Speed-staggered micro-mixing nozzle structure and combustion chamber
The invention relates to the technical field of jet propulsion, and provides a speed-staggered micro-mixing nozzle structure and a combustion chamber. The micro-mixing nozzle structure comprises a mounting seat and a first nozzle unit, the first nozzle unit is arranged on the mounting seat; the firs...
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Main Authors | , , , , |
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Format | Patent |
Language | Chinese English |
Published |
16.05.2023
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Subjects | |
Online Access | Get full text |
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Summary: | The invention relates to the technical field of jet propulsion, and provides a speed-staggered micro-mixing nozzle structure and a combustion chamber. The micro-mixing nozzle structure comprises a mounting seat and a first nozzle unit, the first nozzle unit is arranged on the mounting seat; the first nozzle unit comprises a plurality of reference position pre-mixing micropipes and a plurality of staggered position pre-mixing micropipes; the plurality of reference bit pre-mixing micropipes and the plurality of staggered bit pre-mixing micropipes are arranged side by side, and the plurality of staggered bit pre-mixing micropipes are arranged among the plurality of reference bit pre-mixing micropipes; the outlet end of the staggered position premixing micropipe is flush with the outlet end of the reference position premixing micropipe; the outlet end of the staggered position premixing micropipe and the outlet end of the reference position premixing micropipe have different jet flow speeds on mixed gas, so that |
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Bibliography: | Application Number: CN202310411041 |