Longitudinal flying wing aircraft

Details Longitudinal flying wing aircraft Longitudinal flying wing aircraft

2011-02-21

2011-11-15

Michener, Joshua (Department: 3644)

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

C244S055000, C244S04500R

Reexamination Certificate

active

08056852

ABSTRACT:
The Longitudinal Flying Wing aircraft idea provides for design of large cargo and passenger aircraft in range from low to high subsonic and transonic speed. Such aircraft would have up to twice lower fuel consumption per unit of payload, higher lift capacity, and a significantly longer range, while having a significantly lower level of noise inside passenger cabin and cockpit relative to classical concept aircraft. This idea is further providing for efficient, reliable, and simple flight controls, hence it may be successfully applied for design of all-size, long range, high-lift-capacity unmanned aircraft throughout the entire range of subsonic speeds.

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“Model1” French Journal: Gazette-Air & Cosmos No. 1386, Jul. 1992, p. 4 (see attachment—non-black and white drawings).
“Model2” French Journal: Gazette-Air & Cosmos No. 1386, Jul. 1992, p. 4 (see attachment—non-black and white drawings).

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