Compressor and turbomachine with optimized efficiency
A turbine engine and compressor technology, applied in the field of axial flow compressors, can solve the problems of reduced pumping margin, small improvement, and no improvement in pumping margin, so as to achieve good pumping margin and good interaction effect, good efficiency
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[0047] figure 1 The axial compressor of the turbine engine 10 is shown. The compressor has a casing 12 in which a rotor impeller 14 is installed. The rotor impeller 14 itself includes a rotor disk 16 to which the radial blades 18 are fixed in an axisymmetric structure in a known manner. The rotor impeller is arranged to be able to rotate around the rotation axis A in the case 12.
[0048] The box 12 has a generally shaped inner wall 20 that defines an aerodynamic reference surface 22 (see image 3 ), the aerodynamic reference surface defines the passage through which gas can pass. The aerodynamic reference surface is a rotating surface, usually in a substantially conical shape, in this example cylindrical.
[0049] Reference image 3 The arrangement of the vanes 18 and the inner wall 20 for reducing the clearance vortex of the compressor of the present invention will be described.
[0050] Such as image 3 As shown, each blade has a leading edge 26, a trailing edge 28, and a radia...
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