Supersonic radial-inward-flow turbine
A supersonic and turbine technology, applied to steam engine devices, stators, engine components, etc., can solve the problems of increasing expansion ratio and higher and higher requirements for inlet pressure, and achieve the effect of occupying less space and increasing the amount of work done
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[0034] See Figure 1 to Figure 3 A supersonic centripetal turbine provided by this embodiment includes:
[0035] The centripetal impeller 2, the annular shell 1 and a plurality of Rafar nozzles 5, the annular shell 1 surrounds the centripetal impeller 2, and the outer wall of the annular shell 1 is evenly distributed with a plurality of The gas inlet 4 for the gas to enter, the Rafar nozzle 5 is arranged in the annular shell 1, and the inlet end 54 of the Rafar nozzle 5 is communicated with the gas inlet 4, and the outlet of the Rafar nozzle 5 The end 55 faces the center of the centripetal impeller 2, and the air flow enters the centripetal impeller 2 in the radial direction of the centripetal impeller 2 through the Raphael nozzle 5.
[0036] In this embodiment, the Rafal nozzle 5 is used to convert the high-pressure gas pressure energy into high-speed kinetic energy. The Mach number of the nozzle outlet can usually reach 2 or more. The high-speed airflow entering radially will pu...
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