| 发明名称 |
TURBINE COMPONENT SURFACE COOLING SYSTEM WITH PASSIVE FLOW MODULATION |
| 摘要 |
A system according to various embodiments includes: a cooling network within a turbine component, the cooling network including at least one passageway fluidly connected with a surface of the turbine component; a cooling fluid source for providing a cooling fluid to the cooling network; and a temperature-actuated flow modulating device fluidly connected with the cooling fluid source and the cooling network, the temperature-actuated flow modulating device configured to: detect an ambient air temperature proximate the turbine component; and control a flow of the cooling fluid to the cooling network based upon the detected ambient air temperature. |
| 申请公布号 |
US2017044914(A1) |
申请公布日期 |
2017.02.16 |
| 申请号 |
US201514825553 |
申请日期 |
2015.08.13 |
| 申请人 |
General Electric Company |
发明人 |
Miranda Carlos Miguel;Lacy Benjamin Paul;Rubinsztajn Slawomir |
| 分类号 |
F01D9/06;F02C7/12;F01D25/12 |
主分类号 |
F01D9/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system comprising:
a cooling network within a turbine component, the cooling network including at least one passageway fluidly connected with a surface of the turbine component; a cooling fluid source for providing a cooling fluid to the cooling network; and a temperature-actuated flow modulating device fluidly connected with the cooling fluid source and the cooling network, the temperature-actuated flow modulating device configured to:
detect a temperature of an ambient air temperature proximate the turbine component; andcontrol a flow of the cooling fluid to the cooling network based upon the detected ambient air temperature. |
| 地址 |
Schenectady NY US |
