Turning angle over-limit alarm device for aircraft traction
The utility model provides a turning angle over-limit alarm device for aircraft traction, which comprises a target component arranged on the outer cylinder wall of a nose landing gear of an aircraft, the target component is an arc-shaped component with the radius equal to that of the outer cylinder...
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| Format: | Patent |
| Sprache: | chi ; eng |
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| Zusammenfassung: | The utility model provides a turning angle over-limit alarm device for aircraft traction, which comprises a target component arranged on the outer cylinder wall of a nose landing gear of an aircraft, the target component is an arc-shaped component with the radius equal to that of the outer cylinder of the nose landing gear of the aircraft, and the maximum turning angle of the aircraft is set by adjusting the radian of the target component. The sensor module is arranged on the wall of a front turning sleeve of the airplane, the output end of the sensor module is connected with the alarm device, the sensor module is used for detecting the relative position state of the sensor module and the target assembly when the airplane turns and outputting an alarm signal to the alarm device when the turning angle of the airplane exceeds the maximum turning angle, and the alarm device is used for achieving turning angle overrun alarm. By means of the simple structural design, the turning angle of the airplane is monitored |
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