Torso restraint system

Aeronautics and astronautics – Safety lowering devices – Parachutes

Patent

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Details

297484, 280801, B64D 2506

Patent

active

044886918

ABSTRACT:
A harness system is disclosed for releasably restraining the torso of a cman in a seat aboard an aircraft. The harness system includes an upper torso restraint adapted to engage the seat at points on either side thereof and wherein a pair of chest straps connected to either side of a backpad are slidingly routed through respective roller fittings in a criss-cross fashion across the crewman to permit upper torso rotation. A separate lower torso restraint is coupled to the upper torso restraint and adapted to engage the seat at the same points of engagement as the upper torso restraint. A single-action release mechanism, actuated manually or automatically by water immersion, disengages both the upper and lower restraints from the seat thereby divesting the crewman of the harness system.

REFERENCES:
patent: 2655329 (1953-10-01), Martin
patent: 2664610 (1954-01-01), Hannemann
patent: 2868581 (1959-01-01), Minty et al.
patent: 3785597 (1974-01-01), Gaylord
patent: 4028948 (1977-06-01), Frost et al.
patent: 4253628 (1981-03-01), Marek

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