| 发明名称 |
MODIFIED FLOATWALL PANEL DILUTION HOLE COOLING |
| 摘要 |
Aspects of the disclosure are directed to a liner of an aircraft. The liner comprises a panel including at least one dilution hole, a rail coupled to the panel, and at least one effusion cooling hole located between a wall of the at least one dilution hole and a side of the rail. The liner may be associated with a combustion engine of the aircraft. |
| 申请公布号 |
US2016265777(A1) |
申请公布日期 |
2016.09.15 |
| 申请号 |
US201514884506 |
申请日期 |
2015.10.15 |
| 申请人 |
United Technologies Corporation |
发明人 |
Hoke James B.;Kwoka David |
| 分类号 |
F23R3/06;F23R3/60;F23R3/00 |
主分类号 |
F23R3/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A liner of an aircraft, comprising:
a panel including at least one dilution hole; a rail coupled to the panel; and at least one effusion cooling hole located between a wall of the at least one dilution hole and a side of the rail. |
| 地址 |
Hartford CT US |
