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针对航空活塞式发动机功率损失可能造成的事故危害,拟从低温环境下起飞影响、汽化器加温或进气加温影响、高温高原机场影响、空气湿度影响、点火系统影响、发动机进气系统泄漏和气缸活塞组不密封等七个主要影响因子分别进行原因分析,并给出应对方法和参考性建议。
In view of the potential damage caused by the power loss of the aircraft piston engine, the proposed take-off from low temperature environment, the heating or warming of the carburetor, the airport impact of the high-temperature plateau, the influence of air humidity, the influence of the ignition system, the leakage of the engine intake system and Cylinder piston group is not sealed and other seven major influencing factors were analyzed, and give coping methods and reference suggestions.