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低压涡轮内部流动及其气动设计研究进展 被引量:22
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作者 邹正平 叶建 +3 位作者 刘火星 李维 杨琳 冯涛 《力学进展》 EI CSCD 北大核心 2007年第4期551-562,共12页
随着高空无人飞行器研究的不断升温,高空低雷诺数条件下动力装置的研究越来越受到人们的重视.结合近年来国内外相关领域的研究工作,对低雷诺数低压涡轮内部复杂流动机理的研究进展进行了介绍,包括低雷诺数情况下低压涡轮内部非定常流动... 随着高空无人飞行器研究的不断升温,高空低雷诺数条件下动力装置的研究越来越受到人们的重视.结合近年来国内外相关领域的研究工作,对低雷诺数低压涡轮内部复杂流动机理的研究进展进行了介绍,包括低雷诺数情况下低压涡轮内部非定常流动的特点,叶片边界层分离及转捩现象机理,上游周期性尾迹与下游叶片边界层相互作用机理等.在此基础上给出了适合低雷诺数条件的低压涡轮气动设计方法:尾迹通过与边界层的相互作用,能够抑制分离,进而减小叶型损失,在气动设计中有效引入非定常效应可以大幅度提高低压涡轮的气动负荷或降低气动损失,最终达到提高性能的目的;数值及实验结果验证了这种设计方法的有效性. 展开更多
关键词 低雷诺数 低压涡轮 非定常流动 气动设计
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细长轴加工方法探略 被引量:7
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作者 李家伟 《机械》 2007年第9期63-64,共2页
通过分析各种因素对细长轴加工精度的影响,提出细长轴加工的具体方法,保证细长轴的切削质量。
关键词 细长轴 加工精度 加工方法
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航空发动机主轴承定寿方法的研究
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作者 窦蕴萍 《华北水利水电学院学报》 1997年第3期75-80,共6页
探讨了现有航空发动机主轴承定寿方法存在的各种不足,在此基础上提出了加速寿命试验方法;建立了应用加速寿命试验方法的理论基础;
关键词 寿命试验 航空发动机 主轴承 轴承
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Luster Polish Strengthening Treatment for Raceway Surface of Aeroengine Bearings
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作者 邓四二 滕弘飞 +2 位作者 马付建 郝建军 陈涛 《Journal of Southwest Jiaotong University(English Edition)》 2007年第3期197-202,共6页
A new surface strengthening technology, luster polish strengthening treatment, was proposed to treat the raceway surface of aeroengine bearings (9Cr18Mo) with the centrifugal strengthening machine exclusively design... A new surface strengthening technology, luster polish strengthening treatment, was proposed to treat the raceway surface of aeroengine bearings (9Cr18Mo) with the centrifugal strengthening machine exclusively designed for luster polish strengthening treatment. The experimental results showed that luster polish strengthening treatment produced a compressive residual stress layer with a depth of over 80 μm below the surface of the bearing raceway, and thus effectively removed the metamorphic layer in the raceway surface. After luster polish strengthening treatment, the average surface hardness of the aeroengine bearing raceway was increased from 61.02 HRC to 63.01 HRC, the surface roughness was reduced from 0.06 μm to 0.03 μm, and the contact fatigue life of the aeroengine bearings was improved by about 90%, with the dispersion of fatigue life being reduced remarkably. Theoretical calculation result agrees with that obtained by experiment. 展开更多
关键词 Aircraft engines Rolling bearing Luster polish strengthening Surface treatment Fatigue life
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An Overview of Performance Characteristics, Experiencesand Trends of Aerospace Engine Bearings Technologies 被引量:26
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作者 Ebert Franz-Josef 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2007年第4期378-384,共7页
In this paper, the operating conditions, technical requirements, performance characteristics, design ideas, application experiences and development trends of aerospace engine bearings, including material technology, i... In this paper, the operating conditions, technical requirements, performance characteristics, design ideas, application experiences and development trends of aerospace engine bearings, including material technology, integration design and reliability, are reviewed. The development history of aerospace engine bearing is recalled briefly at first. Then today's material technologies and the high bearing performances of the bearings obtained through the new materials are introduced, which play important roils in the aeroengine bearing developments. The integration design ideas and practices are explained to indicate its significant advantages and importance to the aerospace engine bearings. And the reliability of the shaft-bearing system is pointed out and treated as the key requirement with goals for both engine and bearing. Finally, as it is believed that the correct design comes from practice, the pre-qualification rig testing conducted by FAG Aerospace GmbH & Co. KG is briefly illustrated as an example. All these lead to the development trends of aerospace engine bearings from different aspects. 展开更多
关键词 aerospace engine bearing performance characteristic material technology integrated bearing design reliability system cost
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M168H航空用碳石墨轴承的研制
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作者 邓祖柱 《电碳》 1996年第4期14-15,共2页
本文介绍一种用于飞机油泵轴承的碳石墨材料的研制过程,产品特性及应用 。
关键词 石墨 轴承 性能 航空轴承 飞机
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