Low-temperature air intake method for internal combustion engine and engine
A technology for an engine and an internal combustion engine, which is applied to the low-temperature air intake method of an internal combustion engine and the field of the engine, can solve the problems of consuming other work or low-temperature substances, increasing the intake air volume, reducing the thermal efficiency, etc., and achieving energy saving and environmental protection, high utilization rate, structure simple effect
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Embodiment 1
[0058] Such as figure 1 The residual energy refrigeration low-temperature engine shown includes a cylinder-piston mechanism 1, and the exhaust passage of the cylinder-piston mechanism 1 is provided with a refrigeration unit 1100 driven by exhaust energy, and the refrigeration unit 1100 is used to cool the Intake air in the intake duct of the cylinder-piston mechanism 1.
Embodiment 2
[0060] Such as figure 2 The difference between the residual energy refrigeration low-temperature engine shown in Embodiment 1 is that the refrigeration unit 1100 is a compression expansion refrigeration unit A 130 ( figure 2 The dotted box shown in ), the compression expansion refrigeration unit A 130 includes a turbine power mechanism A 20 , an impeller compressor A 30 , a turbine power mechanism B 21 and a heat exchanger A 40 connected in sequence; A cooler A 50 is provided on the communication passage between A 20 and impeller compressor A 30, and the turbine power mechanism A 20 and the impeller compressor A 30 are coaxially arranged; the exhaust passage of the cylinder-piston mechanism 1 is connected to The working fluid inlet of the turbine power mechanism A 20 is connected, and the working fluid outlet of the turbine power mechanism B 21 is connected with the heated fluid inlet of the heat exchanger A 40; the cooled fluid of the heat exchanger A 40 The outlet communi...
Embodiment 3
[0063] Such as image 3 The difference between the residual energy cooling low-temperature engine shown in Embodiment 2 is that a desuperheater B 51 is provided on the communication channel between the impeller compressor A 30 and the turbine power mechanism B 21 .
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