Effects of Speed of Controllable Speed Casing on Flow Stability for Transonic Compressor Rotor

被引:0
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作者
Zhong J.-J. [1 ]
Zhao J.-Y. [1 ]
Wu W.-Y. [1 ]
机构
[1] Merchant Marine College, Shanghai Maritime University, Shanghai
来源
关键词
Controllable speed casing; Numerical research; Stable operating margin; Tip leakage vortex; Transonic compressor rotor;
D O I
10.13675/j.cnki.tjjs.210218
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学科分类号
摘要
Controllable speed casing is a kind of casing treatment method by controlling the rotation of the rotatable ring in casing structure to exert an effect on the tip clearance flow field. It can improve the problem of efficiency reduction and poor adaptability under off-design conditions in casing treatment to a certain extent. A numerical study was carried out on the flow stability of a rotatable ring which started from tip leading edge and had a width of the whole axial chord length of the blade tip at the design speed of a transonic compressor rotor. The results show that the increase of rotatable ring speed can continuously raise the stable operating margin of the rotor. The effect of stability expansion is poor first and then significant. When rotatable ring rotates at the design rotor speed,the stable operating margin is improved by 52.56% under the condition that the maximum efficiency is almost constant. It is found that,at low speed,the stability expansion is mainly achieved by reducing the tip blockage area while,at high speed,the instability is delayed by controlling the breakdown of tip leakage vortex. The stable operating margin is improved to different degrees at various speeds. © 2022 Journal of Propulsion Technology. All rights reserved.
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共 25 条
  • [1] Hoffman W H,, Ballman J., Some Aspects of Tip Vortex Behavior in a Transonic Turbocompressor
  • [2] Yamada K, Funazaki K,, Furukawa M., The Behavior of Tip Clearance Flow at Near-Stall Condition in a Transonic Axial Compressor Rotor [R]
  • [3] 27, 2, pp. 425-430, (2012)
  • [4] Bailey E E., Effect of Grooved Casing Treatment on the Flow Range Capability of a Single-Stage Axial-Flow Compressor
  • [5] Muller M W, Schiffer H P,, Hah C., Effect of Circumferential Grooves on the Aerodynamic Performance of an Axial Single-Stage Transonic Compressor
  • [6] Muller M W, Schiffer H P,, Et al., Interaction of Rotor and Casing Treatment Flow in an Axial Single-Stage Transonic Compressor with Circumferential Grooves [R]
  • [7] Lu X, Et al., Mechanism of the Interaction Between Casing Treatment and Tip Leakage Flow in a Subsonic Axial Compressor
  • [8] Houghton T,, Day I., Enhancing the Stability of Subsonic Compressors Using Casing Grooves[J], Journal of Turbomachinery, 133, 2, (2011)
  • [9] Sakuma Y, Et al., Numerical Analysis of Flow in a Transonic Compressor with a Single Circumferential Casing Groove:Application to Two Different Compressor Rotors
  • [10] Kau H P., A Numerical Investigation of the Flow Mechanisms in a High Pressure Compressor front Stage with Axial Slots[J], Journal of Turbomachinery, 126, 3, pp. 339-349, (2004)