Vacuum Insulation Laminate Structure for Low Heat Bridge Sealing
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Solution Overview
Problem
Vacuum insulating materials face issues with heat bridges due to high thermal conductivity of aluminum foils, poor gas barrier properties of metal deposition films, and workability problems caused by thickness and modulus differences between metal foils and plastics, leading to pinholes and cracks.
Innovation Solution
A laminated structure with a polymer layer, a gas barrier layer, and an adhesive layer, where the gas barrier layer has thermal resistance greater than or equal to 650 K/W and a Young's modulus of greater than or equal to 100 GPa, with the kinetic neutral axis positioned in the gas barrier layer to minimize heat bridges and improve workability.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If aluminum foil is used as the gas barrier layer, then gas barrier properties are improved, but thermal conductivity increases causing heat bridges
Solution Approach 1:
The patent uses a composite laminated structure consisting of multiple layers including polymer layers and a metal foil layer with specific thermal resistance (≥650 K/W) and Young's modulus (≥100 GPa). This composite structure combines the gas barrier properties of metal foils with the thermal resistance characteristics of specific metal compositions, while the adhesive layers between polymer and metal layers create a structure that reduces heat bridge formation through the exterior material.
2Reliability
If metal foil thickness is increased to 20 micrometers, then gas barrier properties are improved, but heat bridge increases due to higher thermal mass
Solution Approach 1:
The patent specifies precise parameter ranges for the metal foil layer: thermal resistance of at least 650 K/W and Young's modulus of at least 100 GPa. These parameter constraints optimize the balance between gas barrier performance and thermal resistance, preventing heat bridge formation while maintaining effective gas barrier properties without requiring excessive thickness.
3Reliability
If metal foil with plastic is laminated, then gas barrier properties are improved, but workability deteriorates due to large difference in Young's modulus
Solution Approach 1:
The patent introduces adhesive layers at the interfaces between polymer layers and the metal foil layer. These adhesive layers have specific mechanical properties that differ from both the polymer and metal layers, creating a gradient structure that reduces stress concentration and improves bending workability during fabrication while maintaining the gas barrier integrity of the metal foil layer.
4Reliability
If excessive heat seal parts are folded, then sealing is improved, but pinholes and cracks are generated due to stress concentration
Solution Approach 1:
The adhesive layers are positioned beforehand at the interfaces between polymer and metal layers, creating a cushioning effect that absorbs and distributes stress during the folding and heat sealing processes. This pre-positioned adhesive cushioning prevents stress concentration that would otherwise cause pinholes and cracks in the exterior material during fabrication.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
The solution effectively reduces heat bridges, enhances workability, and suppresses the generation of pinholes and cracks, maintaining a high vacuum degree and improving the gas barrier properties of vacuum insulating materials.
Implementation Method 1
a gas barrier layer, and a polymer layer comprising at least one layer in sequence
Implementation Method 2
an adhesive layer is interposed between each layer
Data Source
AI summary
A laminated structure includes a polymer layer comprising at least one layer, a gas barrier layer which has thermal resistance of greater than or equal to about 650 degrees Kelvin per watt and a Young's modulus of greater than or equal to about 100 gigapascals, and a position of a neutral axis represented by the following Equation 1 is in the gas barrier layer.y=∑i=1n(Ei·Si)∑i=1n(Ei·Ai)(Equation1)In Equation 1, y denotes a distance from the top surface of a side compressed in bending to the neutral axis, Ei denotes a Young's modulus of the i-th layer, Si denotes a geometrical moment of area of the i-th layer, Ai denotes a cross-sectional area of the i-th layer, and n denotes a number of layers for the laminated structure, which is an integer of greater than or equal to 5.


