Stable measurement method for heat conduction coefficient of non-embedded multilayer composite material

A multi-layer composite material and thermal conductivity technology, applied in the field of heat transfer, can solve the problems of multi-layer composite material damage, inaccurate measurement results, etc., and achieve the effect of high precision

Active Publication Date: 2019-09-20
XI AN JIAOTONG UNIV
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  • Abstract
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  • Application Information

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Problems solved by technology

When the existing measurement technology measures the thermal conductivity of a layer of a multilayer composite material, it is necessary to disassemble the multilayer composite material or insert a detector into the material, which will cause damage to the multilayer composite material
Or, when a certain layer of material is taken out separately and the thermal conductivity is measured, the measurement result will be inaccurate due to excessive radiation heat dissipation

Method used

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  • Stable measurement method for heat conduction coefficient of non-embedded multilayer composite material
  • Stable measurement method for heat conduction coefficient of non-embedded multilayer composite material
  • Stable measurement method for heat conduction coefficient of non-embedded multilayer composite material

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Embodiment Construction

[0027] Specific embodiments of the present invention will be described in more detail below with reference to the accompanying drawings. Although specific embodiments of the invention are shown in the drawings, it should be understood that the invention may be embodied in various forms and is not limited to the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present invention and to fully convey the scope of the present invention to those skilled in the art.

[0028] It should be noted that certain terms are used in the specification and claims to refer to specific components. Those skilled in the art should understand that they may use different terms to refer to the same component. The specification and claims do not use differences in nouns as a way of distinguishing components, but use differences in functions of components as a criterion for distinguishing. "Includes" or "comprises" mentioned throughout the spe...

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Abstract

The invention discloses a stable measurement method for a heat conduction coefficient of a non-embedded multilayer composite material. The method comprises the following steps that the multilayer composite material comprises g composite material layers, a to-be-identified material layer m is clamped in the composite material layers, a heat conduction coefficient of the to-be-identified material layer m is divided into n segments, each segment of heat conduction coefficient serves as a linear function of the temperature, 2n groups of material heat insulation performance test are carried out on the multilayer composite material, a boundary condition of material heat insulation performance test includes a constant temperature boundary of the front side of the multiplayer composite material and a constant heat flow boundary of the back side of the multilayer composite material, after that the multilayer composite material is thermally stabled, the temperature value of the back side of the multilayer composite material is measured and recorded, a one-dimensional model is generated and separated into two one-dimensional models by the to-be-identified material layer, the two one-dimensional models generate corresponding temperature fields based on the boundary condition, and each segment of the heat conduction coefficient of the to-be-identified material layer is generated based on the temperature field to obtain a heat conduction coefficient measuring value of the to-be-identified material layer.

Description

technical field [0001] The invention belongs to the field of heat transfer, in particular to a steady-state measurement method for the thermal conductivity of non-embedded multilayer composite materials. Background technique [0002] In the field of aerospace, due to the extreme and complexity of the application environment, the outer walls of hypersonic vehicles are mostly made of high heat-resistant multilayer composite materials. Multilayer composites are laminated and pressed from several materials with different properties and have excellent mechanical and thermal insulation properties. Accurately obtaining the thermophysical properties of each layer of material is a necessary prerequisite for the use of multilayer composites. In order to accurately obtain the thermal insulation performance of typical multi-layer composite materials in different use environments, and support material application evaluation, it is necessary to carry out typical thermal insulation materi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N25/20
CPCG01N25/20
Inventor 屈治国郭君
Owner XI AN JIAOTONG UNIV
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