发明名称 |
Flow conditioner for use in gas turbine component in which combustion occurs |
摘要 |
A gas turbine component in which combustion occurs. The gas turbine component includes a liner (10), including a first surface facing a first space (13) and a second surface facing a second space (14), the liner (10) being interposed between the first and second spaces (13,14) and having a through-hole (20) defined therein extending from the first to the second surface by which incoming flows proceed from the first space (13) and to the second space (14). At least the first surface is formed to flow condition the incoming flows to resist separating from sidewalls of the through-hole (20).
|
申请公布号 |
EP2211106(A2) |
申请公布日期 |
2010.07.28 |
申请号 |
EP20100151310 |
申请日期 |
2010.01.21 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
CHEN, WEI;CHILA, RONALD JAMES;KING, ERICK WILLIAM |
分类号 |
F23R3/06 |
主分类号 |
F23R3/06 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|