Arm restraint

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

B64D 25115

Patent

active

054153662

ABSTRACT:
An arm restraint system for an ejection seat of an aircraft. The arm restraint system includes a pair of shrouds that are attached to the seat and each contain an outer channel. Extending through each outer channel is a corresponding strap that is coupled to the cockpit and fastened to a ring on the belt of the pilot. When the seat is ejected, the straps are pulled and the shrouds are deployed onto the arms of the pilot. The shrouds extend to a position which captures the wrists of the pilot, thereby preventing both sideward and upward movement of the arms.

REFERENCES:
patent: 2836382 (1960-05-01), Martin
patent: 3083938 (1963-04-01), Brinkworth et al.
patent: 3202384 (1965-08-01), Martin
patent: 4081156 (1978-03-01), Ideskar
patent: 4179086 (1979-12-01), Yamada
patent: 4215835 (1980-08-01), Wedgwood
patent: 4359200 (1982-11-01), Brevard et al.
patent: 4482112 (1984-11-01), Cummings
patent: 4592523 (1986-06-01), Herndon
patent: 4667902 (1987-05-01), Zenobi
patent: 4676462 (1987-06-01), Martin
H 115, Lorch, Published Aug. 5, 1986 (U.S. Statutory Invention Registration).

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