Vacuum heat insulator and testing method for the glass fiber laminate to be used in the insulator
Vacuum insulator includes core member and jacket which covers core member. Jacket is decompressed its interior and core member includes a glass-fiber laminated unit. The glass fiber is formed of toughened glass-fiber which is low brittle and its fiber strength is toughened. This structure allows improving the heat insulating performance as well as lowering the material cost of vacuum insulator.
1. A vacuum insulator comprising:
a core member comprising a laminated unit formed of glass fiber webs, glass fibers forming the glass fiber webs having low brittleness; and
a jacket having a decompressed interior and covering the core member, wherein:
the core member is formed with no binder, and
the core member has a brittleness property B of 0.89 or more, where the brittleness property B is measured such that, when a compressive strength of the core member reaches 1800 hPa in a first compression step, a thickness of the core member is set as first datum thickness T 1800 , and when a thickness of the core member reaches the first datum thickness T 1800 in a second compression step, a ratio of a compressive strength of the core member in the second compression step to 1800 hPa is defined as the brittleness property B.
2. The vacuum insulator of claim 1 , wherein the core member is constructed by forming the laminated unit into a plate shape.
3. The vacuum insulator of claim 2 , wherein the core member is constructed by heat forming the laminated unit into a plate shape.
4. The vacuum insulator of claim 1 , wherein the core member is compressed by a compressive strength of 2000 hPa, then the compressive is removed, and the core member undergoes this compression and removal repeatedly,
wherein when a compressive strength of the core member reaches 1800 hPa in a first compression step, a thickness of the core member is measured as first datum thickness T 1800 ,
wherein when a compressive strength applied to the core member reaches 1800 hPa in a second compression step, a thickness of the core member is set as first measured thickness T M1 ,
wherein first thickness ratio Y 1 is expressed as
Y 1 =T M1 /T 1800 ≧0.98.
5. The vacuum insulator of claim 1 , wherein the glass fibers are toughened glass fibers toughened by a chemical strengthening method.
6. The vacuum insulator of claim 1 , wherein the glass fibers are toughened glass fibers toughened by an ion exchange method.
7. The vacuum insulator of claim 1 , wherein the glass fibers are toughened glass fibers toughened by cool air blasting immediately after the glass fiber is fiberized.
8. The vacuum insulator of claim 1 , wherein immediately after the fiber is fiberized, cooled air blasted to the fiber, so that the fiber structure is quenched and toughened so that the core member has the brittleness property when, the core member is compressed by a compressive strength of 2000 hPa, then the compressive is removed, and the core member undergoes this compression and removal repeatedly.
9. The vacuum insulator of claim 1 , wherein the glass fiber web is formed of first glass fibers disposed substantially in parallel with a cross section of the core member and second glass fibers disposed substantially in a vertical direction with respect to the cross section of the core member.
10. The vacuum insulator of claim 1 , further comprising an adsorbent covered by the jacket.
11. The vacuum insulator of claim 1 , wherein each of the glass fibers has a tensile strength of not lower than 0.5 GPa.
12. The vacuum insulator of claim 1 , wherein a density of the core member is between 225 kg/m 3 and 245 kg/m 3 .
13. A vacuum insulator comprising:
a core member comprising a laminated unit formed of glass fiber webs, glass fibers forming the glass fiber webs having low brittleness; and
a jacket having a decompressed interior and covering the core member, wherein:
the core member is formed with no binder,
the core member has a brittleness property B of 0.89 or more, where the brittleness property B is measured such that, when a compressive strength of the core member reaches 1800 hPa in a first compression step, a thickness of the core member is set as first datum thickness T 1800 , and when a thickness of the core member reaches the first datum thickness T 1800 in a second compression step, a ratio of a compressive strength of the core member in the second compression step to 1800 hPa is defined as the brittleness property B, and
the glass fibers are toughened such that the laminated unit has the brittleness property B of 0.89 or more, by at least one method of:
a chemical strengthening method by which Griffith flaws at surfaces of the glass fibers are removed by using a hydrofluoric acid;
an ion exchange method by which Na ions on surfaces of the glass fibers are replaced with K ions, thereby forming a layer having higher compressive stress on the surfaces of the glass fibers than inside the glass fibers; and
an air-blast quench method by blasting a cool air immediately after the glass fibers are fiberized, thereby forming a layer having higher compressive stress on the surfaces of the glass fibers than inside the glass fibers.