FASTENER ASSEMBLY

Japanese Patent JP3229669

B2

PURPOSE: To offer a fastener assembly which can interconnect a forward shell section and an aft shell of an airframe components independent of the cylindrical support structure, thus maintaining circularity of the airframe components and minimizing circular distortion.
CONSTITUTION: The fastener assembly includes a cylindrical support structure 12 with a bore 44 provided partially therein, the bore 44 having a wall surface with a slot, and a bushing 16, disposed within the bore 44 of the cylindrical support structure 12, having an end and an outer surface with a slot therein. The bushing 16 further includes a bore with a first portion having a first diameter and a second portion having a second different diameter, the bushing 16 also having a pair of tangs extending from the end. The fastener assembly further includes a nut 14, partially disposed within the second portion of the bore of the bushing, the nut 14 having an outer surface with a pair of lugs disposed on the outer surface to engage the pair of tangs of the bushing and a pin 8 disposed juxtapositional the slot of the wall surface of the cylindrical support structure and juxtapositional the slot of the bushing.

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Frank Kay Porter, Junior
Elliott Dee Nelson
Daniel Earl Aliment
Terence Jay Lady

JP28004192A

November 19, 2001

October 19, 1992

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Raytheon Company

B64C1/00; F16B5/02; F16B37/00; F16B37/04; F16L21/08; F16L25/06; F42B15/00; F42B15/36; F16B1/00; (IPC1-7): F16B5/02; B64C1/00; F16B37/00; F16B37/04; F42B15/00; F42B15/36

JP221500U
JP4517742B1

Kazuo Shamoto (5 outside)

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