发明名称 |
COMBUSTOR DOME HEAT SHIELD |
摘要 |
A combustor heat shield has lips with fins distributed on the lips. The lip-fins have an extended end portion projecting rearwardly from the back face of the heat shield. Impingement jets may be directed against the rearwardly extended end portions of the lip-fins to enhance cooling. The heat shield may define a fuel nozzle opening surrounded by a rail on the back side of the heat shield. Impingement holes or slots may be defined in the rail for allowing cooling air passing therethrough to impinge upon the lip-fins. |
申请公布号 |
US2015135720(A1) |
申请公布日期 |
2015.05.21 |
申请号 |
US201314085011 |
申请日期 |
2013.11.20 |
申请人 |
Pratt & Whitney Canada Corp. |
发明人 |
PAPPLE MICHAEL;SZE ROBERT;SREEKANTH SRI |
分类号 |
F23R3/16;F23R3/00 |
主分类号 |
F23R3/16 |
代理机构 |
|
代理人 |
|
主权项 |
1. A heat shield for a combustor of a gas turbine engine, comprising a heat shield panel adapted to be mounted to an inside of a dome of the combustor with a back face of the heat shield panel in spaced-apart facing relationship with an inner surface of the dome, the heat shield configured to receive a flow of cooling air along said back face, at least one radially inner or outer lip along a periphery and projecting downstream of the heat shield panel relative to the flow of cooling air, an array of lip-fins provided on the at least one of the radially inner or outer lip, the lip-fins having extended end portions projecting upstream from the back face of the heat shield panel. |
地址 |
Longueuil CA |