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A platform for research: civil engineering, architecture and urbanism
Semiconductor temperature control auxiliary device applied to aircraft hangar and aircraft hangar
The embodiment of the invention discloses a semiconductor temperature control auxiliary device applied to an aircraft hangar, and belongs to the technical field of aircraft hangars, and the semiconductor temperature control auxiliary device applied to the aircraft hangar comprises a couple pair which is provided with a cold end and a hot end; the heat absorber is installed at the cold end of the galvanic couple pair, and the heat absorber is used for forming internal circulation in the aircraft hangar; the radiator is installed at the hot end of the galvanic couple pair, and the radiator is used for forming outer circulation outside the aircraft hangar in a fan side blowing mode. According to the scheme, the semiconductor cooler can be installed in a small installation space, the heat dissipation efficiency is improved, and meanwhile the weight of the radiator is reduced.
本发明实施例公开了一种应用于飞行器机库的半导体温控辅助装置，属于飞行器机库技术领域，该应用于飞行器机库的半导体温控辅助装置，包括：电偶对，所述电偶对具有冷端和热端；吸热器，所述吸热器安装在电偶对的冷端，所述吸热器用于在所述飞行器机库内形成内循环；散热器，所述散热器安装在所述电偶对的热端，所述散热器用于在所述飞行器机库外通过风扇侧吹的方式形成外循环。本申请的方案，能够在小安装空间安装半导体制冷器，提高了散热效率的同时减轻了散热器的重量。
Semiconductor temperature control auxiliary device applied to aircraft hangar and aircraft hangar
The embodiment of the invention discloses a semiconductor temperature control auxiliary device applied to an aircraft hangar, and belongs to the technical field of aircraft hangars, and the semiconductor temperature control auxiliary device applied to the aircraft hangar comprises a couple pair which is provided with a cold end and a hot end; the heat absorber is installed at the cold end of the galvanic couple pair, and the heat absorber is used for forming internal circulation in the aircraft hangar; the radiator is installed at the hot end of the galvanic couple pair, and the radiator is used for forming outer circulation outside the aircraft hangar in a fan side blowing mode. According to the scheme, the semiconductor cooler can be installed in a small installation space, the heat dissipation efficiency is improved, and meanwhile the weight of the radiator is reduced.
本发明实施例公开了一种应用于飞行器机库的半导体温控辅助装置，属于飞行器机库技术领域，该应用于飞行器机库的半导体温控辅助装置，包括：电偶对，所述电偶对具有冷端和热端；吸热器，所述吸热器安装在电偶对的冷端，所述吸热器用于在所述飞行器机库内形成内循环；散热器，所述散热器安装在所述电偶对的热端，所述散热器用于在所述飞行器机库外通过风扇侧吹的方式形成外循环。本申请的方案，能够在小安装空间安装半导体制冷器，提高了散热效率的同时减轻了散热器的重量。
Semiconductor temperature control auxiliary device applied to aircraft hangar and aircraft hangar
应用于飞行器机库的半导体温控辅助装置及飞行器机库
2022-08-05
Patent
Electronic Resource
Chinese