Cowl structure alignment and shear device

Aeronautics and astronautics – Aircraft power plants

Patent

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Details

244 54, 2441294, 292113, B64D 2906

Patent

active

043657753

ABSTRACT:
An improved latch for aligning and securing together a pair of hinged cowlings surrounding an aircraft engine. The latch not only holds the cowlings together during thrust and reverse thrust loads, but also absorbs shear loads placed thereon by the aircraft.

REFERENCES:
patent: 2695803 (1954-11-01), Summers
patent: 2712955 (1955-07-01), Andrews
patent: 2894777 (1959-07-01), Hogan
patent: 3541794 (1970-11-01), Johnston et al.
patent: 4127305 (1978-11-01), Nielsen

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