Aircraft with reduced wing structure loading

Details Aircraft with reduced wing structure loading Aircraft with reduced wing structure loading

1999-04-28

2000-05-16

Nguyen, Tan

Data processing: vehicles, navigation, and relative location

Vehicle control, guidance, operation, or indication

Aeronautical vehicle

701120, 244117R, 244 75R, 244 7A, 244 7C, 244 8, 244 11, 244 28, 244 72, 702144, 73 178, 258 12, 89 3719, 172700, 364130, B64C 1316

Patent

active

060649232

ABSTRACT:
An aircraft having a reduced-load wing structure is provided with a controllable canard stabilizer (5G, 5D) at the front end of the aircraft and a controller that controls the canard stabilizer. The controller generates a turn command corresponding to an increase in the lift of the canard stabilizer when, simultaneously, the turn command applied by the pilot to the elevational control surfaces (6G, 6D) exceeds a threshold and the measurement of the vertical acceleration of the aircraft exceeds a threshold.

REFERENCES:
patent: 4697768 (1987-10-01), Klein
patent: 5056027 (1991-10-01), Kahler
patent: 5079711 (1992-01-01), Lambregts et al.
patent: 5186416 (1993-02-01), Fabre et al.
patent: 5722615 (1998-03-01), Bilange et al.

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