Invention Grant
- Patent Title: Turbine nozzle segment
- Patent Title (中): 涡轮喷嘴段
-
Application No.: US11967177Application Date: 2007-12-29
-
Publication No.: US08235652B2Publication Date: 2012-08-07
- Inventor: Mark Broomer , Victor Hugo Silva Correia
- Applicant: Mark Broomer , Victor Hugo Silva Correia
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: General Electric Company
- Agent David J. Clement; William Scott Andes
- Main IPC: F01D9/06
- IPC: F01D9/06
Abstract:
A turbine nozzle segment includes a band having a flowpath side and a non-flowpath side and an enclosure disposed on the non-flowpath side of the band. A plenum may be defined between the band and the enclosure and a discourager may extend from the enclosure.
Public/Granted literature
- US20090169360A1 Turbine Nozzle Segment Public/Granted day:2009-07-02
Information query
