| 发明名称 |
ORIENTATION FEATURE FOR SWIRLER TUBE |
| 摘要 |
A cooling structure for a gas turbine engine comprises a gas turbine engine structure defining a cooling cavity. A cooling component is configured to direct cooling flow in a desired direction into the cooling cavity. A bracket supports the cooling component and has an attachment interface to fix the bracket to the gas turbine engine structure. A first orientation feature associated with the bracket. A second orientation feature is associated with the gas turbine engine structure. The first and second orientation features cooperate with each other to ensure that the cooling component is only installed in one orientation relative to the gas turbine engine structure. A gas turbine engine and a method of installing a cooling structure are also disclosed. |
| 申请公布号 |
US2016230666(A1) |
申请公布日期 |
2016.08.11 |
| 申请号 |
US201514617109 |
申请日期 |
2015.02.09 |
| 申请人 |
United Technologies Corporation |
发明人 |
Zacchera Kevin;Hough Matthew Andrew;Lemoine Jonathan;Treat Christopher;Mateo Alberto A. |
| 分类号 |
F02C7/20;F02C7/12 |
主分类号 |
F02C7/20 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A cooling structure for a gas turbine engine comprising:
a gas turbine engine structure defining a cooling cavity; a cooling component configured to direct cooling flow in a desired direction into the cooling cavity; a bracket supporting the cooling component and having an attachment interface to fix the bracket to the gas turbine engine structure; a first orientation feature associated with the bracket; and a second orientation feature associated with the gas turbine engine structure, the first and second orientation features cooperating with each other to ensure that the cooling component is only installed in one orientation relative to the gas turbine engine structure. |
| 地址 |
Hartford CT US |
