Invention Grant
- Patent Title: Fuel nozzle for gas turbine engine
-
Application No.: US14932187Application Date: 2015-11-04
-
Publication No.: US10196983B2Publication Date: 2019-02-05
- Inventor: John Michael Cadman , Thomas Ryan Wallace , Brian Matthias Schaldach , Randy Joseph Tobe
- 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: General Electric Company
- Agent Pamela Kachur
- Main IPC: F02C7/24
- IPC: F02C7/24 ; F02C7/22 ; F23R3/28

Abstract:
A fuel nozzle configured to channel fluid towards a combustion chamber is provided. The fuel nozzle includes a stem having a central passageway and at least one fuel tube disposed within the passageway. The fuel tube includes an outlet end portion having inner and outer walls separated by a cavity defined by a fixed aft face. The inner wall defines a central bore for delivering fuel to the combustion chamber. Further, the fuel nozzle includes an outer heat shield tube concentrically aligned with the outlet end portion of the fuel tube. The heat shield tube includes a circumferential outer wall having an aft face that stops upstream of the fixed aft face of the fuel tube. Thus, during operation, the heat shield tube is configured to thermally expand by sliding against the outer wall of the fuel tube.
Public/Granted literature
- US20170122212A1 FUEL NOZZLE FOR GAS TURBINE ENGINE Public/Granted day:2017-05-04
Information query
IPC分类: