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发明名称
用于航空器涡轮喷射引擎之喷嘴襟翼及其制造方法
摘要
一种用于航空器涡轮喷射引擎之喷嘴襟翼,该喷嘴襟翼系具有一个扁平中空、且向两侧呈渐缩状态的本体。该本体系具有固定厚度之薄壁,且该本体系包括具有最少2倍厚度的弯曲半径之内表面;该本体系由耐火材料制成,该耐火材料系包括与连续性之加强纤维交叉之镶埋于耐火基质里的耐火纤维,其耐火纤维与加强纤维系由两种不同之耐火材料制成。
申请公布号
TW200505744
申请公布日期
2005.02.16
申请号
TW093114967
申请日期
2004.05.26
申请人
斯奈克玛发动机公司
发明人
潘谷 地希;巴雷 赫;科宾 柯罗德;布浓夏 史帝芬
分类号
B64D33/04;D03D11/00
主分类号
B64D33/04
代理机构
代理人
谢宗颖;王云平
主权项
地址
法国
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