Invention Grant
US08474266B2 System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle
有权
具有从扩散器到燃料喷嘴的排放管的燃气轮机燃烧器的系统和方法
- Patent Title: System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle
- Patent Title (中): 具有从扩散器到燃料喷嘴的排放管的燃气轮机燃烧器的系统和方法
-
Application No.: US12508918Application Date: 2009-07-24
-
Publication No.: US08474266B2Publication Date: 2013-07-02
- Inventor: Jonathan Dwight Berry , Geoffrey David Myers
- Applicant: Jonathan Dwight Berry , Geoffrey David Myers
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Cantor Colburn LLP
- Main IPC: F02C1/00
- IPC: F02C1/00 ; F02C6/04 ; F02C7/20 ; F02G3/00
Abstract:
A gas turbine system comprising, a diffuser operative to diffuse an airstream output from a compressor, a fuel nozzle operative to receive fuel and emit the fuel in a combustor, and at least one bleed duct operative to direct bleed air from down stream of the combustor to the fuel nozzle.
Public/Granted literature
- US20110016878A1 Systems and Methods for Gas Turbine Combustors Public/Granted day:2011-01-27
Information query
