Cryogenic tank support system
AssigneeThe Boeing Company
InventorsTin A. Luu, Faith O'Brien
Life of this patent
Estimating the term…
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AssigneeThe Boeing Company
InventorsTin A. Luu, Faith O'Brien
Estimating the term…
A cryogenic tank support system and a method for installing a cryogenic tank on an aircraft. The cryogenic tank support system includes an inner ring of a support collar connected to an inner wall of a cryogenic tank. An outer ring of the support collar is connected to an outer wall of the cryogenic tank. The system also includes a saddle of a saddle bracket connected to the outer ring of the support collar. A mount surface of the saddle bracket is connected to a crown region of a fuselage of the aircraft. The system structurally isolates the cryogenic tank from the aircraft by carrying radial loads of the cryogenic tank and axial loads of the cryogenic tank with at least one support collar and carrying the radial loads of the cryogenic tank while allowing axial expansion/contraction of the cryogenic tank with at least one other support collar.
A cryogenic tank support apparatus comprising:
Dependencies are inferred from the claim text.