Abstract:
According to an embodiment of the present invention, a heat radiation-thermoelectric fin which has an outstanding thermal conversion efficiency, is capable of implementing heat radiation and thermal development at the same time, and includes a composite laminate of graphene and thermal minerals can be provided. A thermoelectric module and a thermoelectric apparatus comprising the heat radiation-thermoelectric fin can be valuably used for cogeneration and thermal nuclear power for military aerospace.
Abstract:
Provided are a composite laminate which is a self-assembly structure and a manufacturing method thereof. The composite laminate includes graphene and a thermoelectric inorganic material. An ionic bond is formed between the graphene and the thermoelectric material. Also, provided are a thermoelectric material including the composite laminate, a thermoelectric device including the same, a thermoelectric module including the thermoelectric device, and a thermoelectric apparatus including the same.
Abstract:
Provided are a composite laminate including graphene and a thermoelectric inorganic material and a manufacturing method thereof. The thermoelectric inorganic material includes a single crystal with a hexagonal crystal system. Also, provided are a thermoelectric material including the composite laminate, a thermoelectric device including the same, a thermoelectric module including the thermoelectric device, and a thermoelectric apparatus including the same.
Abstract:
열 전도 장치는 연소반응물질의 화염을 길이방향으로 전파하는 채널 몸체 및 상기 연소반응물질을 상기 채널 몸체로 전달하는 연료 공급부를 포함하되, 상기 채널 몸체는, 상기 길이방향으로 연장되고, 관(pipe) 형상으로 형성된 단열층 및 상기 단열층 내부면의 상부에 형성된 열 전달층을 포함하고, 상기 열 전달층은 상기 길이방향으로의 열 전달 정도가 상기 길이방향과 수직한 방향으로의 열 전달 정도 보다 큰 열 전달 이등방성을 가진다.