发明名称 |
THERMALLY ACTUATED ASSEMBLY FOR A GAS TURBINE SYSTEM AND METHOD OF CONTROLLING A COOLING AIRFLOW PATH |
摘要 |
A thermally actuated assembly for a gas turbine assembly for a gas turbine system includes a heat transfer component having a first portion and a second portion, wherein the first portion is disposed within a first cavity having a first temperature and the second portion is disposed in a second cavity having a second temperature, wherein the heat transfer component extends through a cavity wall, wherein the first temperature is greater than the second temperature. Also included is a temperature sensitive element disposed within the second cavity and in operable communication with the heat transfer component. Further included is a flow manipulating device disposed within the second cavity and configured to displace in response to a temperature change in the first cavity. |
申请公布号 |
US2013330168(A1) |
申请公布日期 |
2013.12.12 |
申请号 |
US201213494688 |
申请日期 |
2012.06.12 |
申请人 |
LIOTTA GARY CHARLES;MIRANDA CARLOS MIGUEL;GENERAL ELECTRIC COMPANY |
发明人 |
LIOTTA GARY CHARLES;MIRANDA CARLOS MIGUEL |
分类号 |
F01D25/12;F01D25/00 |
主分类号 |
F01D25/12 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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