发明名称 CMCで作られたタービンディストリビュータ要素、タービンディストリビュータ要素の製造方法、ディストリビュータ、およびディストリビュータを含むガスタービン
摘要 <p>A turbine nozzle element including an inner annular platform sector, an outer annular platform sector, and at least one vane extending between the platform sectors and connected to both of them. The nozzle element includes a single piece of composite material including fiber reinforcement densified by a matrix that is at least partially ceramic, and the fiber reinforcement includes a fiber structure that is woven by three-dimensional or multi-layer weaving, and that presents continuity throughout the volume of the nozzle element and throughout the periphery of the vane.</p>
申请公布号 JP5730864(B2) 申请公布日期 2015.06.10
申请号 JP20120515542 申请日期 2010.06.09
申请人 发明人
分类号 F01D25/24;C04B35/80;F01D9/02;F01D9/04 主分类号 F01D25/24
代理机构 代理人
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