Patent · US Active

Stator blade, compressor structure and compressor

US11408440B2 · kind B2 · utility

0Cited by
2References
6Claims
0Family size

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Inventors

Key dates

Filing dateDec 22, 2017
Grant dateAug 9, 2022
Priority date
Expiry dateAug 8, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2250/291
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

The present application provides a stator blade, a compressor structure and a compressor. The stator blade comprises a blade body, wherein a cavity is formed inside the blade body, and a gas supply hole is formed on the blade body. The present application forms a jet on the suction surface of the stator blade by supplemented gas, thereby blowing off the low-speed low-energy region formed by the suction surface, reducing the gas flow mixing loss caused by the supplemented gas, thereby improving the aerodynamic efficiency of the centrifugal compressor.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.