Method for adjusting combustion heat release distribution through plasma
A plasma and discharge plasma technology, which is applied in the field of ramjets, can solve the problems of rapid regulation and control of the intensity distribution of combustion heat release in the non-combustible area, and achieve the effect of rapid regulation and reduction of thermal energy consumption.
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Embodiment 1
[0031] like Figure 1-2 As shown, this embodiment provides a method for regulating the distribution of combustion heat release by plasma. In the engine combustion chamber, a plasma acting on the combustion zone is constructed, and a large number of high-energy active particles therein are used to increase the combustion heat release rate; through Changing the spatial distribution of high-energy active particles in the combustion zone affects the development of the flame form from a diffuse state to a high-concentration zone of active particles, causing axial changes in the main combustion zone, and realizing the adjustment of the spatial distribution of the law of combustion heat release.
[0032] In this embodiment, the discharge plasma has a large number of different types of high-energy active particles, which can accelerate physical processes such as fuel diffusion and atomization; because the active groups contained therein can accelerate the process of combustion reaction...
Embodiment 2
[0042] This embodiment is an improvement made on the basis of Embodiment 1, and its improvements are as follows:
[0043] The combustion chamber of the engine is a sub-combustion ramjet combustion chamber, and the method of adjusting the law of combustion heat release distribution is as follows: Figure 3-4 As shown, the engine combustion chamber is generally of the straight section type.
Embodiment 3
[0045] This embodiment is an improvement carried out on the basis of embodiment one or two, and its improvements are as follows:
[0046] The combustion chamber of the engine is a dual-mode ramjet combustion chamber, and the overall shape and structure of the combustion chamber is similar to that of a general scramjet engine.
[0047] Verify this example below:
[0048] (1) air flows into the engine; (2) engine fuel is injected into the engine; (3) the plasma igniter is turned on with a certain excitation intensity of a single power supply, and a stable central flame is formed in the engine combustion chamber; (4) the plasma igniter is converted A certain strong power into the coupling power supply is turned on.
[0049] According to the verification results of the above steps, through the enhanced effect of discharge plasma on combustion heat release, after the plasma igniter is turned on with a certain strong excitation power, the total temperature of the engine along the cou...
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