Application of Contra-Rotating Turbine without Guide Vanes to High Thrust Loading Aeroengine

LIU Si-yong; WANG Ping; FANG Xiang-jun; YAN Shan-ping

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Application of Contra-Rotating Turbine without Guide Vanes to High Thrust Loading Aeroengine

更新时间：2026-07-07

- Application of Contra-Rotating Turbine without Guide Vanes to High Thrust Loading Aeroengine
- Vol. 17, Issue 4, (2002)
- 作者机构：
  
  北京航空航天大学动力系,北京,100083
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2002
- 稿件说明：
移动端阅览
LIU Si-yong, WANG Ping, FANG Xiang-jun, et al. Application of Contra-Rotating Turbine without Guide Vanes to High Thrust Loading Aeroengine[J]. 2002, 17(4).
DOI：

LIU Si-yong, WANG Ping, FANG Xiang-jun, et al. Application of Contra-Rotating Turbine without Guide Vanes to High Thrust Loading Aeroengine[J]. 2002, 17(4). DOI：

摘要

由于当代新的歼击机发展的需要

推重比 1 0以上的涡扇发动机的研制势在必行

而对于涡轮部件

采用超跨音、大负荷、低稠度、无导叶、大转折角的对转涡轮方案是一个重大的技术措施。它将大幅度减轻发动机重量

提高推动比。文中对此论述了它的主要优点

以及由此带来涡轮气动设计、计算方面的新问题和新概念。我们设计并制造出了试验件

并与 6 0 8所合作在北航建立了对转涡轮试验台。

Abstract

To meet the needs for developing contemporary new fighter

it is imperative to develop fan turbo-engine with thrust loading exceeding ten.Adopting contra-rotating turbine characterized by transonic-supersonic profiles

large load

low blade density

without guide vanes and high deflection angle is an important measure.It would greatly reduce the weight of engine and raise the thrust loading.This paper reviews its primary advantages and new requirements for aerodynamics design and computing.A contra-rotating turbine test rig has been constructed in cooperation with 608 Research Institute of China Aviation Industry.

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Related Author

LU Cong-ming

YAN Shan-ping

BAI Shu-sheng

ZHANG Wei

WU Dong

LI Guang-chao

ZHOU Yan-wei

MA Fu-jian

Related Institution

Research Institute of China Aviation Industry

Liaoning Key Laboratory of Digital Technology Simulation and Test Technique, College of Power and Energy Engineering, Shenyang Aerospace University

School of Mechatronics Engineering, Henan University of Science and Technology

School of Mechanical Engineering, Da1ian University of Technology

th Dept., Beijing University of Aeronautics and Astronautics

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