A dual-channel power turbine system and its control method
A power turbine and dual-channel technology, which is applied to engine components, combustion engines, machines/engines, etc., can solve the problem of low energy recovery rate of exhaust gas, achieve high energy recovery rate of exhaust gas, increase turbocharger turbine speed, and increase output The effect of power
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Embodiment 1
[0048] see figure 1 , a dual-channel power turbine system, comprising an internal combustion engine body 1, a turbocharger 3, and a mechanical transmission 6, the turbocharger 3 comprising a mechanically connected compressor 31 and a turbocharger turbine 32, the compressor 31 The air outlet is connected with the internal combustion engine body 1 gas path after the intake manifold 11, the air inlet of the supercharger turbine 32 is connected with the internal combustion engine body 1 gas path after the exhaust manifold 12, and the gas outlet of the supercharger turbine 32 is connected with the internal combustion engine body 1 gas path. The dual-channel power turbine 7 is connected to the air path, and the dual-channel power turbine 7 is mechanically connected to the internal combustion engine body 1 through the mechanical transmission device 6; the dual-channel power turbine 7 includes a No. 1 power turbine flow channel 71 and a No. 2 power turbine flow channel 72 The air inle...
Embodiment 2
[0051] Basic content is the same as embodiment 1, the difference is:
[0052] see figure 1 , the flow cross-sectional area of the first power turbine flow channel 71 and the second power turbine flow channel 72 is smaller than the flow cross-sectional area of the supercharger turbine 32; The gas manifold 11 is connected with the gas path of the internal combustion engine body 1;
[0053] The compressed air enters the internal combustion engine body 1 through the air outlet of the compressor 31 and the intake manifold 11 successively, which means that the compressed air enters the intercooler 9 after passing through the air outlet of the compressor 31, and the compressed air The air enters the intake manifold 11 after being cooled by the intercooler 9, and then enters the internal combustion engine body 1.
Embodiment 3
[0055] Basic content is the same as embodiment 1, the difference is:
[0056] see figure 1 , the air inlet of the No. 1 power turbine channel 71 is connected to the gas path of the internal combustion engine body 1 through the bypass valve 5, the bypass pipeline 4, and the exhaust manifold 12 in sequence; the bypass valve 5 is electronically controlled Butterfly valve, the control end of the bypass valve 5 is connected to the signal of the internal combustion engine ECU2, the internal combustion engine ECU2 is connected to the signal of the internal combustion engine body 1, and the signal of the internal combustion engine ECU2 is connected to the pressure sensor 13 arranged on the intake manifold 11;
[0057] When the internal combustion engine is at low speed and low load: the bypass valve 5 is closed, at this time, the exhaust gas in the internal combustion engine body 1 passes through the exhaust manifold 12 and the turbocharger turbine 32 and then enters the No. The powe...
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