Invention Grant
US06382913B1 Method and apparatus for reducing turbine blade tip region temperatures
失效
降低涡轮叶片尖端区域温度的方法和装置
- Patent Title: Method and apparatus for reducing turbine blade tip region temperatures
- Patent Title (中): 降低涡轮叶片尖端区域温度的方法和装置
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Application No.: US09783279Application Date: 2001-02-09
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Publication No.: US06382913B1Publication Date: 2002-05-07
- Inventor: Ching-Pang Lee , Chander Prakash
- Applicant: Ching-Pang Lee , Chander Prakash
- Main IPC: F01D518
- IPC: F01D518

Abstract:
A rotor blade for a gas turbine engine including a tip region that facilitates reducing operating temperatures of the rotor blade is described. The tip region includes a first tip wall and a second tip wall extending radially outward from a tip plate of an airfoil. The tip walls extend from adjacent a leading edge of the airfoil to connect at a trailing edge of the airfoil. A portion of the second tip wall is recessed to define a tip shelf that extends from the airfoil leading edge to the airfoil trailing edge.
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