Invention Application
- Patent Title: AIRFOIL HAVING INTEGRAL FINS
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Application No.: US15891401Application Date: 2018-02-08
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Publication No.: US20200149399A1Publication Date: 2020-05-14
- Inventor: Nicholas Joseph Kray , Nitesh Jain , Nagashiresha Gontla , Narendra Digamber Joshi , Paul Gerard Marsland , Wayne Allen Spence
- Applicant: GENERAL ELECTRIC COMPANY
- Main IPC: F01D5/12
- IPC: F01D5/12 ; F01D5/30

Abstract:
A blade and a turbomachine engine having the blade are disclosed. The blade includes an airfoil having a root portion, a tip portion, and a plurality of fins integrally coupled to the root portion. The plurality of fins is disposed along a thickness of the airfoil.
Public/Granted literature
- US10724376B2 Airfoil having integral fins Public/Granted day:2020-07-28
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