Premixed carbon dioxide pneumatic laser driven by combustion of continuous rotary detonation rocket
A technology driven by combustion and carbon dioxide, which is applied to lasers, laser components, phonon exciters, etc., can solve the problems of low energy efficiency ratio, low light output rate, low laser efficiency, etc., and achieve high thermal cycle efficiency, improved laser efficiency, The effect of high laser efficiency
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[0042] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific preferred embodiments.
[0043] In the description of the present invention, it should be understood that the orientations or positional relationships indicated by the terms "left side", "right side", "upper", "lower" are based on the orientations or positional relationships shown in the accompanying drawings, and are only For the purpose of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operate in a specific orientation, "first", "second" and the like do not represent components importance, and therefore should not be construed as limiting the invention. The specific dimensions used in this embodiment are only for illustrating the technical solution, and do not limit the protection scope of the present in...
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