首页> 外文会议>International Symposium on Stability Control of Rotating Machinery(ISCORMA-3); 20050919-23; Cleveland,OH(US) >NONLINEAR WHIRL RESPONSE OF A HIGH-SPEED SEAL TEST ROTOR WITH MARGINAL AND EXTENDED SQUEEZE-FILM DAMPERS
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NONLINEAR WHIRL RESPONSE OF A HIGH-SPEED SEAL TEST ROTOR WITH MARGINAL AND EXTENDED SQUEEZE-FILM DAMPERS

机译:具有边际挤压和扩展膜阻尼的高速密封测试转子的非线性涡旋响应

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Synchronous and nonsynchronous whirl response analysis of a double overhung, high-speed seal test rotor with ball bearings supported in 5.84- and 12.7-mm-long, un-centered squeeze-film oil dampers is presented. Test performance with the original damper of length 5.84 mm was marginal, with nonsynchronous whirling at the overhung seal test disk and high amplitude synchronous response above 32,000 rpm near the drive spline section occurring. A system critical speed analysis of the drive system and the high-speed seal test rotor indicated that the first two critical speeds are associated with the seal test rotor. Nonlinear synchronous unbalance and time transient whirl studies were conducted on the seal test rotor with the original and extended damper lengths. With the original damper design, the nonlinear synchronous response showed that unbalance could cause damper lockup at 33,000 rpm. Alford cross-coupling forces were also included at the overhung seal test disk for the whirl analysis. Sub-synchronous whirling at the seal test disk was observed in the nonlinear time transient analysis. With the extended damper length of 12.7 mm, the sub-synchronous motion was eliminated and the rotor unbalance response was acceptable to 45,000 rpm with moderate rotor unbalance. However, with high rotor unbalance, damper lockup could still occur at 33,000 rpm, even with the extended squeeze-film dampers. Therefore, the test rotor must be reasonably balanced in order for the un-centered dampers to be effective.
机译:提出了双悬垂的高速密封测试转子的同步和非同步涡流响应分析,该转子的球轴承支撑在5.84和12.7毫米长的无心挤压膜油阻尼器中。原始阻尼器的长度为5.84毫米,测试性能微不足道,悬臂密封测试盘上出现了非同步涡动,并且在驱动花键部分附近出现了高于32,000 rpm的高振幅同步响应。对驱动系统和高速密封测试转子的系统临界速度分析表明,前两个临界速度与密封测试转子相关。在具有原始和扩展阻尼器长度的密封测试转子上进行了非线性同步不平衡和时间瞬态涡旋研究。对于原始的风门设计,非线性同步响应表明不平衡会导致风门在33,000 rpm时锁死。悬空密封测试盘上还包括Alford交叉耦合力,用于旋转分析。在非线性时间瞬态分析中,在密封测试盘处观察到次同步回旋。随着减震器长度的延长(12.7毫米),亚同步运动得以消除,转子不平衡响应在中等转子不平衡的情况下达到45,000 rpm是可接受的。但是,在转子不平衡度较高的情况下,即使使用扩展的挤压膜减震器,减震器仍会以33,000 rpm的转速发生锁定。因此,测试转子必须合理地平衡,以使不居中的阻尼器有效。

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