Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Patent
1978-02-16
1982-01-12
Barefoot, Galen L.
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
244123, 244132, B64C 106, B64C 112
Patent
active
043101321
ABSTRACT:
A fuselage structure is disclosed in which the skin is comprised of layers of a matrix fiber reinforced composite, with the stringers reinforced with the same composite material. The high strength to weight ratio of the composite, particularly at elevated temperatures, and its high modulus of elasticity, makes it desirable for use in airplane structures.
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Webb et al., "Retort Braze Bonding of Borsic Al. Comp. Sheet to ti". Jun. 1975, NASA-CR-132730.
Bonn, "Joining of Fiber Reinforced Al. by Diffusion Bonding", 1975, Avail. NTIS, DOKZENTBw DM30.00
Frosch Robert A. Administrator of the National Aeronautics and Space
Robinson Robert K.
Tomlinson Harry M.
Barefoot Galen L.
Manning John R.
Osborn Howard J.
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