发明名称 System, method, and apparatus for leading edge structures and direct manufacturing thereof
摘要 Leading edge structures for high performance aircraft and the direct manufacture thereof are disclosed. Direct manufacturing technology is used to deposit leading edge structures directly from a digital model to form near-net shape products. This technique permits a wider range of materials to be utilized, such as casting alloys capable of the highest temperature usage that are not available in billet or sheet form. Refractory metals or high temperature ceramics also may be used to form the entire lead edge structure, or just a replaceable tip of the leading edge structure.
申请公布号 US7871041(B2) 申请公布日期 2011.01.18
申请号 US20070873439 申请日期 2007.10.17
申请人 LOCKHEED MARTIN CORPORATION 发明人 BRICE CRAIG A.;ROSENBERGER BRIAN T.
分类号 B64C1/00 主分类号 B64C1/00
代理机构 代理人
主权项
地址