Invention Grant
- Patent Title: Segmented cooling air cavity for turbine component
- Patent Title (中): 用于涡轮机部件的分段冷却空气腔
-
Application No.: US11861662Application Date: 2007-09-26
-
Publication No.: US08128348B2Publication Date: 2012-03-06
- Inventor: Paul M. Lutjen , Susan M. Tholen
- Applicant: Paul M. Lutjen , Susan M. Tholen
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, PC
- Main IPC: F01D11/08
- IPC: F01D11/08
Abstract:
A component for a gas turbine engine has an airfoil with internal cooling channels for delivering air from a radially outer end of the airfoil toward a radially inner end of the airfoil. The cooling channels are separated from adjacent cooling channels by sets of at least two disconnected wall segments.
Public/Granted literature
- US20090081025A1 SEGMENTED COOLING AIR CAVITY FOR TURBINE COMPONENT Public/Granted day:2009-03-26
Information query
