发明名称 Cooling circuit for reducing thermal growth differential of turbine rotor and shell supports
摘要 A standard for supporting a turbine rotor and a turbine shell includes a bearing block including a housing enclosing bearing surfaces engageable by the turbine rotor. Turbine shell-arm supports are located on opposite sides of the housing, the turbine shell-arm supports each having a horizontal and one or more vertical surfaces adapted to be engaged by support arms of a turbine shell enclosing at least a portion of the turbine. An internal cooling/heating circuit is arranged to simultaneously cool or heat the bearing block and the turbine shell-arm supports to thereby reduce differential thermal growth characteristics of the turbine rotor and turbine shell.
申请公布号 US9376934(B2) 申请公布日期 2016.06.28
申请号 US201213594609 申请日期 2012.08.24
申请人 General Electric Company 发明人 Cooper Edward Jay;Eizenzopf Peter John;Zheng Xiaoqing;Rusch William Patrick;Kumar Hemanth GS;Ivancic Craig Daniel;Sharrow Edward John
分类号 F01D25/12;F01D25/14;F01D25/16;F01D25/24 主分类号 F01D25/12
代理机构 Nixon & Vanderhye P.C. 代理人 Nixon & Vanderhye P.C.
主权项 1. A standard for supporting a turbine rotor and a turbine shell comprising: a bearing block including a housing enclosing bearing surfaces engageable by the turbine rotor; turbine shell-arm supports on opposite sides of said housing, said turbine shell-arm supports each having a horizontal and one or more vertical surfaces adapted to be engaged by support arms of a turbine shell enclosing at least a portion of the turbine; and a cooling/heating circuit utilizing a heat exchange medium arranged to simultaneously cool or heat the bearing block and the turbine shell-arm supports to thereby reduce differential thermal growth characteristics of the turbine rotor and turbine shell.
地址 Schenectady NY US