Aviation fuel storage device
The utility model relates to the technical field of aviation fuel tanks, and discloses an aviation fuel storage device which comprises an outer shell and an inner shell, a cavity is formed between the outer wall of the outer shell and the inner wall of the inner shell, and a temperature sensor is fi...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The utility model relates to the technical field of aviation fuel tanks, and discloses an aviation fuel storage device which comprises an outer shell and an inner shell, a cavity is formed between the outer wall of the outer shell and the inner wall of the inner shell, and a temperature sensor is fixedly installed on the inner wall of the inner shell. The outer wall of the inner shell is fixedly sleeved with a refrigeration assembly used for cooling aviation fuel, and cooling fins are evenly distributed on the outer wall of the refrigeration assembly. Through cooperation of the temperature sensor, the heating assembly, the junction box and the inner shell, the heating effect on aviation fuel in the inner shell is achieved through the arrangement of the heating assembly, the problem that a barrel type heating piece in the technical content is slow in heating is effectively solved, and the service life of the barrel type heating piece is prolonged. The mode that the heating piece in the heating assembly is woun |
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