Invention Application
- Patent Title: ROTOR BLADE HAVING A FLARED TIP
- Patent Title (中): 带有刀尖的转子叶片
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Application No.: US14699321Application Date: 2015-04-29
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Publication No.: US20160319673A1Publication Date: 2016-11-03
- Inventor: Jeffrey Clarence Jones , Xiuzhang James Zhang , Mitchell Allan Merrill
- Applicant: General Electric Company
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F02C7/18 ; F02C3/04

Abstract:
A rotor blade includes an airfoil having a blade tip and a tip cavity formed at the blade tip. The tip cavity includes a tip cap that is recessed radially inwardly from the tip and surrounded continuously by pressure and suction side walls of the airfoil. The tip cap further includes an aperture that extends through the tip cap and provides for fluid communication between an internal cavity defined within the airfoil and the tip cavity. An exhaust port provides for fluid communication out the tip cavity through one of the pressure side wall, the suction side wall or the trailing edge. A portion of at least one of the suction side wall and the pressure side wall that defines the tip cavity extends obliquely outwardly from the tip cavity with respect to a radial direction.
Public/Granted literature
- US10107108B2 Rotor blade having a flared tip Public/Granted day:2018-10-23
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