Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Patent
1994-03-25
1995-06-20
Grant, William
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
242379, B64D 2506, A62B 3500
Patent
active
054255171
ABSTRACT:
A strap adjusting device for a harness-adjustment strap having a length, a first end affixed to an aircraft seat-mounted harness and a spaced opposite second end which is free. A wind up device removably affixed to the strap at the second end. The wind up device automatically winds up the strap for a determined length from the second end. The determined length of the strap is thus compacted and restrained from hanging loose. The wind up device includes a housing and a spring in the housing for winding up the strap. A clamp releasably clamps the second end of the strap to the spring.
REFERENCES:
patent: 3319907 (1967-05-01), McAninch et al.
patent: 3421711 (1969-01-01), Brow et al.
patent: 3425646 (1969-02-01), Hollowell
patent: 3465983 (1969-09-01), Taggart
Grant William
Grumman Aerospace Corporation
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