Method for calculating thermal performance of working process of air cylinder of marine main engine
A technology of ship main engine and thermal performance, applied in computing, special data processing applications, instruments, etc., can solve problems such as insufficient real-time performance
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[0026] The technical solutions of the present invention are further described below in conjunction with specific embodiments.
[0027] Based on the mean value model, the invention uses the Seiliger cycle to divide the process of the main engine cylinder of the ship into a variable compression process, a constant volume combustion process, an isobaric combustion process and a variable expansion process, and the thermal performance parameters of each process are calculated separately.
[0028] figure 1 is the Seiliger cycle p-ψ, the abscissa ψ in the figure represents the crankshaft angle, the ordinate p represents the pressure in the cylinder, BDC is the bottom dead center, TDC is the top dead center, IC is the closing time of the scavenging hole, and EC is the closing time of the exhaust valve , EO is the opening time of the exhaust valve, 1-2 is the variable compression process, 2-3 is the constant volume combustion process, 3-4 is the isobaric combustion process, 4-5 is the ...
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