| 涡轴型发动机冷却通风系统参数在机动试飞中的变化规律与分析 |
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| 引用本文： | 王婕.涡轴型发动机冷却通风系统参数在机动试飞中的变化规律与分析[J].工程与试验,2012,52(2):28-32. |
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| 作者姓名： | 王婕 |
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| 作者单位： | 中国飞行试验研究院,陕西西安,710089 |
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| 摘 要： | 涡轴型发动机是直升机的主要动力,而直升机具有机动能力强、灵活的特点。本文以某型涡轴发动机配装某型直升机为研究对象,在高温条件下,对各种机动动作进行了全面的考核,通过对试验数据的总结,归纳、分析了冷却通风系统参数在机动飞行中的变化规律。
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| 关 键 词： | 涡轴型发动机 冷却通风系统 机动飞行 |
Change Law and Analysis of Cooling System Parameters for Turbo-shaft Engine in Maneuver Flight |
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| Wang Jie.Change Law and Analysis of Cooling System Parameters for Turbo-shaft Engine in Maneuver Flight[J].ENGINEERING & TEST,2012,52(2):28-32. |
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| Authors: | Wang Jie |
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| Affiliation: | Wang Jie(Chinese Flight Test Establishment,Xi ＇ an710089,Shanxi,China) |
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| Abstract: | The turbo-shaft engine provides power for helicopter,and the helicopter has the characteristic of flexibility and agility.Turbo-shaft engine installed on a helicopter is studied in this paper.The different kinds of maneuver flight are demonstrated fully on hot days,the test data are analyzed,and the change laws of the cooling system parameters in the maneuver flight are summarized. |
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| Keywords: | turbo-shaft engine cooling system maneuver flight |
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