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| 某涡轴发动机整机逼喘试验研究 | |
| 引用本文： | 旷桂兰,姚峥嵘,王道波,吴志勇,彭文雯.某涡轴发动机整机逼喘试验研究[J].航空动力学报,2009,24(3):588-595. |
| 作者姓名： | 旷桂兰 姚峥嵘 王道波 吴志勇 彭文雯 |
| 作者单位： | 1. 南京航空航天大学能源与动力学院,南京,210016;中国航空动力机械研究所株洲,412002 2. 中国航空动力机械研究所株洲,412002 3. 南京航空航天大学自动化学院,南京,210016 |
| 摘 要： | 根据某型涡轴发动机研制的需要,在整机试验台进行了逼喘试验方法的探索,本文详述了发动机逼喘、试验方法设计、试验装置及试验过程,最后对试验结果进行了分析,研究结果表明利用该发动机上的飞机引气口接入高压气源的方法能够成功地进行该型发动机的整机逼喘试验,从而能够真实获得压气机装在整机上工作时的喘振边界线. |
| 关 键 词： | 涡轴发动机 逼喘试验 测试 喘振边界 |
| 收稿时间： | 3/3/2008 12:00:00 AM |
| 修稿时间： | 2008/11/5 0:00:00 |
Surge experimentation research for a whole turbine-shaft engine |
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| KUANG Gui-lan,YAO Zheng-rong,WANG Dao-bo,Wu Zhi-yong and Peng Wen-wen.Surge experimentation research for a whole turbine-shaft engine[J].Journal of Aerospace Power,2009,24(3):588-595. | |
| Authors: | KUANG Gui-lan YAO Zheng-rong WANG Dao-bo Wu Zhi-yong and Peng Wen-wen |
| Institution: | 1.College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Nanjing 210016;China;2.China Aviation Powerplant Research Institute;Zhuzhou 412002;3.College of Automation;China |
| Abstract: | For the requirement of a turbine-shaft engine research,surge experimentation had been done exploringly in a whole engine test-bed.This paper describes engine surge,the design of surge experimentation method,experimentation equipment and the process of the experimentation.In the end,the results of the experimentation have been analysed and summarized,the results make clear that the experimentation method is valid,connecting high pressure air to the engine bleeds can do the engine surge experimentation succes... |
| Keywords: | turbine-shaft engine surge experimentation test surge margin |
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