Gallery retainer

Aeronautics and astronautics – Aircraft structure – Details

Patent

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Details

2441181, 292202, B64C 100, B64C 120, E05C 304

Patent

active

06010094&

ABSTRACT:
A gallery retainer is provided having a axial bore through which is fitted a bushing. The bushing has radial slots which interface with a detent mechanism formed in an angular bore drilled through the axial bore wall from a rear face of the retainer. A rotation limiting mechanism is formed near the front face of the retainer in the bore. The retainer provides for maximization of material thickness at the retainer critical load bearing areas while reducing the overall material volume.

REFERENCES:
patent: 5156359 (1992-10-01), Noble et al.
patent: 5741032 (1998-04-01), Chaput
patent: 5887916 (1997-09-01), Finkelstein et al.

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