Experimental device for measuring low-temperature foam breaking characteristic of porous metal screen
A technology of porous metal and experimental device, applied in measurement device, measurement of fluid pressure, pressure difference measurement between multiple valves, etc., can solve the limitations of low-temperature propulsion system PMD design optimization and on-orbit mature application, unable to form efficient and reliable The problems of low temperature propellant space gas-liquid management scheme, transient characteristics, influencing factors and performance improvement strategies are not clear, etc.
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[0022] The technical solutions of the present invention will be further described below in conjunction with the drawings and embodiments.
[0023] refer to figure 1 , an experimental device for measuring the low-temperature bubble breaking characteristics of a porous metal screen, comprising a vacuum insulating glass Dewar 1, a booster chamber 11, a filling / discharging system, a pressure regulating system, and a data acquisition system;
[0024] The material of the vacuum insulating glass Dewar 1 is high borosilicate glass (colorless and transparent); refer to figure 2 , the main body of the vacuum insulating glass Dewar 1 is a double wall structure with a vacuum interlayer, and the interior of the vacuum interlayer is less than 1.0×11 -4 In the high-vacuum environment of Pa, the vacuum insulation technology is used to reduce the thermal influence of the external thermal environment on the low-temperature inner cavity; the inner wall surface of the vacuum interlayer is plate...
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