发明授权
- 专利标题: Combustor for gas turbine engines with low air flow swirlers
- 专利标题(中): 具有低气流旋流器的燃气涡轮发动机燃烧器
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申请号: US09874854申请日: 2001-06-05
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公开(公告)号: US06487861B1公开(公告)日: 2002-12-03
- 发明人: Robert Gregory Carita , Irven Charles Ball , Frank Anthony Lastrina
- 申请人: Robert Gregory Carita , Irven Charles Ball , Frank Anthony Lastrina
- 主分类号: F02C100
- IPC分类号: F02C100
摘要:
A combustor for a gas turbine engine includes outer and inner liners defining a combustion chamber and an igniter mounted to the outer liner. A dome plate is disposed between the outer and inner liners and has a plurality of circumferentially spaced openings formed therein. A fuel-air mixer is disposed in each one of the openings; each fuel-air mixer includes a swirler mounted in the corresponding opening and a fuel nozzle received in the corresponding swirler. Two adjacent ones of the swirlers are low air flow swirlers in general circumferential alignment with the igniter and the rest of the swirlers are higher air flow swirlers. Each one of the fuel nozzles provides a similar amount of fuel so that the two fuel-air mixers having low air flow swirlers produce a local region of increased fuel-to-air ratio in the vicinity of the igniter.
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