低损失融合式预旋喷嘴设计与研究

doi:10.13675/j.cnki.tjjs.200214

推进技术 ›› 2020, Vol. 41 ›› Issue (9): 2011-2020.DOI: 10.13675/j.cnki.tjjs.200214

低损失融合式预旋喷嘴设计与研究

唐国庆，薛伟鹏，曾军，赵云

中国航发四川燃气涡轮研究院，四川成都 610500

出版日期:2020-09-15 发布日期:2020-09-15
作者简介:齐　旻，博士生，研究领域为短舱进气道流动与风扇耦合。E-mail：qimin111@foxmail.com
基金资助:
国家科学自然基金（51876176；51906204）；民机专项科研项目。

Design and Study of Low Loss Integrated Pre-swirl Nozzle

AECC Sichuan Gas Turbine Establishment，Chengdu 610500，China

Online:2020-09-15 Published:2020-09-15

摘要/Abstract

摘要： 为减小整个预旋系统的流动损失，首先对带预旋集气腔进气孔、预旋集气腔、预旋喷嘴的冷气预旋流路进行了分析，发现进气孔和集气腔会导致预旋喷嘴进口流场不均匀，相较于进口均匀条件，预旋喷嘴总压损失系数增大0.026。在此基础上提出了一种将预旋集气腔进气孔、预旋集气腔和预旋喷嘴融合设计的低损失融合式预旋喷嘴设计方案，分析表明：融合式预旋喷嘴能有效减小冷气在预旋系统内的流动损失，在设计工况总压损失系数减小0.032，并使冷气在预旋系统内流动更加均匀，提升了预旋系统的整体性能。

关键词: 低损失;预旋;预旋喷嘴;冷气;融合

Abstract: To reduce the flow loss of the pre-swirl system, the pre-swirl system with inlet holes, a collecting chamber and pre-swirl nozzles was analyzed. The results showed that, with the inlet holes and collecting chamber, the inlet flow field of the pre-swirl nozzles showed strong non-uniformity. Compared to uniform inlet flow field, the total pressure loss coefficient increased by 0.026. On this basis, a low loss integrated pre-swirl nozzle design method was proposed. The design results showed that the integrated design of inlet holes, the collecting chamber and the pre-swirl nozzle can reduce the flow loss of the cool air in the pre-swirl system. The total pressure loss coefficient at the design condition decreased by 0.032. And the cool air flowed more evenly in the pre-swirl system, which improved the overall performance of the pre-swirl system.

Key words: Low loss;Pre-swirl;Pre-swirl nozzle;Cool air;Integration

唐国庆，薛伟鹏，曾军，赵云. 低损失融合式预旋喷嘴设计与研究[J]. 推进技术, 2020, 41(9): 2011-2020.

TANG Guo-qing, XUE Wei-peng, ZENG Jun, ZHAO Yun. Design and Study of Low Loss Integrated Pre-swirl Nozzle[J]. Journal of Propulsion Technology, 2020, 41(9): 2011-2020.

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低损失融合式预旋喷嘴设计与研究

Design and Study of Low Loss Integrated Pre-swirl Nozzle

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