| 吸附式风扇/压气机技术的进展与展望 |
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| 引用本文： | 刘波,南向谊,王掩刚,姜键,靳军.吸附式风扇/压气机技术的进展与展望[J].航空动力学报,2007,22(6):945-954. |
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| 作者姓名： | 刘波 南向谊 王掩刚 姜键 靳军 |
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| 作者单位： | 西北工业大学动力与能源学院, 西安 710072 |
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| 摘 要： | 吸附式风扇/压气机是目前国内外高增压比压缩系统的一个重要研究方向.对其产生的背景, 研制的必要性, 技术特点以及研究动向进行了回顾和分析.这一技术的采用能够大幅度提高压比, 减少发动机的轴向长度和重量, 降低风扇的噪音;在做功能力增加重量减轻的同时, 能够增加飞行器的灵活性以及有效载荷, 从而减少燃油消耗.但是这种新型的结构也带来了强度、气弹稳定性等问题, 对此给出了一些分析结果和建议.
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| 关 键 词： | 航空、航天推进系统 吸附式风扇/压气机 附面层 流动控制 压比 效率 |
| 文章编号： | 1000-8055(2007)06-0945-10 |
| 收稿时间： | 2006/5/23 0:00:00 |
| 修稿时间： | 2006年5月23日 |
Development and prospect of aspirated fan/compressor |
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| LIU Bo,NAN Xiang-yi,WANG Yan-gang,JIANG Jian and JIN Jun.Development and prospect of aspirated fan/compressor[J].Journal of Aerospace Power,2007,22(6):945-954. |
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| Authors: | LIU Bo NAN Xiang-yi WANG Yan-gang JIANG Jian and JIN Jun |
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| Institution: | School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China |
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| Abstract: | Aspirated fan/compressor(ASFC) is an integral part of high pressure ratio compression system.So,the background,necessity,technical features and research trend of ASFC were reviewed and analyzed.With ASFC technology,it shall be possible to increase efficiently fan/compressor pressure ratio,but also reduce the axial length and weight of the engine as well as the noise of fans.Meanwhile,it increases the flexibility and payload of the flight vehicle,thus reducing the fuel consumption.However,this new structure also leads to some problems in strength and aeroelasticity,so some analytical results and suggestions are presented. |
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| Keywords: | aerospace propulsion system aspirated fan stage and compressor boundary layer flow control pressure ratio efficiency |
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