Direct-current cold-wall type engine combustor
A combustion chamber and engine technology, which is applied in the direction of machines/engines, rocket engine devices, mechanical equipment, etc., can solve the problems of reducing cooling effect and engine performance loss, and achieve improved atomization effect, long jet impact distance, and improved thermal protection effect of ability
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[0020] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention. In describing the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", The orientation or positional relationship indicated by "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying the referred device Or elements must have...
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