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The Application of Advanced Composite Material in Tail Driver Shaft of the Helicopter

机译:先进复合材料在直升机尾部驱动轴中的应用

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The helicopter tail drive shafts are designed by using aluminum alloy conventionally. The composite materials have the advantages of high strength ratio, good fatigue and erosion resistance. It can reduce weight 10%~30% than metal, and improve the pneumatic elasticity characteristics and flight performances of helicopter. This cannot be realized by using other materials. The design of the tail driver shaft has used composite material, so the advantages of light weight, good dynamic performances, high reliability, long life, excellent survivability can be achieved, and critical speed are increased. Torsional vibration problem of helicopter is also solved.
机译:直升机尾部驱动轴是通过常规使用铝合金设计的。复合材料具有高强度比,疲劳和耐腐蚀性高的优点。它可以减轻比金属10%〜30%,提高直升机的气动弹性特性和飞行性能。这不能使用其他材料来实现。尾部驱动轴的设计使用复合材料,因此重量轻,动态性能良好,高可靠性,长寿命,可以实现优异的生存能力,并且临界速度增加。直升机的扭转振动问题也得到解决。

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