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航空发动机热管理(宁波研究院复杂能量系统数字孪生创新团队)
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采用轻质板翅式换热器的喷射热泵机组
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回收节流损失驱动的强制对流循环满液式蒸发器制冷系统
可调整喷嘴喉口面积的喷射器
Release Time:2022-10-20
Hits:
First Author:
刘秀明
Disigner of the Invention:
张博,吴勇
Application Number:
201120570097.1