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Simplified aircraft control system

阅读:587发布:2022-02-28

专利汇可以提供Simplified aircraft control system专利检索,专利查询,专利分析的服务。并且A control system resiliently interconnects aileron and rudder controls. When the aileron is controlled, the rudder is trimmed sufficiently to maintain a desired bank and turn orientation without separately controlling the rudder. For stall minimization the elevator is restricted from moving up to the position where the angle of attack of the air foil is at the burble point.,下面是Simplified aircraft control system专利的具体信息内容。

1. An airplane control system comprising a plurality of movable control surfaces including aileron, rudder, and elevator surfaces, means for selectively exerting a pulling force upon said airplane along a flight path, and elevator control means independent of the stabilizer of the airplane for selectively positioning the elevator surfaces to control the angle of attack of the wing of the airplane, said elevator control means including mechanical limiting means for mechanically limiting the movement of said elevator surfaces to preclude raising the angle of the attack of the wing of said airplane to the burble point while still enabling sufficient angle of attack to safely maneuver.
1. An airplane control system comprising a plurality of movable control surfaces including aileron, rudder, and elevator surfaces, means for selectively exerting a pulling force upon said airplane along a flight path, and elevator control means independent of the stabilizer of the airplane for selectively positioning the elevator surfaces to control the angle of attack of the wing of the airplane, said elevator control means including mechanical limiting means for mechanically limiting the movement of said elevator surfaces to preclude raising the angle of the attack of the wing of said airplane to the burble point while still enabling sufficient angle of attack to safely maneuver.
2. The control system of claim 1 wherein said elevator control means comprises a control yoke, and wherein said elevator limiting means comprises a stop for limiting the movement of said control yoke.
3. An airplane control system comprising a plurality of movable control surfaces including aileron, rudder, and elevator surfaces, means for selectively exerting a pulling force upon said airplane along a flight path, elevator control means independent of the stabilizer of the airplane for selectively positioning the elevator surfaces that control the angle of attack of the wing of the airplane, said elevator control means including limiting means for limiting the movement of said elevator surfaces to preclude raising the angle of attack of the wing of said airplane to the burble point while still enabling sufficient angle of attack to safely maneuver, a plurality of control cables for separately controlling said aileron and rudder surfaces, and means for resiliently interconnecting said control cables so that a pull upon an aileron simultaneously pulls said rudder with a yielding force.
4. The control system of claim 3 wherein said means for interconnecting said control cables comprises coiled springs.
5. The control system of claim 3 and means for manually overriding said yielding force.
6. An airplane control system comprising aileron and rudder movement control devices resiliently interconnected to move said rudder by a predetermined amount responsive to movement of said ailerons, and means for manually overriding the movement of said rudder responsive to the movement of said ailerons.
7. An airplane control system comprising aileron and rudder control devices resiliently interconnected to move said rudder by a predetermined amount responsive to movement of said aileron, and means for precluding the stalling of said airplane.
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