公开(公告)号：US20080317591A1

公开(公告)日：2008-12-25

申请号：US12018980

申请日：2008-01-24

申请人： Samuel Golinkin ,  Russell V. Caggiano ,  Timothy Ewer ,  Gennaro J. Diorio ,  Michael J. Lipski

发明人： Samuel Golinkin ,  Russell V. Caggiano ,  Timothy Ewer ,  Gennaro J. Diorio ,  Michael J. Lipski

IPC分类号： F01D25/26

CPC分类号： F01D25/28 ,  F05D2230/64

摘要： A centerline suspension arrangement (42) for a turbine (40). A turbine inner casing (44) is supported within an outer casing (46) via a support member (60) that includes an inner portion (62) contacting the inner casing and an outer portion (66) extending into a slot (68) formed in the outer casing. The support member is slid into an axially oriented slot (64) formed in the inner casing and is body bound therein with respect to radial movements, with the support member and the inner casing slot including opposed vertical support surfaces (82, 90) and a pair of oppositely facing opposed horizontal support surfaces (80, 88 and 86, 92). Thus, dead weight and operating loads from the inner casing are reacted through the support member and into the outer casing without the necessity for any bolting or other fastener attachment in the design load path between the support member and the inner casing.

摘要翻译： 一种用于涡轮机（40）的中心线悬挂装置（42）。 涡轮机内壳（44）经由支撑构件（60）支撑在外壳（46）内，支撑构件（60）包括接触内壳的内部部分（62）和延伸到形成的槽（68）的外部部分（66） 在外壳中。 支撑构件滑动到形成在内壳体中的轴向定向的狭槽（64）中，并且相对于径向运动被限制在其中，支撑构件和内壳狭槽包括相对的垂直支撑表面（82,90）和 一对相对的相对的水平支撑表面（80,88和86,92）。 因此，来自内壳体的自重和操作载荷通过支撑构件反应并进入外壳，而不需要在支撑构件和内壳之间的设计载荷路径中进行任何螺栓连接或其他紧固件附接。

公开(公告)号：US08790076B2

公开(公告)日：2014-07-29

申请号：US13719297

申请日：2012-12-19

申请人： Samuel Golinkin ,  Russell V. Caggiano ,  Timothy Ewer ,  Gennaro J. DiOrio ,  Michael J. Lipski

发明人： Samuel Golinkin ,  Russell V. Caggiano ,  Timothy Ewer ,  Gennaro J. DiOrio ,  Michael J. Lipski

IPC分类号： F01D25/26

CPC分类号： F01D25/28 ,  F05D2230/64

摘要： A centerline suspension arrangement (42) for a turbine (40). A turbine inner casing (44) is supported within an outer casing (46) via a support member (60) that includes an inner portion (62) contacting the inner casing and an outer portion (66) extending into a slot (68) formed in the outer casing. The support member is slid into an axially oriented slot (64) formed in the inner casing and is body bound therein with respect to radial movements, with the support member and the inner casing slot including opposed vertical support surfaces (82, 90) and a pair of oppositely facing opposed horizontal support surfaces (80, 88 and 86, 92). Thus, dead weight and operating loads from the inner casing are reacted through the support member and into the outer casing without the necessity for any bolting or other fastener attachment in the design load path between the support member and the inner casing.

摘要翻译： 一种用于涡轮机（40）的中心线悬挂装置（42）。 涡轮机内壳（44）经由支撑构件（60）支撑在外壳（46）内，支撑构件（60）包括接触内壳的内部部分（62）和延伸到形成的槽（68）的外部部分（66） 在外壳中。 支撑构件滑动到形成在内壳体中的轴向定向的狭槽（64）中，并且相对于径向运动被限制在其中，支撑构件和内壳狭槽包括相对的垂直支撑表面（82,90）和 一对相对的相对的水平支撑表面（80,88和86,92）。 因此，来自内壳体的自重和操作载荷通过支撑构件反应并进入外壳，而不需要在支撑构件和内壳之间的设计载荷路径中进行任何螺栓连接或其他紧固件附接。

公开(公告)号：US08430625B2

公开(公告)日：2013-04-30

申请号：US12018980

申请日：2008-01-24

申请人： Samuel Golinkin ,  Russell V. Caggiano ,  Timothy Ewer ,  Gennaro J. Diorio ,  Michael J. Lipski

发明人： Samuel Golinkin ,  Russell V. Caggiano ,  Timothy Ewer ,  Gennaro J. Diorio ,  Michael J. Lipski

IPC分类号： F01D25/26

CPC分类号： F01D25/28 ,  F05D2230/64

摘要： A centerline suspension arrangement (42) for a turbine (40). A turbine inner casing (44) is supported within an outer casing (46) via a support member (60) that includes an inner portion (62) contacting the inner casing and an outer portion (66) extending into a slot (68) formed in the outer casing. The support member is slid into an axially oriented slot (64) formed in the inner casing and is body bound therein with respect to radial movements, with the support member and the inner casing slot including opposed vertical support surfaces (82, 90) and a pair of oppositely facing opposed horizontal support surfaces (80, 88 and 86, 92). Thus, dead weight and operating loads from the inner casing are reacted through the support member and into the outer casing without the necessity for any bolting or other fastener attachment in the design load path between the support member and the inner casing.

摘要翻译： 一种用于涡轮机（40）的中心线悬挂装置（42）。 涡轮机内壳（44）经由支撑构件（60）支撑在外壳（46）内，支撑构件（60）包括接触内壳的内部部分（62）和延伸到形成的槽（68）的外部部分（66） 在外壳中。 支撑构件滑动到形成在内壳体中的轴向定向的狭槽（64）中，并且相对于径向运动被限制在其中，支撑构件和内壳狭槽包括相对的垂直支撑表面（82,90）和 一对相对的相对的水平支撑表面（80,88和86,92）。 因此，来自内壳体的自重和操作载荷通过支撑构件反应并进入外壳，而不需要在支撑构件和内壳之间的设计载荷路径中进行任何螺栓连接或其他紧固件附接。

公开(公告)号：US20130108437A1

公开(公告)日：2013-05-02

申请号：US13719297

申请日：2012-12-19

申请人： SAMUEL GOLINKIN ,  RUSSELL V. CAGGIANO ,  TIMOTHY EWER ,  GENNARO J. DiORIO ,  MICHAEL J. LIPSKI

发明人： SAMUEL GOLINKIN ,  RUSSELL V. CAGGIANO ,  TIMOTHY EWER ,  GENNARO J. DiORIO ,  MICHAEL J. LIPSKI

IPC分类号： F01D25/28

CPC分类号： F01D25/28 ,  F05D2230/64

摘要： A centerline suspension arrangement (42) for a turbine (40). A turbine inner casing (44) is supported within an outer casing (46) via a support member (60) that includes an inner portion (62) contacting the inner casing and an outer portion (66) extending into a slot (68) formed in the outer casing. The support member is slid into an axially oriented slot (64) formed in the inner casing and is body bound therein with respect to radial movements, with the support member and the inner casing slot including opposed vertical support surfaces (82, 90) and a pair of oppositely facing opposed horizontal support surfaces (80, 88 and 86, 92). Thus, dead weight and operating loads from the inner casing are reacted through the support member and into the outer casing without the necessity for any bolting or other fastener attachment in the design load path between the support member and the inner casing.

摘要翻译： 一种用于涡轮机（40）的中心线悬挂装置（42）。 涡轮机内壳（44）经由支撑构件（60）支撑在外壳（46）内，支撑构件（60）包括接触内壳的内部部分（62）和延伸到形成的槽（68）的外部部分（66） 在外壳中。 支撑构件滑动到形成在内壳体中的轴向定向的狭槽（64）中，并且相对于径向运动被限制在其中，支撑构件和内壳狭槽包括相对的垂直支撑表面（82,90）和 一对相对的相对的水平支撑表面（80,88和86,92）。 因此，来自内壳体的自重和操作载荷通过支撑构件反应并进入外壳，而不需要在支撑构件和内壳之间的设计载荷路径中进行任何螺栓连接或其他紧固件附接。