航空绞车的反求设计技术及验证 |
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引用本文: | 李红泉,张力,韩方军.航空绞车的反求设计技术及验证[J].航空发动机,2008,34(4):16-18. |
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作者姓名: | 李红泉 张力 韩方军 |
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作者单位: | 1. 解放军92419部队,辽宁兴城,125106 2. 沈阳发动机设计研究所,沈阳,110015 |
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摘 要: | 在无任何原始资料的情况下,为生产一体化程度较高、结构相对复杂的航空绞车系统,并改进不合理结构,完善某些功能,而采用了反求设计技术.介绍了反求设计技术的原理、航空绞车结构和制造流程、性能改进方法和各种性能验证试验.
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关 键 词: | 航空绞车 反求设计技术 试验验证 |
Inverse Design Technology and Validation of Aeroengine Winch |
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Authors: | LI Hong-quan ZHANG Li HAN Fang-jun |
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Institution: | LI Hong-quan1,ZHANG Li2,HAN Fang-jun2(1.PLA Unit No.92419,Xingcheng125106,Liaoning,China,2.Shenyang Aeroengine Research Institute,Shenyang110015,China) |
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Abstract: | The inverse design technology was used form ore integrated and complicated aeroengine winch system without any raw materials,which could improve the unreasonable structure and function.The principle of inverse design technol-ogy,aeroengine winch structure,manufacturing process,m ethod ofperformance improvem ent and various performance verification tests were presented. |
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Keywords: | aeroengine winch inverse design technology verification test |
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