An Integrated Model for Performance Optimization of Aerospace Bearings Considering High-Speed Rotations and Temperature Variations

摘要

In this work, a comprehensive analytical model is established to study the performance of the bearings of a helicopter high-speed-input gear shaft. The high-speed shaft, rotating above 15,000 rpm, transmits power to the second stage through a bevel gear that is straddle mounted by a duplex ball bearing and a cylindrical roller bearing. The effects of centrifugal forces, the change of bearing internal clearances due to interference fits, and uneven thermal expansions are studied in the outlined approach. Then the influence of temperature elevations (that may arise due to inadequate cooling) on the performance of high-speed bearings is explored by employing the proposedmodel. This study emphasizes that bearing internal clearances are very critical in assessing the performance of the high-speed system and optimal manufactured bearing clearances are greatly dependent on the operating conditions. Thus, a bearing internal clearance optimization study is carried out considering a broad range of operating temperatures. This optimization study provides "operation condition maps" for high-speed bearings and guides the designer for the optimal selections of bearing clearances by considering different conditions.