发明名称 |
THERMALLY ISOLATED TURBINE SHROUD ASSEMBLY |
摘要 |
In one aspect the present subject matter is directed to a system (100) for thermally isolating a turbine shroud (102) of a turbine shroud assembly (104). The system (100) includes a shroud support (106) having an inner surface (108) and a turbine shroud (102) that is connected to the shroud support (106). The turbine shroud (102) includes a hot side surface (114) that is radially spaced from a back side surface (116). At least a portion of the back side surface (116) is oriented towards the inner surface (108) of the shroud support (106). The system (100) further includes a coating (126) that is disposed along the back side surface (116) of the turbine shroud (102). The coating (126) regulates heat transfer from the turbine shroud (102) to the shroud support (106) or other hardware that may surround or be adjacent to the turbine shroud (102). |
申请公布号 |
EP3093448(A1) |
申请公布日期 |
2016.11.16 |
申请号 |
EP20160168869 |
申请日期 |
2016.05.10 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
TURA, CHRISTOPHER PAUL;FITZPATRICK, DYLAN JAMES |
分类号 |
F01D11/08;F01D9/04 |
主分类号 |
F01D11/08 |
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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