Invention Grant
- Patent Title: Reverse cavity blade for a gas turbine engine
- Patent Title (中): 用于燃气涡轮发动机的反向腔叶片
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Application No.: US12843832Application Date: 2010-07-26
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Publication No.: US08740567B2Publication Date: 2014-06-03
- Inventor: Gabriel L. Suciu , James D. Hill , Gary M. Stetson
- Applicant: Gabriel L. Suciu , James D. Hill , Gary M. Stetson
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds P.C.
- Main IPC: F01D5/14
- IPC: F01D5/14 ; B23P15/02 ; F01D5/18 ; F01D5/22 ; F01D5/30
Abstract:
A rotor blade for a turbine engine includes an airfoil section which extends from a platform section opposite a root section, the airfoil section defines a cavity which extends from an airfoil tip section toward a root section.
Public/Granted literature
- US20120020805A1 REVERSE CAVITY BLADE FOR A GAS TURBINE ENGINE Public/Granted day:2012-01-26
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