Method for automatically identifying diesel spray crushing process and automatically realizing spray continuous calculation
A crushing process and automatic identification technology, which is applied in the testing of engines, engine components, fuel injection devices, etc., can solve the problems of not being able to dynamically change the interval position, not suitable for changing the working state, and greatly affecting the calculation accuracy.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2020-02-28
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Abstract
Description
technical field
[0001] The invention belongs to the research field of diesel engine spray characteristics and relates to a simulation calculation method of spray characteristics. Background technique
[0002] The high-pressure diesel oil enters the cylinder of the diesel engine through the nozzle jet flow. During the jet flow process, the diesel oil will firstly form a liquid film on the periphery of the liquid column from the continuous liquid column state at the outlet, and further develop with the jet flow, the liquid film breaks and begins to produce droplets. These The droplets are further broken and developed, and finally atomized. This is a process along the direction of the jet, where there is a continuous liquid phase region, a transition region where the continuous phase and the discrete phase are mixed, and a full droplet region where all the discrete phases are present. The cost of existing optical testing methods is high, and simulation calculation simulation i...
Examples
Embodiment Construction
[0030] Enter the entire flow field calculation domain from the outlet of the nozzle, calculate the flow field grid at the first step, and use the large eddy simulation method for the atomization flow field, and in order to simplify the calculation amount, use the RANS equation for near-wall processing, free shear The layer is simulated by LES. In order to reduce the calculation amount under the premise of ensuring the calculation accuracy, the sub-model of the large eddy equation is calculated using WNLES S-Omega, the near-field VOF model is calculated using the Explicit method, and the far-field DDM model is calculated using the KH-RT fragmentation model calculate.
[0031] The simulation boundary conditions and calculation model parameters are as follows: inlet pressure 100Mpa, back pressure 1Mpa, nozzle diameter 0.3mm, aspect ratio 5, fluid diesel, wall temperature 298.15K, fluid density 850kg / m3, surface tension coefficient 0.031N / m, the air is a compressible gas, the air...