Invention Grant
- Patent Title: Turbine blade
-
Application No.: US14884100Application Date: 2015-10-15
-
Publication No.: US10443398B2Publication Date: 2019-10-15
- Inventor: Matthew Lee Krumanaker , Weston Nolan Dooley , Steven Robert Brassfield
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: McGarry Bair PC
- Main IPC: F01D5/18
- IPC: F01D5/18 ; F01D5/14 ; F01D5/20
Abstract:
An airfoil for a gas turbine engine comprises a cooling circuit defined within the airfoil providing a flow of cooling fluid within the airfoil. The cooling circuit exhausts the flow of cooling fluid out a slot opening comprising an airfoil element. The slot opening further defines an acceleration zone and a deceleration zone to meter the flow of cooling fluid within the airfoil.
Public/Granted literature
- US20170107828A1 TURBINE BLADE Public/Granted day:2017-04-20
Information query
