Invention Grant
- Patent Title: Method of manufacturing a turbine fan blade
- Patent Title (中): 制造涡轮风扇叶片的方法
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Application No.: US11967484Application Date: 2007-12-31
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Publication No.: US07805839B2Publication Date: 2010-10-05
- Inventor: Jerald C Cammer
- Applicant: Jerald C Cammer
- Applicant Address: US GA Thomasville
- Assignee: Turbine Engine Components Technologies Corporation
- Current Assignee: Turbine Engine Components Technologies Corporation
- Current Assignee Address: US GA Thomasville
- Agent Jones Day
- Main IPC: B21D53/78
- IPC: B21D53/78

Abstract:
A metal leading edge of a turbine fan blade is manufactured by cutting and shaping an elongated metal part. The metal part has front and rear edges extending lengthwise of the part, and has a generally wedge-shaped transverse cross-section with opposite sides diverging from the front edge toward the rear edge. A cavity is cut inward from the rear edge toward the front edge. This provides the part with a generally V-shaped transverse cross-section having opposite side walls diverging rearwardly from the front edge. A mandrel is inserted into the cavity, and the side walls of the V-shaped part are deflected toward each other to constrict the cavity into the configuration of the mandrel. The part is then mounted as a metal leading edge by inserting a turbine fan blade component into the constricted cavity and fastening the part to the component.
Public/Granted literature
- US20090165299A1 Method of Manufacturing a Turbine Fan Blade Public/Granted day:2009-07-02
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