发明名称 SYSTEM AND METHOD FOR SUPPORTING A TURBINE SHROUD
摘要 In one aspect the present subject matter is directed to a system for supporting a turbine shroud. The system includes a shroud support at least partially defining a first piston sleeve and a piston assembly having a first piston head disposed within the first piston sleeve and a second piston head coupled to the first piston head. The first piston head is slideably engaged with an inner surface of the first piston sleeve. The second piston head is slideably engaged with an inner surface of a second piston sleeve. The system also includes a turbine shroud that is fixedly connected to the piston assembly and that extends radially inwardly from the shroud support. The piston assembly provides for radially inward and radially outward movement of the turbine shroud in response to a change in a radial force applied to a hot side surface of the turbine shroud.
申请公布号 US2017044922(A1) 申请公布日期 2017.02.16
申请号 US201514825201 申请日期 2015.08.13
申请人 General Electric Company 发明人 Shapiro Jason David
分类号 F01D11/16;F01D9/04;F01D5/12 主分类号 F01D11/16
代理机构 代理人
主权项 1. A system for supporting a turbine shroud, the system comprising: a shroud support, the shroud support at least partially defining a first piston sleeve therein; a piston assembly having a first piston head disposed within the first piston sleeve and a second piston head coupled to the first piston head, wherein the first piston head is slideably engaged with an inner surface of the first piston sleeve, wherein the second piston head is slideably engaged with an inner surface of a second piston sleeve; and a turbine shroud fixedly connected to the piston assembly and extending radially inwardly from the shroud support, wherein the piston assembly provides for radially inward and radially outward movement of the turbine shroud in response to a radially outward force applied to a hot side surface of the turbine shroud.
地址 Schenectady NY US