Trouble shooting analysis for the primary flight control system on a large transport category airplane
碩士 === 國立虎尾科技大學 === 飛機工程系航空與電子科技碩士班 === 106 === The aircraft is mainly controlled by the three major flight control surfaces. When the three primary flight control system fail, it has a great influence on the aircraft. After the aircraft lands safely, the ground maintenance personnel can efficiently...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2018
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| Online Access: | http://ndltd.ncl.edu.tw/handle/h6f6qv |
| Summary: | 碩士 === 國立虎尾科技大學 === 飛機工程系航空與電子科技碩士班 === 106 === The aircraft is mainly controlled by the three major flight control surfaces. When the three primary flight control system fail, it has a great influence on the aircraft. After the aircraft lands safely, the ground maintenance personnel can efficiently find out where the problem lies. And it is the focus of this study to properly exclude problems.
This study uses the traditional aircraft MD-11 as a sample to study the diagnosis and elimination of the failure of the main control surface. The MD-11 is an aircraft that uses cable to control the three major primary flight control system and transmits and touches through the cable. The Actuator allows the flight control surface to be manipulated. The structure of the cable and the Actuator are one of the main focuses of this study.
Through the McDonnell Douglas MD-11 Train Manual and the McDonnell Douglas LAMM SCHEMATICS, the mechanical structure and hydraulic system of the MD-11 flight control system were discussed in depth, and the reasons for the failure of the mechanical system and the hydraulic system were sorted out, and the troubleshooting method was summarized. program.
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