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A test method for measuring low temperature thermal insulation performance of vacuum conveying pipe

A low-temperature insulation and test method technology, applied in the direction of thermal development of materials, can solve problems such as differences in thermal insulation performance and difficult thermodynamic parameters, and achieve the effects of avoiding overflow, high test safety, and reducing the influence of heat leakage.

Active Publication Date: 2021-09-07
BEIJING INST OF ASTRONAUTICAL SYST ENG +1
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  • Description
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Problems solved by technology

[0004] It is difficult to directly measure the low-temperature thermodynamic parameters of the vacuum conveying pipe. The main difficulties are: 1. The vacuum chamber of the conveying pipe is a closed structure, and it is difficult to arrange temperature measuring points in the vacuum chamber for temperature measurement; 2. The flanges and compensators at both ends of the vacuum conveying pipe etc. adopt the external insulation scheme, the insulation performance of the above components is significantly different from that of the vacuum tube part, so it is difficult to use a simple thermodynamic model to describe the insulation performance of the whole tube

Method used

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  • A test method for measuring low temperature thermal insulation performance of vacuum conveying pipe
  • A test method for measuring low temperature thermal insulation performance of vacuum conveying pipe
  • A test method for measuring low temperature thermal insulation performance of vacuum conveying pipe

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Embodiment Construction

[0040] 1. Parametric model of low temperature insulation performance of vacuum conveying pipe

[0041] Considering that the low temperature insulation performance of vacuum pipeline determines the heat exchange rate between the inside and outside of the pipeline, the heat flow Q can be used as a characterization parameter of the insulation performance. The heat flow Q is defined as the heat that enters the interior (liquid hydrogen temperature) from the outside (normal temperature) of the pipeline per unit time. This parameter reflects the overall thermal insulation performance of the pipeline, which naturally includes heat exchange at complex structures such as flanges and compensators.

[0042] Since it is difficult to arrange temperature measuring points in the vacuum chamber of the pipeline, the heat flow Q cannot be calculated from the temperature test data. Considering that the heat from the outside of the pipeline into its interior will be absorbed by the liquid hydrog...

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Abstract

The invention relates to a test method for measuring the low-temperature thermal insulation performance of a vacuum conveying pipe, which belongs to the field of testing the thermal insulation performance of the vacuum conveying pipe at low temperature (in the liquid hydrogen temperature zone). The present invention adopts real low-temperature propellant (liquid hydrogen) to test, and both ends of the vacuum conveying pipe to be tested are connected with tooling filled with liquid hydrogen, which is consistent with the working state of the vacuum conveying pipe on the arrow; hydrogen (liquid hydrogen) has easy However, in the test system proposed by the present invention, the liquid hydrogen (liquid hydrogen) is isolated from the outside world, which is safe and reliable; the lower end of the vacuum delivery pipe to be tested is connected to the cold screen, and at the same time, the method of connecting the pipeline to the tooling can be The construction of the heat insulation structure minimizes the impact of heat leakage; the liquid hydrogen filling conduit has a U-shaped backwater bend structure to prevent liquid hydrogen vapor from overflowing from the liquid hydrogen filling conduit.

Description

technical field [0001] The invention relates to a test method for measuring the low-temperature thermal insulation performance of a vacuum conveying pipe, which belongs to the field of testing the thermal insulation performance of the vacuum conveying pipe at low temperature (in the liquid hydrogen temperature zone). Background technique [0002] The new generation of launch vehicle core-level liquid hydrogen delivery pipes adopts a vacuum condensation scheme to achieve pipe insulation. The vacuum conveying pipe is mainly composed of inner pipe and outer pipe, and also includes compensator, flange and other components to meet the needs of pipeline installation and compensation. In order to reduce the heat loss of the tube wall and improve the thermal insulation performance of the pipeline, the interlayer between the inner and outer tubes of the vacuum delivery tube must be evacuated before use and filled with carbon dioxide for protection, forming a double-layer vacuum pipel...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01N25/20
CPCG01N25/20
Inventor 吴立夫刘艳吴云峰张萌陈牧野武园浩王儒文卫强石佳霍毅税晓菊
Owner BEIJING INST OF ASTRONAUTICAL SYST ENG
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