Company
InventorAlfred H. Greiert
Life of this patent
Estimating the term…
Abstract
A removable slider shoe for mounting on a translating sleeve of a jet engine cowl and duct. The sleeve includes a slider which moves in a track on the cowl when the engine is in a reverse thrust mode in order to expose airflow turning vanes. The movable shoe is mounted on the slider.
Claims2
A removable slider shoe for mounting on a translating device of a jet engine cowl and duct, the sleeve having a slider which moves in a circular track on the cowl, the shoe comprising:
- an elongated first shoe half having a portion of its outer circumference rounded and adapted for receipt on one side of the slider, the first shoe half having a plurality of lugs integrally formed in the inner circumference thereof and extending outwardly therefrom, the lugs adapted for receipt in slots along the length of the slider;
- an elongated second shoe half having a portion of its outer circumference rounded and adapted for receipt on the opposite side of the slider, the second shoe half having a plurality of lugs integrally formed in the inner circumference thereof and extending outwardly therefrom, the lugs adapted for receipt in slots along the length of the slider, the lugs of the first and second shoe halves transmitting fore and aft loads from the shoe halves to the slider;
- and
- a plurality of apertures through the shoe halves and the slider for receiving fasteners therethrough and securing the shoe halves to the sides of the slider.
1 more element
Dependencies are inferred from the claim text.