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A New Computational Method of the Friction Power Loss of Spiral Bevel Gears of a Helicopter Reducer

机译:直升机减速机螺旋锥齿轮摩擦功率损失的一种新计算方法

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The objective of this paper is to develop a new computational method of friction power loss of the spiral bevel gears transmission system of the helicopter tail reducer. At first, the velocity and force of the meshing point were analyzed during meshing process. Then a computational model of friction power loss for spiral bevel gear was established based on the principle of meshing and tribology theory, considering the effects of actual contact ratio and time-variant factors. This model considered the effects of actual contact ratio and time-variant factors including mesh point relative sliding velocity of mesh point, normal load, friction coefficient, etc.
机译:本文的目的是开发一种新的直升机机尾减速器螺旋锥齿轮传动系统摩擦功率损耗的计算方法。首先,在啮合过程中分析了啮合点的速度和力。然后,根据啮合原理和摩擦学原理,考虑实际接触比和时变因素的影响,建立了螺旋锥齿轮摩擦功率损失的计算模型。该模型考虑了实际接触比和时变因素的影响,包括网点相对于网点的相对滑动速度,法向载荷,摩擦系数等。

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