航空学报 > 2010, Vol. 31 Issue (3): 459-465

流体力学、飞行力学与发动机

基于壁面压力梯度控制的压气机S形过渡段设计

阙晓斌, 侯安平, 周盛   

  1. 北京航空航天大学 航空发动机气动热力重点实验室
  • 收稿日期:2009-01-16 修回日期:2009-06-18 出版日期:2010-03-25 发布日期:2010-03-25
  • 通讯作者: 阙晓斌

S-shaped Compressor Transition Duct Design Based on Wall Pressure Gradient Control

Que Xiaobin, Hou Anping, Zhou Sheng   

  1. National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics
  • Received:2009-01-16 Revised:2009-06-18 Online:2010-03-25 Published:2010-03-25
  • Contact: Que Xiaobin

摘要: 建立了S形过渡段流道几何的参数化描述方式,并提出了半程落差比的概念,将过渡段流道几何归结为内壁半程落差比及控制点面积比的函数;探讨了通过半程落差比及控制点面积比控制壁面压力梯度的方法;将该方法应用于过渡段的设计,探索其设计规律。研究结果表明:适当增大半程落差比可使过渡段内壁扩压前移,减小后半程的逆压梯度,从而抑制过渡段内壁出口附近低能附面层的分离,减小损失;同时,控制点面积比也将显著改变壁面压力分布,构造先扩张后收缩的面积变化可减小过渡段内壁进口的吸力峰值,并且进一步减小后半程的逆压梯度;对于所研究的进出口面积相等的压气机S形过渡段,当半程落差比在0.55~0.65之间,控制点面积比在1.1附近时,过渡段的总压损失最小。

关键词: 过渡段, S形, 风扇/压气机, 压力梯度, 气动设计

Abstract: A method for the parameterization of an S-shaped transition duct is presented. The midway offset ratio (MWOR), a parameter closely related to the curvature of the duct, is introduced, to enable the duct geometry to be expressed by only two independent parameters: MWOR and control-point area ratio (CPAR) in a selected axial position. Approaches of controlling the wall pressure gradient through MWOR and the area ratio is then investigated respectively. Finally, the method is applied to the design of a compressor transition duct to explore the design principle. The results show that larger values of MWOR tend to move the loading forward, while they decrease the adverse pressure gradient in the rear half of the inner wall where separation is likely to occur, thus reducing the loss. In addition, the area variation in an increase-decrease sequence along the duct, which can be controlled by CPAR, generates a mean pressure gradient counteracting that of the inner wall, and the integral pressure gradient can be further diminished. For the transition duct with equal area at its inlet and outlet, the loss is significantly decreased with the MWOR between 0.55 and 0.65, and CPAR around 1.1.

Key words: transition duct, S-shaped, fan/compressor, pressure gradient, aerodynamic design

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