| 直11MB1型机燃油系统热油飞行试验研究 |
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| 引用本文： | 叶宁武,胡招才,黄昆,赵亚峰.直11MB1型机燃油系统热油飞行试验研究[J].直升机技术,2009(3). |
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| 作者姓名： | 叶宁武 胡招才 黄昆 赵亚峰 |
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| 作者单位： | 中国直升机设计研究所,景德镇,333001 |
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| 摘 要： | 直11MB1型机热油飞行试验是风险试飞科目,在国内直升机上首次进行。针对适航条款CCAR27.961(燃油系统在热气候条件下的工作)的要求,本文提出了试验的关键及其解决方法,确定了飞行试验的内容,对试验结果进行了分析。
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| 关 键 词： | 燃油系统 热油飞行试验 |
The Research of Hot Fuel Flow Test for Z11MB1 Helicopter |
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| Authors: | YE Ningwu HU Zhaocai HUANG Kun ZHAO Yafeng |
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| Institution: | YE Ningwu; HU Zhaocai; HUANG Kun; ZHAO Yafeng(China Helicopter Research and Development Institute; Jingdezhen; 333001); |
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| Abstract: | The hot fuel flow flight test of Z11MB1 helicopter is first carried out in our country.This test is the risk subject of helicopter flight test.According to require of CCAR27.961(fuel system work in the hot climate),the paper introduces content and means of the flight test,analyzes result of the test. |
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| Keywords: | fuel system hot fuel flow flight test |
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