The present invention provides a heat pipe for a satellite, comprising: a main body extending long in the longitudinal direction; a hollow formed to penetrate in the longitudinal direction of the main body; a plurality of protrusions formed to protrude from the inner surface of the main body; a first coupling part disposed on one side of the main body and coupled to a first panel disposed on one side thereof; and a second coupling part disposed on the other side of the main body and coupled to a second panel disposed on the other side, wherein the first coupling part and the second coupling part are arranged to face in opposite directions to each other. In the present invention, since the first coupling part is coupled to the first panel and the second coupling part is coupled to the second panel, heat transfer between the two panels can be maximized and the rigidity of the two panels can be improved.

    본 발명은 길이 방향으로 길게 연장되어 형성된 메인바디; 상기 메인바디의 길이 방향으로 관통되게 형성된 중공; 상기 메인바디의 내측면에서 돌출되어 형성된 복수개의 돌기; 상기 메인바디의 일측에 배치되고, 일측면에 배치된 제 1 패널에 결합되는 제 1 결합부; 상기 메인바디의 타측에 배치되고, 타측면에 배치된 제 2 패널에 제 2 결합부;를 포함하고, 상기 제 1 결합부 및 제 2 결합부가 서로 반대방향을 향하게 배치된 인공위성을 위한 히트파이프를 제공한다. 본 발명은 제 1 결합부가 제 1 패널에 결합되고, 제 2 결합부가 제 2 패널에 결합되기 때문에, 2개의 패널 사이에서 열전달을 극대화할 수 있고, 2개 패널들의 강성을 향상시킬 수 있는 장점이 있다.


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    Title :

    heat pipe for satellite


    Additional title:

    인공위성을 위한 히트파이프


    Contributors:

    Publication date :

    2021-08-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    F28D Wärmetauscher, soweit in keiner anderen Unterklasse vorgesehen, in denen die Wärmetauschmittel nicht in direkte Berührung miteinander kommen , HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT / B64G Raumfahrt , COSMONAUTICS



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