| 发明名称 |
COMBUSTOR CONFIGURATIONS FOR A GAS TURBINE ENGINE |
| 摘要 |
The present disclosure relates to combustor configurations and components for a gas turbine engine. In one embodiment, a combustor for a gas turbine engine includes a support structure and a plurality of panels mounted to the structure. The plurality of panels define a combustion cavity of the combustor. The plurality of panels include a first panel having a leading and trailing edge, and a second panel having a leading edge and trailing edge, wherein a trailing edge of the first panel extends beyond the leading edge of the second panel and wherein the second panel is mounted to the support structure aft of the first panel. |
| 申请公布号 |
US2016290642(A1) |
申请公布日期 |
2016.10.06 |
| 申请号 |
US201514673629 |
申请日期 |
2015.03.30 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
KWOKA David;REZVANI Reza;EASTWOOD Jonathan Jeffery |
| 分类号 |
F23R3/00;F23R3/44;F23R3/06 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A combustor for a gas turbine engine, the combustor comprising:
a support structure; and a plurality of panels mounted to the structure, the plurality of panels defining a combustion cavity of the combustor, wherein the plurality of panels include
a first panel having a leading and trailing edge, anda second panel having a leading edge and trailing edge, wherein a trailing edge of the first panel extends beyond the leading edge of the second panel and wherein the second panel is mounted to the support structure aft of the first panel. |
| 地址 |
Farmington CT US |
