发明名称 Integrally woven ceramic composites
摘要 <p>A woven preform for a ceramic composite has a plurality of layers and structural members. The plurality of layer are of woven yarns of fibrous material. The structural members extend between the layers. The layers and members define interlayer spaces. One or more of the layers may have a plurality of openings extending therethrough. Low density ceramic insulation made be deposited in the interlayer spaces via a slurry that enters the preform, or the preform after it has been made a part of a composite, through the openings. The carrier of the slurry exits the preform, leaving the randomly packed fibers in the interlayer spaces. The structural members may be walls that, along with the layers, define channels. The channels may be used to direct fluid through so as the composite functions as an insulator. The channels may be directed in the warp direction for achieving increased benefits. &lt;IMAGE&gt;</p>
申请公布号 EP1013412(B1) 申请公布日期 2011.11.30
申请号 EP19990204165 申请日期 1999.12.06
申请人 THE BOEING COMPANY 发明人 COX, BRIAN N.;MARSHALL, DAVID B.;DAVIS, JANET D.;BERBON, MIN Z.
分类号 B32B5/02;B32B5/26;C04B35/14;C04B35/185;C04B35/447;C04B35/571;C04B35/589;C04B35/622;C04B35/628;C04B35/80;C04B35/83;D01F9/08;D03D11/02;D03D13/00;D03D25/00;F02K1/82;F02K9/64;F02K9/97;F23M5/00 主分类号 B32B5/02
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