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公开(公告)号:US10677259B2
公开(公告)日:2020-06-09
申请号:US15148631
申请日:2016-05-06
Applicant: General Electric Company
Inventor: Nitesh Jain , Vikulp Sharma , Nicholas Joseph Kray
Abstract: A metal leading edge includes a nose positioned along the leading edge of a fan blade airfoil body. The metal leading edge also includes a first edge extending axially aftward from the nose along a pressure side of the fan blade airfoil body. The metal leading edge further includes a second edge extending axially aftward from the nose along a suction side of the fan blade airfoil body. The first edge and the second edge forming a notch at the conjunction of the first edge, the second edge, and the nose. The metal leading edge also includes a nose length extending from a nose tip to the notch. The nose length at a first radial location is different from the nose length at a second radial location.
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公开(公告)号:US20170321714A1
公开(公告)日:2017-11-09
申请号:US15148631
申请日:2016-05-06
Applicant: General Electric Company
Inventor: Nitesh Jain , Vikulp Sharma , Nicholas Joseph Kray
Abstract: A metal leading edge includes a nose positioned along the leading edge of a fan blade airfoil body. The metal leading edge also includes a first edge extending axially aftward from the nose along a pressure side of the fan blade airfoil body. The metal leading edge further includes a second edge extending axially aftward from the nose along a suction side of the fan blade airfoil body. The first edge and the second edge forming a notch at the conjunction of the first edge, the second edge, and the nose. The metal leading edge also includes a nose length extending from a nose tip to the notch. The nose length at a first radial location is different from the nose length at a second radial location.
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