Invention Grant
- Patent Title: Method for building a gas turbine engine component
- Patent Title (中): 燃气涡轮发动机部件的构成方法
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Application No.: US14460633Application Date: 2014-08-15
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Publication No.: US09359897B2Publication Date: 2016-06-07
- Inventor: Gerald J. Bruck , Ahmed Kamel
- Applicant: Siemens Energy, Inc.
- Applicant Address: US FL Orlando
- Assignee: SIEMENS ENERGY, INC.
- Current Assignee: SIEMENS ENERGY, INC.
- Current Assignee Address: US FL Orlando
- Main IPC: B23K9/04
- IPC: B23K9/04 ; F01D5/00 ; B23K26/06 ; B23K26/34 ; B23K15/00 ; B23P6/00

Abstract:
A method, including: providing a layer of powder material (156) on a substrate (130); and traversing an energy beam (15) across the layer of powder material to form a cladding layer (10), wherein the cladding layer forms a layer of an airfoil. The traversing step includes: starting a first path (40) and a second path (44) of traversal of the energy beam from a common initiation point (48); forming a portion (60) of a first side wall (18) of the cladding layer and a first rib section (24) by traversing the energy beam along the first path and concurrently forming a portion (62) of a second side wall (16) of the cladding layer by traversing the energy beam along the second path; and creating not more than one initiation point (72, 96, 118) for each rib section (24, 26, 28) in the cladding layer.
Public/Granted literature
- US20160045989A1 METHOD FOR BUILDING A GAS TURBINE ENGINE COMPONENT Public/Granted day:2016-02-18
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