Vacuum suction cup isolation type automatic anti-ice device and method of low-temperature filling system
A filling system and vacuum suction cup technology, applied in valve devices, engine components, safety valves, etc., can solve the problems of high risk factor, high labor intensity, easy to cause explosions, etc. in field operation, and achieve a high degree of automation and high versatility. , to solve the effect of surface frosting
Active Publication Date: 2017-11-24
BEIJING INST OF SPACE LAUNCH TECH +1
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Problems solved by technology
At present, before the secondary docking process is performed, the frost and ice on the surface of the inner cavity of the low-temperature filling system are usually wiped off by manual multiple erasing, which is inefficient, labor-intensive, and has a high risk factor for on-site operations and is prone to explosions. and other security incidents
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[0026] Such as figure 1 shown, combined with figure 2 As shown, what the two figures show is the low-temperature filling system 1 in the prior art. The vacuum suction cup isolation type automatic anti-icing device of the low-temperature filling system in the present invention is just applied to this system to prevent its surface from frosting and freezing. ice.
[0027] Such as image 3 shown, combined with Figure 4 As shown, the vacuum suction cup isolation automatic anti-icing device of the low temperature filling system in the present invention includes a suction cup 3, the edge of the suction cup 3 is provided with a sealing body, and the outer surface of the suction cup 3 is fixed with a tray 5 and an elastic support plate 4, The tray 5 and the elastic support plate 4 are fixedly connected, the tray 5 is fixed with a sliding shaft 15, the sliding shaft 15 is set in a base 10, and a spring 11 is arranged between the base 10 and the sliding shaft 15 , the base 10 is p...
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The invention discloses a vacuum suction cup isolation type automatic anti-ice device and method of a low-temperature filling system. The device comprises a suction cup (3). A tray (5) and elastic supporting plates (4) are fixed to the suction cup (3). A sliding shaft (15) is fixedly arranged on the tray and is mounted in a base (10) in a sleeved manner. A proximity switch (14) and an induction block (9) are fixedly arranged on the base and the sliding shaft correspondingly. An air suction hole connector (7), an air inlet hole connector (8) and a pressure sensor (6) are arranged on the tray. The method comprises the following steps that the device is aligned to and approaches to the low-temperature filling system, after the device is in contact with the low-temperature filling system, a spring is compressed, and the device stops propulsion; negative pressure is formed in the suction cup; and the device is adsorbed to the low-temperature filling system, and the anti-ice function is achieved. The vacuum suction cup isolation type automatic anti-ice device and method of the low-temperature filling system have the beneficial effects of being good in anti-ice good, high in adaptability, high in universality, high in automation degree, safe to use and the like.
Description
technical field [0001] The invention relates to the field of automatic low-temperature filling, in particular to a vacuum suction cup isolated automatic anti-icing device and method for a low-temperature filling system. Background technique [0002] In aerospace, aviation, LNG and other fields, cryogenic filling systems are widely used to fill cryogenic media (liquid hydrogen, liquid oxygen, liquid natural gas, etc.) During the low-temperature filling process, the temperature of the filling device, connectors, valves and other equipment in the filling system drops rapidly under the action of the low-temperature medium, and due to the moisture in the outside air, frost and ice appear on the outer wall. Especially after the low-temperature filling is completed and the equipment falls off, the inner cavity of the equipment is exposed to the air, and frosting and freezing occur rapidly. In order to ensure the safety of the low-temperature filling system and the normal execution...
Claims
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IPC IPC(8): F16K17/00
CPCF16K17/00
Inventor 李泳峄吴新跃何冠杰白文龙李帅
Owner BEIJING INST OF SPACE LAUNCH TECH