Flight controls with automatic balance

Details Flight controls with automatic balance Flight controls with automatic balance

1998-07-02

2000-08-29

Swiatek, Robert P.

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

B64C 350

Patent

active

061095672

ABSTRACT:
Flight controls with automatic balance for use in control of the movement of an aircraft through a fluid system, the control system consists of ailerons divided into two parts, which at low speed adopt the shape of a conventional aileron and rotate in their entirety with the same degree and at high speeds, a part of it rotates or extends to a determinated angle by means of the actuator and the other part of the aileron, that is hinged or articulated to the main part of the aileron, rotates with reference to the main part as a function of the air speed pressure, opposing to this rotation by means of one or more springs.

REFERENCES:
patent: 3987984 (1976-10-01), Fischer
patent: 3994452 (1976-11-01), Cole
patent: 4053124 (1977-10-01), Cole
patent: 5115996 (1992-05-01), Moller
patent: 5794893 (1998-08-01), Diller et al.

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