|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||165/41 ; 165/10425 ; 165/10427 ; 415/89|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 3|
A heat management system especially adapted for spacecraft including a first heat exchanger in heat exchange relation with a sink having a widely varying temperature and a second heat exchanger in heat exchange relation with a variable heat load. An equilibrator is provided to maintain respective bodies of heat exchange fluid in the liquid state and in the gaseous state. A first flow path is provided for circulating a mixture of liquid phase fluid and gaseous phase fluid from the equilibrator to the first heat exchanger and return fluid from the first he...
A heat management system for use in spacecraft or the like comprising a first heat exchanger of the radiator type for radiating heat into space; a second heat exchanger for transferring heat from a variable heat load on a spacecraft; means for establishing a heat exchange fluid flow path between said heat exchangers; means for regulating fluid flow in said flow path; and a pump forming part of said flow path comprising a rotary drum driven about an axis at sufficient speed to cause fluid therein in the liquid phase to move radially outwardly and form an ...