Invention Application
- Patent Title: Control system for an aircraft
- Patent Title (中): 飞机控制系统
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Application No.: US10993497Application Date: 2004-11-19
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Publication No.: US20060108472A1Publication Date: 2006-05-25
- Inventor: Walter Clark
- Applicant: Walter Clark
- Main IPC: B64C9/00
- IPC: B64C9/00

Abstract:
The invention is a system for controlling an aircraft, the aircraft having a longitudinal axis, vertical and horizontal axis and right and left wings and right and left ailerons mounted on the right and left wings. In detail, the system includes a right stabilizer mounted to the right wing, the right stabilizer canted from the right wing such that the outer end thereof is down and deflectable about an axis of rotation parallel to the span axis of the stabilizer. A left stabilizer is mounted to the left wing, the left stabilizer canted from the left wing such that the outer end thereof is down and deflectable about an axis of rotation parallel to the span axis of the stabilizer. A control system is provided to simultaneously deflect the right aileron and stabilizer downward and the left aileron and stabilizer upward to turn left and to deflect the right aileron and stabilizer upward and the left aileron and stabilizer downward to turn right.
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