发明名称 |
AN ACTIVE COOLING PANEL OF THERMOSTRUCTURAL COMPOSITE MATERIAL AND METHOD FOR ITS MANUFACTURE |
摘要 |
The active cooling panel (10) comprises a first part (20) and a second part (30) of thermostructural composite material, each having an inside face and an opposite outside face, the parts being assembled together by bonding their inside faces (21, 31) together, and channels (24) being formed by indentations formed in the inside face of at least one of the first and second parts. The panel further includes a sealing layer (38) bonded to at least one of the first and second parts and situated at a distance from the assembled-together inside faces thereof. The invention is applicable to making heat exchanger walls such as the walls for the combustion chambers of aircraft engines, or the diverging portions of rocket engines, or plasma confinement chambers in nuclear fusion reactors.
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申请公布号 |
CA2456403(A1) |
申请公布日期 |
2004.07.30 |
申请号 |
CA20042456403 |
申请日期 |
2004.01.29 |
申请人 |
SNECMA PROPULSION SOLIDE |
发明人 |
UHRIG, GILLES;LARRIEU, JEAN-MICHEL;THEBAULT, JACQUES;BOUQUET, CLEMENT |
分类号 |
F01D5/28;B23K20/00;B23K103/16;C04B37/00;C04B41/88;F02C7/00;F02C7/18;F02C7/28;F02K9/34;F02K9/64;F02K9/97;F23R3/00;F23R3/42;F28F3/12;F28F21/08;(IPC1-7):B32B15/04 |
主分类号 |
F01D5/28 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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