发明授权
- 专利标题： Turbine engine fuel injector
- 专利标题（中）： 涡轮发动机燃油喷射器
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申请号： US10691791申请日： 2003-10-23
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公开(公告)号： US06935117B2公开(公告)日： 2005-08-30
- 发明人: Curtis C. Cowan
- 申请人： Curtis C. Cowan
- 申请人地址： US CT Hartford
- 专利权人： United Technologies Corporation
- 当前专利权人： United Technologies Corporation
- 当前专利权人地址： US CT Hartford
- 代理机构： Bachman & LaPointe, P.C.
- 主分类号： F02C7/22
- IPC分类号： F02C7/22 ; F02C7/224 ; F23D11/10 ; F23D17/00 ; F23R3/28 ; F23R3/30 ; F23R3/34 ; F23R3/36
摘要：
A gas turbine engine is piloted with a pilot flow of fuel delivered to a combustor as a liquid. A first additional flow of the fuel is also delivered to the combustor as a liquid. A second additional flow of the fuel is vaporized and delivered to the combustor as a vapor. A fuel injector may have passageways associated with each of the three flows.
公开/授权文献
- US20050086944A1 Turbine engine fuel injector 公开/授权日：2005-04-28