发明申请
US20080098736A1 COMBUSTOR AND MULTI COMBUSTOR INCLUDING THE COMBUSTOR, AND COMBUSTING METHOD
有权
COMBUSTOR和多个燃烧器,包括燃烧器和燃烧方法
- 专利标题: COMBUSTOR AND MULTI COMBUSTOR INCLUDING THE COMBUSTOR, AND COMBUSTING METHOD
- 专利标题(中): COMBUSTOR和多个燃烧器,包括燃烧器和燃烧方法
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申请号: US11928522申请日: 2007-10-30
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公开(公告)号: US20080098736A1公开(公告)日: 2008-05-01
- 发明人: Min-Chul LEE , Jae-Hwa Chung , Seok-Bin Seo , Yong-Jin Joo , Jong-Jin Kim , Dal-Hong Ahn
- 申请人: Min-Chul LEE , Jae-Hwa Chung , Seok-Bin Seo , Yong-Jin Joo , Jong-Jin Kim , Dal-Hong Ahn
- 优先权: KR10-2006-0106423 20061031
- 主分类号: F02C9/26
- IPC分类号: F02C9/26 ; F23R3/04
摘要:
A dual fuel nozzle of a gas turbine combustor with a variable jetting hole diameter is disclosed. The combustor includes a plurality of swirling wings disposed along an outer peripheral surface of a central shaft to have at least one main fuel jetting hole, an air duct positioned at the lower side of the swirling wings to supply air to the swirling wings, a pilot fuel injection hole and jetting hole formed to pass through a central portion of the central shaft to supply a pilot fuel, a switching plate disposed inside the swirling wings to vary the size of the main fuel jetting hole, a driving unit disposed to be connected to the switching plate to move a position of the switching plate, and a casing containing the swirling wings, the air duct, the switching plate and the driving unit. It is possible to enhance fuel flexibility in a multiple fuel system for applying two or more fuels to a gas turbine at the same time.