发明授权
US5439750A Titanium metal matrix composite inserts for stiffening turbine engine
components
失效
用于加固涡轮发动机部件的钛金属基体复合材料刀片
- 专利标题: Titanium metal matrix composite inserts for stiffening turbine engine components
- 专利标题(中): 用于加固涡轮发动机部件的钛金属基体复合材料刀片
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申请号: US76670申请日: 1993-06-15
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公开(公告)号: US5439750A公开(公告)日: 1995-08-08
- 发明人: Richard Ravenhall , Charles R. Wojciechowski , Stephen C. Mitchell , Gary D. Mercer , Thomas J. Kelly , Melvin A. Schobert , Harvey M. Maclin
- 申请人: Richard Ravenhall , Charles R. Wojciechowski , Stephen C. Mitchell , Gary D. Mercer , Thomas J. Kelly , Melvin A. Schobert , Harvey M. Maclin
- 申请人地址: OH Cincinnati
- 专利权人: General Electric Company
- 当前专利权人: General Electric Company
- 当前专利权人地址: OH Cincinnati
- 主分类号: C22C1/10
- IPC分类号: C22C1/10 ; F01D5/28 ; B32B15/02
摘要:
A cast article having a reinforced structural composite core is disclosed. The cast article includes a structural element which is embedded in the otherwise cast metal article. The structural element is comprised of a metal matrix composite structural core. It includes a plurality of reinforcing fibers within a metal matrix. The fibers are generally a non-metallic material such as a ceramic which degrade at a temperature below the melting temperature of the cast metal comprising the article. The metal matrix composite structural core is encased with a sheath. The sheath, attached to and completely surrounding the core, is made of the same metal as the cast metal article. In a preferred embodiment, the article is a titanium alloy strut for a gas turbine engine.
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