Spatial efficient heat transfer micropump-driven fluid loop apparatus
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- SHANGHAI SATELLITE ENG INST
- Publication Date
- 2017-02-22
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
technical field
[0001] The invention relates to an aircraft thermal control device, in particular to a space-efficient heat transfer micropump driving fluid circuit. Background technique
[0002] With the development of future space missions, thermal control technology is facing new severe challenges for the increasingly harsh and complex space application environment and the development needs of multi-functional and multi-mission aircraft platforms. Conventional thermal control design concepts based on passive thermal control technologies such as multi-layers and coatings, supplemented by active thermal control technologies such as electric heaters, have been unable to meet the needs of ever-changing task development. The new thermal control technology represented by the active fluid circuit thermal control technology is widely used in manned spaceflight, space station, deep space exploration, High-power communication satellites and other fields have been widely demonstrat...