发明名称 |
Gas turbine combustion chamber with fuel injection over the whole combustion chamber ring |
摘要 |
<p>A gas turbine engine has one or more annular combustion chambers each with one or more fuel injection jets. The front end of each annular combustion chamber has a circular array of vortex generators around the combustion chamber center axis. The fuel jets are located essentially at uniform intervals around the combustion chamber ring.</p> |
申请公布号 |
EP1816400(A2) |
申请公布日期 |
2007.08.08 |
申请号 |
EP20070001760 |
申请日期 |
2007.01.26 |
申请人 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG |
发明人 |
BECKER, JOCHEN |
分类号 |
F23R3/50;F23R3/10 |
主分类号 |
F23R3/50 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|