Aircraft empennage with fixed trailing edge horizontal stabilize

Details Aircraft empennage with fixed trailing edge horizontal stabilize Aircraft empennage with fixed trailing edge horizontal stabilize

1986-10-14

1988-12-13

Barefoot, Galen L.

Aeronautics and astronautics

Aircraft control

Rudders and empennage

244214, 244 48, B64C 502

Patent

active

047904941

ABSTRACT:
An aircraft empennage has a vertical stabilizer, a trailing edge fixed horizontal stabilizer rigidly attached to the aircraft and a movable leading edge elevator affixed to the aircraft. The elevator is movable through a high position and a low position relative to the horizontal stabilizer, thereby providing variable camber and incidence deflection and optimizing deflections while providing adequate power for all flight conditions.

REFERENCES:
patent: D189328 (1960-11-01), Thieblot
patent: 1451352 (1923-04-01), Voracek
patent: 1533323 (1925-04-01), McCauley
patent: 1652618 (1927-12-01), Fairey
patent: 1691376 (1928-11-01), Brimm, Jr.
patent: 1732873 (1929-10-01), Yock
patent: 1873662 (1932-08-01), O'Malley
patent: 2430793 (1947-11-01), Wells
patent: 2563757 (1951-08-01), Thorp
patent: 2953322 (1960-09-01), Lewis
patent: 3417946 (1968-12-01), Hartley
patent: 3756529 (1973-09-01), Backlund et al.
patent: 4034939 (1986-07-01), Ridley, Jr. et al.

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