A double-pulse burner with time-sharing ignition output in one chamber
A dual-pulse, combustor technology, applied in the direction of rocket engine devices, machines/engines, jet propulsion devices, etc., can solve the problems of unable to dynamically compensate for temperature loss, difficult to meet the endurance time, and low proportion of charge mass, etc. Achieve the effect of reducing the space of structural parts, improving space utilization, and avoiding insufficient inflation or overpressure
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[0029] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0030]Below in conjunction with accompanying drawing, the present invention is described in further detail:
[0031] Such as Figure 1 to Figure 4 As shown, according to the present invention, a double-pulse burner with time-sharing ignition output in a common chamber includes: a housing part 1, a primary charge 5, a secondary charge 9, a pr...
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