Invention Grant
- Patent Title: Dual fuel combustor nozzle for a turbomachine
- Patent Title (中): 用于涡轮机的双燃料燃烧器喷嘴
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Application No.: US12563491Application Date: 2009-09-21
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Publication No.: US08365536B2Publication Date: 2013-02-05
- Inventor: Abdul Rafey Khan , Christian Xavier Stevenson , Baifang Zuo
- Applicant: Abdul Rafey Khan , Christian Xavier Stevenson , Baifang Zuo
- 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

Abstract:
A dual fuel combustor nozzle includes a body member including a first end portion that extends to a second end portion through an intermediate portion. The intermediate portion includes an outer wall portion and an inner wall portion with the inner wall portion defining a first fuel plenum. The dual fuel nozzle also includes an inner nozzle member arranged within the first fuel plenum. The inner nozzle member includes a first end section that extends to a second end section through an intermediate section. The intermediate section defines a second fuel plenum. The second end section being spaced from the second end portion of the body member so as to define a pre-emergence zone.
Public/Granted literature
- US20110067379A1 DUAL FUEL COMBUSTOR NOZZLE FOR A TURBOMACHINE Public/Granted day:2011-03-24
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