Heat receiving tile formed of carbon fiber composite material and method of manufacturing the same

Patent metadata

Field	Value
Publication number	US-2017167802-A1
Application number	US-201515117009-A
Country	US
Kind code	A1
Filing date	Feb 5, 2015
Priority date	Feb 5, 2014
Publication date	Jun 15, 2017
Grant date	—

Abstract

This heat receiving tile formed of CFC is provided with a heat receiving block formed of a carbon fiber composite material and having a through hole, a cooling pipe inserted through the through hole of the heat receiving block, a buffer material provided to an outer periphery of the cooling pipe, a first brazing portion joining an inner surface of the through hole with an outer surface of the buffer material, a second brazing portion joining an inner surface of the buffer material with an outer surface of the cooling pipe, and a material discontinuous portion extending from a heat receiving surface of the heat receiving block up to the outer surface of the cooling pipe over a full length of the heat receiving block in an axis direction of the through hole.

First claim

1 . A heat receiving tile formed of carbon fiber composite material used for a high heat load heat receiving equipment, comprising:
a heat receiving block formed of a carbon fiber composite material and having a through hole; a cooling pipe inserted through the through hole of the heat receiving block; a buffer material provided to an outer periphery of the cooling pipe; a first brazing portion joining an inner surface of the through hole with an outer surface of the buffer material; a second brazing portion joining an inner surface of the buffer material with an outer surface of the cooling pipe; and a material discontinuous portion extending from a heat receiving surface of the heat receiving block up to at least the outer surface of the buffer material over a full length of the heat receiving block in an axis direction of the through hole.

2 . The heat receiving tile formed of carbon fiber composite material according to claim 1 , wherein the material discontinuous portion is defined by a pair of material surfaces opposed to each other.

3 . The heat receiving tile formed of carbon fiber composite material according to claim 2 , wherein the pair of material surfaces are formed so as to be separated from each other.

4 . The heat receiving tile formed of carbon fiber composite material according to claim 3 , wherein the material discontinuous portion is a slit.

5 . The heat receiving tile formed of carbon fiber composite material according to claim 2 , wherein the pair of material surfaces are in contact with each other at least on a side of the heat receiving surface.

6 . The heat receiving tile formed of carbon fiber composite material according to claim 1 , wherein the material discontinuous portion is formed by making a cut in the heat receiving block in a process of manufacturing the heat receiving tile.

7 . The heat receiving tile formed of carbon fiber composite material according to claim 1 , wherein the cooling pipe is formed of a copper alloy material.

8 . The heat receiving tile formed of carbon fiber composite material according to claim 1 , wherein the high heat load heat receiving equipment is an equipment used as a first wall of a nuclear fusion device.

9 . The heat receiving tile formed of carbon fiber composite material according to claim 1 , wherein the material discontinuous portion extends from the heat receiving surface of the heat receiving block up to the outer surface of the cooling pipe.

10 . A method of manufacturing a heat receiving tile formed of carbon fiber composite material used for a high heat load heat receiving equipment comprising the steps of:
providing a heat receiving block formed of a carbon fiber composite material and having a through hole, the heat receiving block having a slit extending from a heat receiving surface of the heat receiving block up to the through hole over a full length of the heat receiving block in an axis direction of the through hole; disposing a first thin film bra/ins material on an inner surface of the through hole: disposing a buffer material on an inside of the first thin film brazing material; disposing a second thin film brazing material on an inside of the buffer material; disposing a cooling pipe to an inside of the second thin film brazing material; and brazing an assembly configured by the heat receiving block, the first thin film brazing material, the buffer material, the second thin film brazing material, and the cooling pipe.

11 . The method of manufacturing a heat receiving tile formed of carbon fiber composite material according to claim 10 , wherein the step of providing the heat receiving block includes a step of forming the slit by making a cut in a material forming the heat receiving block.

12 . The method of manufacturing a heat receiving tile formed of carbon fiber composite material according to claim 10 , wherein a width of the slit of the heat receiving block is set to a value such that the slit of the heat receiving block is closed at least on a side of the heat receiving surface when a brazing processing has been finished, resulting from a deformation of the heat receiving block caused by a difference between a thermal expansion coefficient of the heat receiving block and a thermal expansion coefficient of the cooling pipe in the step of brazing the assembly.

13 . The method of manufacturing a heat receiving tile formed of carbon fiber composite material according to claim 10 , wherein the cooling pipe is formed of a copper alloy material.

14 . The method of manufacturing a heat receiving tile formed of carbon fiber composite material according to claim 10 , wherein the high heat load heat receiving equipment is an equipment used as a first wall of a nuclear fusion device.

15 . The method of manufacturing a heat receiving tile formed of carbon fiber composite material according to claim 10 , wherein the heat receiving block has a fitting groove on an opposite side of the heat receiving surface, and wherein a jig is applied for suppressing a deformation of the fitting groove caused by a deformation of the slit in the step of brazing.

16 . The method of manufacturing a heat receiving tile formed of carbon fiber composite material according to claim 10 , wherein the buffer material has a slit extending in the axis direction of the though hole, the buffer material being disposed on the inside of the first thin film brazing material such that the slit of the heat receiving block and the slit of the buffer material coincide with each other.

Assignees

• Kawasaki Heavy Ind Ltd

Inventors

• Yamada Hirokazu
• Satou Kouji
• TSURU Daigo
• Sakurai Shinji
• Nakamura Shigetoshi

Classifications

• F28D20/0056 Primary

  using solid heat storage material (F28D20/0052 takes precedence) · CPC title

• F28F2275/04

  by brazing · CPC title

• F28F21/08

  of metal · CPC title

• B23K2103/12

  Copper or alloys thereof · CPC title

• F28F19/02

  by using coatings, e.g. vitreous or enamel coatings · CPC title