| 发明名称 |
CASE AND LINER ARRANGEMENT FOR A COMBUSTOR |
| 摘要 |
A combustor adapted for use in a gas turbine engine is disclosed. The combustor includes a metallic case forming a cavity and a ceramic liner arranged in the cavity of the metallic case. The ceramic liner defines a combustion chamber in which fuel is burned during operation of a gas turbine engine. The ceramic liner is located in the metallic case using a plurality of cross key connectors. |
| 申请公布号 |
US2017051917(A1) |
申请公布日期 |
2017.02.23 |
| 申请号 |
US201615214865 |
申请日期 |
2016.07.20 |
| 申请人 |
Rolls-Royce Corporation ;Rolls-Royce North American Technologies, Inc. |
发明人 |
Varney Bruce E.;Freeman Ted J.;Chamberlain Adam L. |
| 分类号 |
F23R3/00 |
主分类号 |
F23R3/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A combustor for use in a gas turbine engine, the combustor comprising
a case comprising metallic materials adapted to be mounted in a gas turbine engine and formed to define an interior space, a combustion liner comprising ceramic matrix composite materials arranged in the interior space of the case, the combustion liner shaped to define a combustion chamber within the case and shield at least a portion of the case from the combustion chamber, and a plurality of pins that extend through the case and into blind holes formed in the combustion liner to provide cross key connections between the case and the combustion liner locating the combustion liner relative to the case. |
| 地址 |
Indianapolis IN US |
