Aircraft control surface angle measurement device and measurement method thereof

The invention relates to an aircraft control surface angle measurement device and a measurement method thereof. The device comprises a support and a slope measurement instrument arranged on the support, and further comprises a sucker making the slope measurement instrument and the control surface co...

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Bibliographische Detailangaben
Hauptverfasser: WANG WEI, YOU JIONGHUA, LEI HENG, ZHOU HU, QIAN YUSHENG
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The invention relates to an aircraft control surface angle measurement device and a measurement method thereof. The device comprises a support and a slope measurement instrument arranged on the support, and further comprises a sucker making the slope measurement instrument and the control surface cooperate, the upper end of the sucker is provided with a swing arm, the lower end of the sucker is provided with a connector matching with the support, and a cardan shaft enabling the slope measurement instrument to rotate and measure is arranged between the support and the connector. The measurementmethod comprises specific steps of (1) fixing; (2) horizontal state; (3) zero clearing; (4) working angle; and (5) finishing measurement. An electronic slope measurement instrument replaces the original mechanical protractor to measure the deflection angle of the control surface. Through adoption of the aircraft control surface angle measurement device and the measurement method, control surfacedeflection angles are disp