Invention Grant
- Patent Title: Method of manufacturing gas turbine engine component from a molybdenum-rich alloy
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Application No.: US14849644Application Date: 2015-09-10
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Publication No.: US10335857B2Publication Date: 2019-07-02
- Inventor: John P. Rizzo, Jr.
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: B21J5/00
- IPC: B21J5/00 ; C22F1/18 ; F01D5/28 ; B23K20/10 ; B22F3/20 ; B23K26/352 ; B22F1/00 ; B22F3/17 ; C22C1/04 ; B22F9/16 ; B23H7/00 ; C22C27/04 ; C22C32/00 ; F01D25/00
Abstract:
A method for manufacturing a gas turbine engine component from a molybdenum-rich alloy. The method includes the steps of providing a molybdenum powder of at least 50% molybdenum by weight, extruding the molybdenum powder to provide a first shape, forming the first shape to a second shape and forging the second shape to provide a third shape.
Public/Granted literature
- US20160089722A1 METHOD OF MANUFACTURING GAS TURBINE ENGINE COMPONENT FROM A MOLYBDENUM-RICH ALLOY Public/Granted day:2016-03-31
Information query
