Helicopter Throttle Micro Switch Development Of Testing Equipment

• Main Authors: YIN,CHIEN-HSING, 殷建興
• Other Authors: WANG,YU-CHENG
• Format: Others
• Language: zh-TW
• Published: 2016
• Online Access: http://ndltd.ncl.edu.tw/handle/37021141321561258291

碩士 === 中華科技大學 === 飛機系統工程研究所在職專班 === 104 === The throttle of power control of helicopter has been playing a decisive role in the history of aviation development. If the warning light of power control system illuminate during both engines running on ground, the crewmenbers must abort the flight mission for fault. If some specific maintenance or test can be done at right time for the faulty component of throttle power control system, for example, adjustment or replacement, we can efficiently eliminate the malfunction and save time for the maintenance action. This study is based on the research of disposition of micro switch in helicopter, and done by ergonomics. First, to get critical factors by increasing incorrect measure point, distorted pins of plug, and human being errors. The research shows that measurement by using test set is more efficient, saving man power and time, and the results of test set has greatly eliminated in correction of measurement comparable to human beings. The result of manufactured external electrical testing box used in this research can be a critical reference in all power quadrants test for military and civilian helicopters. Thus we can sharply increase efficiency for maintenance and minimize any potential problem, such as bending pin. Aslo, this study of throttle cost percentage, to reduce 50% man-hours and human resource management and to save budget $245,900.