Aircraft

Details Aircraft Aircraft

2005-11-29

2005-11-29

Eldred, J. Woodrow (Department: 3644)

Aeronautics and astronautics

Aircraft, heavier-than-air

Airplane sustained

C244S04500R, C244S11700R

Reexamination Certificate

active

06969026

ABSTRACT:
The aircraft has a main body1and a pair of sub bodies4and5positioned substantially in parallel with the main body1and respectively in both of the left and right sides of the main body1. A canard3and main wings8and9each have a central portion fixed to the main body1and portions fixed respectively to the sub bodies4and5, near left and right ends of the wings. Engines6and7are respectively mounted on outer surfaces of the sub bodies4and5. The sub bodies4and5are thinner than the main body1. The canard3, which is positioned closest to the fore end of the aircraft, has a shorter wing span than the other wings. The sub bodies4and5contain fuel. The fuel is supplied to the engines6and7assuring high safety. The main wings8and9are positioned, shifted respectively forth and back relative to the main body1. Therefore, stability is not impaired even if cargos are loaded into the main body over a wide range from the bow to the tail.

REFERENCES:
patent: D120187 (1940-04-01), Silverstein
patent: 2406625 (1946-08-01), Oglesby
patent: 2460804 (1949-02-01), Brentnall
patent: 5071088 (1991-12-01), Betts
patent: 5145129 (1992-09-01), Gebhard
patent: 6367738 (2002-04-01), Wadleigh

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