Receptacles – Flaccid wall material permanently united with a skeletal...
Patent
1975-03-17
1976-09-07
Price, William
Receptacles
Flaccid wall material permanently united with a skeletal...
220 4R, 220 22, 244135R, 206521, 220 5A, B65D 2504, B65D 8100, B65D 8570, B65D 8724
Patent
active
039790053
ABSTRACT:
A cryogenic fuel tank of a cylindrical design having toroidal surface ends, is suspended in aircraft structure through a central front mount member; and the rear tank is supported by rod elements which extend from a mounting ring about the tank, to mount points rearwardly within the interior of the fuselage. The central front mount member has baffles attached thereto, so as to prevent undue sloshing of the liquid within the tank. The front end of the tank suspension absorbs radial and axial loads, but no bending moments; and the aft linkage suspension arrangement takes primarily radical and torsional loads. Also the aft suspension provides for unrestrained axial and radial contraction and expansion of the outer shell of the tank.
REFERENCES:
patent: 2379126 (1945-06-01), Welden
patent: 3078004 (1963-02-01), Randolph
patent: 3110318 (1963-11-01), Edlitz
patent: 3157147 (1964-11-01), Ludwig
patent: 3321159 (1967-05-01), Jackson
Robinson Robert K.
Whitener Philip C.
Donahue Bernard A.
Hartmann H. Gus
Moy Joseph M.
Price William
The Boeing Company
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