Gas compressor stationary blade cascade with equal-width linear groove formed in blade root
A technology for compressors and sub-leaf cascades, which is applied in passive flow control, a flow control scheme for the blade root of a compressor stator cascade, and the flow control field of a compressor stator cascade, which can solve the slotting scheme to connect the arcs randomly and control the The solution is difficult to optimize the design, lack of design guidelines and other problems, to achieve the effect of convenient optimization design, good engineering application prospects, and easy processing
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[0024] The specific embodiments of the present invention will be described below with reference to the accompanying drawings.
[0025] like figure 1 As shown, the compressor stator cascade with equal-width linear grooves at the blade root is provided with equal-width linear grooves 5 at the root end wall 2 of the blade cascade 1 from the pressure surface 3 to the suction surface 4 of the blade cascade 1 .
[0026] like figure 2 As shown, according to the flow field of the PVD prototype stator cascade, the position of the outlet of the channel 5 on the suction surface 4 is selected before the separation point; along the axial direction of the cascade, the position of the inlet of the channel 5 on the pressure surface 3 is located on the suction surface 4 Upstream of the outlet position; according to the surface pressure distribution of the PVD prototype stator cascade, the inlet position of the channel 5 on the pressure surface 3 is selected at the position where the static p...
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