发明名称 COMPOSITION GRADIENT THERMOSTRUCTURAL COMPOSITE STRUCTURE AND METHOD FOR THE PRODUCTION THEREOF
摘要 <p>Thermostructural composite structure having a compositional gradient, formed from a porous core (5) made of a refractory having a pore volume content of greater than or equal to 80%. The core (5) lies between two intermediate layers (6a, 6b) comprising the carbon fiber reinforcement, densified by a matrix composed of the carbon phase and of a ceramic phase, and a refractory solid filler. Two monolithic ceramic shells (7a, 7b) cover the intermediate layers in order to give stiffness to the entire structure.</p>
申请公布号 EP1651435(A2) 申请公布日期 2006.05.03
申请号 EP20040767700 申请日期 2004.07.16
申请人 SNECMA PROPULSION SOLIDE 发明人 THEBAULT, JACQUES;DAVID, LAURENT
分类号 B32B18/00;C04B35/571;C04B35/83;C04B41/52;C04B41/89;C04B111/00;C04B111/40;C04B111/80;C08F2/38;(IPC1-7):B32B18/00 主分类号 B32B18/00
代理机构 代理人
主权项
地址