Invention Grant
- Patent Title: Combustor apparatus in a gas turbine engine
- Patent Title (中): 燃气涡轮发动机中的燃烧器装置
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Application No.: US13928476Application Date: 2013-06-27
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Publication No.: US09322558B2Publication Date: 2016-04-26
- Inventor: Stephen A. Ramier , David J. Wiebe , Lawrence P. Budnick , Mark L. Adamson , Daniel W. Garan , Robert H. Bartley , Yadollah Naghian
- Applicant: Stephen A. Ramier , David J. Wiebe , Lawrence P. Budnick , Mark L. Adamson , Daniel W. Garan , Robert H. Bartley , Yadollah Naghian
- Applicant Address: DE München
- Assignee: SIEMENS AKTIENGESELLSCHAFT
- Current Assignee: SIEMENS AKTIENGESELLSCHAFT
- Current Assignee Address: DE München
- Main IPC: F23R3/60
- IPC: F23R3/60 ; F23R3/28 ; F23R3/54 ; F16L19/06 ; F23R3/34

Abstract:
A combustor apparatus defining a combustion zone where air and fuel are burned to create high temperature combustion products. The combustor apparatus comprises an outer wall including a fuel inlet opening for receiving a fuel feed pipe. A coupling assembly is engaged with the fuel feed pipe at the fuel inlet opening to attach the fuel feed pipe to the outer wall. A fuel injection system is located in the interior volume of the outer wall and comprises fuel supply structure including a fuel feed block having a fuel intake passage aligned with the outlet portion of the fuel feed pipe. A coupling fastener is engaged against an exterior outer face of the fuel feed block to create a sealed coupling for containing fuel passing from the fuel feed pipe into the fuel feed block, and to secure the fuel feed block relative to the coupling assembly.
Public/Granted literature
- US20150000283A1 COMBUSTOR APPARATUS IN A GAS TURBINE ENGINE Public/Granted day:2015-01-01
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