Invention Grant
- Patent Title: Turbine engine airfoil with a modified leading edge
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Application No.: US15471729Application Date: 2017-03-28
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Publication No.: US11156099B2Publication Date: 2021-10-26
- Inventor: Nitesh Jain , Abhijeet Jayshingrao Yadav , Kishore Budumuru , Nicholas Joseph Kray
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Venable LLP
- Agent Michele V. Frank
- Main IPC: F01D5/14
- IPC: F01D5/14 ; F15D1/00 ; F01D25/02 ; F01D17/16
Abstract:
A turbine engine can comprise a fan section, compressor section, a combustion section, and a turbine section in axial flow arrangement. At least one of the fan section and compressor section can include an airfoil with a leading edge, and a plurality of riblets can be arranged on the leading edge.
Public/Granted literature
- US20180283180A1 TURBINE ENGINE AIRFOIL WITH A MODIFIED LEADING EDGE Public/Granted day:2018-10-04
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