Control system for forward wing aircraft

Details Control system for forward wing aircraft Control system for forward wing aircraft

1975-06-16

1976-05-04

Reger, Duane A.

Aeronautics and astronautics

Aircraft control

Automatic

244 45A, 244 83R, 244 90R, B64C 1304

Patent

active

039542319

ABSTRACT:
This invention relates to the arrangement of lifting, stabilizing, and flight controlling, wing surfaces, placed near the front of an aircraft, with main lifting wing surfaces, placed toward the rear. Control surfaces placed rearwardly on the aft fuselage and/or the rear main lifting wing surfaces, are also indicated.

REFERENCES:
patent: 1886932 (1932-11-01), Anderson
patent: 1936786 (1933-11-01), Gebhert
patent: 2082172 (1937-06-01), Mignet
patent: 2363550 (1944-11-01), Reichert
patent: 2430793 (1947-11-01), Wells
patent: 2681776 (1954-06-01), Howard
patent: 2747816 (1956-05-01), Howard
patent: 2773659 (1956-12-01), Feeney
patent: 3155344 (1964-11-01), Vogt
patent: D129548 (1941-09-01), Rocheville
patent: D234079 (1975-01-01), Whitever

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