发明名称 Method for making a sealed passage in a refractory composite part, and application to the production of a refractory composite structure cooled by fluid circulation
摘要 PCT No. PCT/FR92/01243 Sec. 371 Date Jun. 29, 1994 Sec. 102(e) Date Jun. 29, 1994 PCT Filed Dec. 30, 1992 PCT Pub. No. WO93/13636 PCT Pub. Date Jul. 8, 1993A sealed passage is formed in a part of refractory composite material by inserting a tubular metal lining in a hole in the part, brazing material being interposed between the lining and the hole, and by heating to braze the metal lining to the wall of the hole, so that the metal lining defines a sealed passage (38). The metal lining (39) is plastically deformable under the conditions of use of the part such that differential expansion of thermal origin between the refractory composite material and the metal lining can be compensated by plastic deformation of the lining. The method is particularly applicable to providing thermal protection that is cooled by the flow of a cooling fluid, and that is suitable for a deflector in an electromagnetic confinement chamber for a plasma in an installation for controlled thermonuclear fusion, said protection being constituted by a plurality of elements (30) made of refractory composite material and having sealed internal passages (38) connected to pipework (40, 42) for feeding and removing a cooling fluid.
申请公布号 US5583895(A) 申请公布日期 1996.12.10
申请号 US19940256253 申请日期 1994.06.29
申请人 SOCIETE EUROPEENNE DE PROPULSION 发明人 FILIPUZZI, LUDOVIC;HUET, PHILIPPE
分类号 G21B1/11;F28F7/02;F28F19/02;G21B1/13;G21B1/17;H05H1/12;(IPC1-7):G21C11/08 主分类号 G21B1/11
代理机构 代理人
主权项
地址