Concentric combined dual-rotor exhaust turbocharging system structure
An exhaust gas turbine and supercharging system technology, which is applied in gas turbine devices, machines/engines, internal combustion piston engines, etc., can solve the problems of low single-stage supercharging pressure ratio, increased weight, and narrow single-vortex dual-pressure flow range. The effect of improving the compactness, increasing the power density, and broadening the working range
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[0036] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other.
[0037] The present invention will be described in detail below with reference to the accompanying drawings and examples.
[0038] The structure of the concentric combined dual-rotor exhaust gas turbocharging system of the present invention includes twin compressor impellers and twin turbines connected together by concentric shafts to form a two-stage exhaust gas turbocharging structure; the dual compressor impellers are respectively low-pressure stage compressors The impeller 2 and the high-pressure stage compressor impeller 6, the twin turbines are respectively a high-pressure stage turbine 10 and a low-pressure stage turbine 11, and the low-pressure stage compressor impeller 2 and the low-pressure stage turbine 11 form a low-pressure stage turbine-compressor structure. The high-pressure stage compressor im...
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