| 发明名称 |
DUAL FUEL AIRCRAFT ENGINE CONTROL SYSTEM AND METHOD FOR OPERATING SAME |
| 摘要 |
A dual fuel engine control system comprising a first fuel control system configured to control the flow of a first fuel to an aircraft gas turbine engine, and a second fuel control system configured to control the flow of a second fuel to the aircraft gas turbine engine. |
| 申请公布号 |
EP2622193(A1) |
申请公布日期 |
2013.08.07 |
| 申请号 |
EP20110770294 |
申请日期 |
2011.09.30 |
| 申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
KAMATH, DEEPAK, MANOHAR;LEIGHTON, DAVID, MARK;MORTON, SCOTT, CHANDLER |
| 分类号 |
F02C9/40;F02C7/228;F23R3/36 |
主分类号 |
F02C9/40 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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