Aircraft console

Aeronautics and astronautics – Aircraft structure – Details

Patent

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Details

D 3 40, D12155, 220 4B, 224 4242, B64C 700

Patent

active

043961720

ABSTRACT:
An aircraft console provided with a pair of opposed shell housing members which matingly engage to provide an aircraft console outside wall housing. Each of the shell housing members provided with outwardly extending floor-engaging flange portions along the lower perimeter thereof. The floor-engaging flange portions cooperate to form a floor-engaging stabilizing support flange along the bottom perimeter of the assembled aircraft console. A plurality of internal partition panels and compartment floor panels provided which are selectively oriented to form a plurality of compartments within the aircraft console when fixedly positioned intermediate and in fixed engagement with the shell housing members. Transversely oriented connector floor-engaging anchor panels provided transversely across the bottom of the aircraft console so as to matingly engage the stabilizing support flange. A floor-engaging anchor assembly is provided to selectively engage the aircraft cabin floor, the floor-engaging anchor panels and the floor-engaging stabilizing support flange so as to anchor the aircraft console in its operative use position on the floor of the aircraft cabin.

REFERENCES:
patent: D207916 (1967-06-01), White
patent: D237166 (1975-10-01), Jensen
patent: D252540 (1979-08-01), Murphy
patent: D264525 (1982-05-01), Page
patent: 3136461 (1964-06-01), Gregg
patent: 3177033 (1965-04-01), Daniels
patent: 3195272 (1965-07-01), Mosher et al.
patent: 3236404 (1966-02-01), Boscamp
patent: 3561589 (1971-02-01), Larkin et al.
patent: 3670936 (1972-06-01), Pronovost et al.
patent: 4154355 (1979-05-01), Shackelford
patent: 4300709 (1981-11-01), Page

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