Invention Application
- Patent Title: Maxmet Composites for Turbine Engine Component Tips
- Patent Title (中): Maxmet复合材料涡轮发动机组件提示
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Application No.: US14775927Application Date: 2013-12-16
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Publication No.: US20160024955A1Publication Date: 2016-01-28
- Inventor: Shahram Amini , Christopher W Strock , Sergei F Burlatsky , Dmitri Novikov , David Ulrich Fuller
- Applicant: UNITED TECHNOLOGIES CORPORATION
- International Application: PCT/US2013/075292 WO 20131216
- Main IPC: F01D11/12
- IPC: F01D11/12 ; F01D9/04 ; B23K1/00 ; B23K1/19 ; C23C24/04 ; B23K20/22 ; B23K26/34 ; B23K26/00 ; C23C4/12 ; F01D5/28 ; B23K20/02
Abstract:
A turbine engine system includes a turbine engine component having an airfoil portion and a tip, which turbine engine component having a MAXMET composite bonded to the tip. The MAXMET composite has MAX phases in a metal matrix.
Information query
