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1. 发明申请

US20140026414A1 METHOD AND SYSTEM FOR ASSEMBLING AND DISASSEMBLING TURBOMACHINES 有权
标题翻译：用于组装和拆卸涡轮机的方法和系统
公开(公告)号：US20140026414A1
公开(公告)日：2014-01-30
申请号：US13558526
申请日：2012-07-26
申请人： James Bradford Holmes , Kenneth Damon Black , Christopher Paul Cox , Matthew Stephen Casavant , Bradley Edwin Wilson , Brett Darrick Klingler
发明人： James Bradford Holmes , Kenneth Damon Black , Christopher Paul Cox , Matthew Stephen Casavant , Bradley Edwin Wilson , Brett Darrick Klingler
IPC分类号： B23P6/00
CPC分类号： F01D9/04 , B66F3/24 , F01D25/26 , F01D25/28 , F01D25/285 , F05D2230/60 , F05D2230/644 , F05D2230/70 , F05D2260/53 , F05D2260/57 , Y10T29/49238 , Y10T29/53
摘要： A method and system adapted for removing one or more shells from an assembly of multiple annular shells, for example, turbine shells of a gas turbine engine. The method includes removing an upper shell positioned in an upper position relative to a lower shell of the assembly of multiple annular shells, and then positioning and securing a counterweight in the upper position and securing the counterweight to the lower shell as a replacement for the upper shell in the upper position. The counterweight and the lower shell are then rotated in unison until the lower shell is in the upper position and the counterweight is in a lower position previously occupied by the lower shell. Thereafter, the lower shell can be removed from the assembly.
摘要翻译：一种适于从多个环形壳体的组件（例如燃气涡轮发动机的涡轮机壳体）移除一个或多个壳体的方法和系统。该方法包括去除位于相对于多个环形壳体的组件的下壳体的上部位置的上壳体，然后将配重定位并固定在上部位置，并将配重固定到下部壳体，以代替上部壳在上位。然后，配重和下壳同时旋转，直到下壳体处于上部位置，并且配重处于先前被下壳体占据的较低位置。此后，可以从组件中移除下壳。

2. 发明授权

US09097123B2 Method and system for assembling and disassembling turbomachines 有权
标题翻译：组装和拆卸涡轮机的方法和系统
公开(公告)号：US09097123B2
公开(公告)日：2015-08-04
申请号：US13558526
申请日：2012-07-26
申请人： James Bradford Holmes , Kenneth Damon Black , Christopher Paul Cox , Matthew Stephen Casavant , Bradley Edwin Wilson , Brett Darrick Klingler
发明人： James Bradford Holmes , Kenneth Damon Black , Christopher Paul Cox , Matthew Stephen Casavant , Bradley Edwin Wilson , Brett Darrick Klingler
IPC分类号： F01D25/26 , F01D25/28 , F01D25/24 , F03B11/02 , F04D29/60 , B23P6/00 , B23P23/00 , B23P19/04 , B23P19/00 , F01D9/04
CPC分类号： F01D9/04 , B66F3/24 , F01D25/26 , F01D25/28 , F01D25/285 , F05D2230/60 , F05D2230/644 , F05D2230/70 , F05D2260/53 , F05D2260/57 , Y10T29/49238 , Y10T29/53
摘要： A method and system adapted for removing one or more shells from an assembly of multiple annular shells, for example, turbine shells of a gas turbine engine. The method includes removing an upper shell positioned in an upper position relative to a lower shell of the assembly of multiple annular shells, and then positioning and securing a counterweight in the upper position and securing the counterweight to the lower shell as a replacement for the upper shell in the upper position. The counterweight and the lower shell are then rotated in unison until the lower shell is in the upper position and the counterweight is in a lower position previously occupied by the lower shell. Thereafter, the lower shell can be removed from the assembly.
摘要翻译：一种适于从多个环形壳体的组件（例如燃气涡轮发动机的涡轮机壳体）移除一个或多个壳体的方法和系统。该方法包括去除位于相对于多个环形壳体的组件的下壳体的上部位置的上壳体，然后将配重定位并固定在上部位置，并将配重固定到下部壳体，以代替上部壳在上位。然后，配重和下壳同时旋转，直到下壳体处于上部位置，并且配重处于先前被下壳体占据的较低位置。此后，可以从组件中移除下壳。

3. 发明申请

US20130326875A1 METHOD AND APPARATUS FOR ROLL-IN AND ALIGNMENT OF A CASING SHELL OF A GAS TURBINE 审中-公开
标题翻译：气体涡轮机外壳的滚动和对准的方法和装置
公开(公告)号：US20130326875A1
公开(公告)日：2013-12-12
申请号：US13492297
申请日：2012-06-08
申请人： Kenneth Damon Black , Matthew Stephen Casavant , Brett Darrick Klingler
发明人： Kenneth Damon Black , Matthew Stephen Casavant , Brett Darrick Klingler
IPC分类号： B23P19/04 , B23P17/00
CPC分类号： F01D25/285 , F01D9/04 , F01D25/26 , F04D29/644 , F05D2230/60 , F05D2230/644 , F05D2230/70 , F05D2260/53 , F05D2260/57 , Y10T29/49231 , Y10T29/53687
摘要： A method and apparatus for rolling and aligning a casing of a gas turbine is disclosed. At least one jack having a roller at one end is positioned at a location to couple the roller to the casing. The casing is rolled within the turbine by rolling over the roller of the at least one jack. The roller is moved relative to the at least one jack to align the casing within the turbine.
摘要翻译：公开了一种用于滚动和对准燃气轮机壳体的方法和装置。在一端具有辊的至少一个插孔定位在将辊连接到壳体的位置。通过滚动至少一个千斤顶的辊子将壳体在涡轮机内滚动。辊子相对于至少一个千斤顶移动，以使壳体在涡轮机内对准。

4. 发明授权

US08992167B2 Turbine casing assembly mounting pin 有权
标题翻译：涡轮机壳总成安装销
公开(公告)号：US08992167B2
公开(公告)日：2015-03-31
申请号：US13226823
申请日：2011-09-07
申请人： Matthew Stephen Casavant , Kenneth Damon Black
发明人： Matthew Stephen Casavant , Kenneth Damon Black
IPC分类号： F01D25/24
CPC分类号： F01D25/243 , F01D25/246 , F01D25/26 , F01D25/28 , F05D2230/644 , F05D2260/30 , Y10T29/4932
摘要： In certain embodiments of the present disclosure a turbine casing assembly is described. The turbine casing assembly includes an inner casing and an outer casing surrounding the inner casing. The outer casing includes a first outer casing section and a second outer casing section that join together along a flange. Two bolts extend through the flange and join together the first outer casing section and the second outer casing section. A pin having a first segment having a first diameter and a second segment having a second diameter extends through the inner casing and the outer casing and supports the inner casing relative to the outer casing. The pin has a first diameter that is greater than the second diameter and is located between the two bolts along the axis of the flange.
摘要翻译：在本公开的某些实施例中，描述了涡轮机壳体组件。涡轮机壳体组件包括内壳体和围绕内壳体的外壳体。外壳包括沿法兰连接在一起的第一外壳部分和第二外壳部分。两个螺栓延伸穿过凸缘并将第一外壳部分和第二外壳部分接合在一起。具有第一直径的第一段和具有第二直径的第二段的销延伸穿过内壳和外壳并相对于外壳支撑内壳。销具有大于第二直径的第一直径，并且沿着凸缘的轴线位于两个螺栓之间。

5. 发明申请

US20130058780A1 TURBINE CASING ASSEMBLY MOUNTING PIN 有权
标题翻译：涡轮机壳组装安装孔
公开(公告)号：US20130058780A1
公开(公告)日：2013-03-07
申请号：US13226847
申请日：2011-09-07
申请人： Matthew Stephen Casavant , Kenneth Damon Black
发明人： Matthew Stephen Casavant , Kenneth Damon Black
IPC分类号： F01D25/28 , B23P11/00 , F01D25/26
CPC分类号： F01D25/243 , Y10T29/49323
摘要： In certain embodiments of the present disclosure, a turbine casing assembly is described. The turbine casing assembly includes an inner casing and an outer casing surrounding the inner casing. The outer casing has a first outer casing section and a second outer casing section that join together along a flange. A bolt extends through the flange and joins together the first outer casing section and the second outer casing section. The turbine casing assembly further includes a pin. The pin has a segment defining an opening therethrough. The pin extends through the inner casing and the outer casing and supports the inner casing relative to the outer casing. The bolt passes through the opening defined by the pin.
摘要翻译：在本公开的某些实施例中，描述了涡轮机壳体组件。涡轮机壳体组件包括内壳体和围绕内壳体的外壳体。外壳具有沿法兰连接在一起的第一外壳部分和第二外壳部分。螺栓延伸穿过凸缘并将第一外壳部分和第二外壳部分连接在一起。涡轮机壳体组件还包括销。销具有限定穿过其中的开口的段。销延伸穿过内壳和外壳，并相对于外壳支撑内壳。螺栓穿过由销定义的开口。

6. 发明申请

US20130064649A1 PIPING ASSEMBLY AND METHOD FOR CONNECTING INNER AND OUTER SHELL IN TURBINE SYSTEM 有权
标题翻译：用于连接涡轮机内部和外壳的管道组件和方法
公开(公告)号：US20130064649A1
公开(公告)日：2013-03-14
申请号：US13227907
申请日：2011-09-08
申请人： Kenneth Damon Black , Matthew Stephen Casavant
发明人： Kenneth Damon Black , Matthew Stephen Casavant
IPC分类号： F16L27/00 , B23P11/00 , F01D25/26
CPC分类号： F02C7/00 , F01D25/14 , F01D25/243 , F05D2250/32 , F05D2250/71 , Y10T29/49323
摘要： A piping assembly and a method for connecting an inner shell and an outer shell in a turbine system are disclosed. The piping assembly includes an inner fitting for connection to the inner shell and an outer fitting for connection to the outer shell. The piping assembly further includes an attenuation member extending between the inner fitting and the outer fitting and comprising an attenuation curve. The attenuation curve permits movement of the attenuation member in at least one of a longitudinal direction, a radial direction, or a tangential direction.
摘要翻译：公开了一种管道组件和用于连接涡轮机系统中的内壳和外壳的方法。管道组件包括用于连接到内壳的内部配件和用于连接到外壳的外部配件。管道组件还包括在内部配件和外部配件之间延伸并包括衰减曲线的衰减构件。衰减曲线允许衰减构件在纵向方向，径向方向或切向方向中的至少一个中移动。

7. 发明授权

US08864459B2 Turbine casing assembly mounting pin 有权
标题翻译：涡轮机壳总成安装销
公开(公告)号：US08864459B2
公开(公告)日：2014-10-21
申请号：US13226847
申请日：2011-09-07
申请人： Matthew Stephen Casavant , Kenneth Damon Black
发明人： Matthew Stephen Casavant , Kenneth Damon Black
IPC分类号： F01D25/26 , F01D25/24
CPC分类号： F01D25/243 , Y10T29/49323
摘要： In certain embodiments of the present disclosure, a turbine casing assembly is described. The turbine casing assembly includes an inner casing and an outer casing surrounding the inner casing. The outer casing has a first outer casing section and a second outer casing section that join together along a flange. A bolt extends through the flange and joins together the first outer casing section and the second outer casing section. The turbine casing assembly further includes a pin. The pin has a segment defining an opening therethrough. The pin extends through the inner casing and the outer casing and supports the inner casing relative to the outer casing. The bolt passes through the opening defined by the pin.
摘要翻译：在本公开的某些实施例中，描述了涡轮机壳体组件。涡轮机壳体组件包括内壳体和围绕内壳体的外壳体。外壳具有沿法兰连接在一起的第一外壳部分和第二外壳部分。螺栓延伸穿过凸缘并将第一外壳部分和第二外壳部分连接在一起。涡轮机壳体组件还包括销。销具有限定穿过其中的开口的段。销延伸穿过内壳和外壳，并相对于外壳支撑内壳。螺栓穿过由销定义的开口。

8. 发明授权

US08915701B2 Piping assembly and method for connecting inner and outer shell in turbine system 有权
标题翻译：用于连接涡轮机内壳和外壳的管道组件和方法
公开(公告)号：US08915701B2
公开(公告)日：2014-12-23
申请号：US13227907
申请日：2011-09-08
申请人： Kenneth Damon Black , Matthew Stephen Casavant
发明人： Kenneth Damon Black , Matthew Stephen Casavant
IPC分类号： F01D25/14 , F02C7/00 , F01D25/24
CPC分类号： F02C7/00 , F01D25/14 , F01D25/243 , F05D2250/32 , F05D2250/71 , Y10T29/49323
摘要： A piping assembly and a method for connecting an inner shell and an outer shell in a turbine system are disclosed. The piping assembly includes an inner fitting for connection to the inner shell and an outer fitting for connection to the outer shell. The piping assembly further includes an attenuation member extending between the inner fitting and the outer fitting and comprising an attenuation curve. The attenuation curve permits movement of the attenuation member in at least one of a longitudinal direction, a radial direction, or a tangential direction.
摘要翻译：公开了一种管道组件和用于连接涡轮机系统中的内壳和外壳的方法。管道组件包括用于连接到内壳的内部配件和用于连接到外壳的外部配件。管道组件还包括在内部配件和外部配件之间延伸并包括衰减曲线的衰减构件。衰减曲线允许衰减构件在纵向方向，径向方向或切向方向中的至少一个中移动。

9. 发明申请

US20130058779A1 TURBINE CASING ASSEMBLY MOUNTING PIN 有权
标题翻译：涡轮机壳组装安装孔
公开(公告)号：US20130058779A1
公开(公告)日：2013-03-07
申请号：US13226823
申请日：2011-09-07
申请人： Matthew Stephen Casavant , Kenneth Damon Black
发明人： Matthew Stephen Casavant , Kenneth Damon Black
IPC分类号： F01D25/28 , B23P15/04
CPC分类号： F01D25/243 , F01D25/246 , F01D25/26 , F01D25/28 , F05D2230/644 , F05D2260/30 , Y10T29/4932
摘要： In certain embodiments of the present disclosure a turbine casing assembly is described. The turbine casing assembly includes an inner casing and an outer casing surrounding the inner casing. The outer casing includes a first outer casing section and a second outer casing section that join together along a flange. Two bolts extend through the flange and join together the first outer casing section and the second outer casing section. A pin having a first segment having a first diameter and a second segment having a second diameter extends through the inner casing and the outer casing and supports the inner casing relative to the outer casing. The pin has a first diameter that is greater than the second diameter and is located between the two bolts along the axis of the flange.
摘要翻译：在本公开的某些实施例中，描述了涡轮机壳体组件。涡轮机壳体组件包括内壳体和围绕内壳体的外壳体。外壳包括沿法兰连接在一起的第一外壳部分和第二外壳部分。两个螺栓延伸穿过凸缘并将第一外壳部分和第二外壳部分接合在一起。具有第一直径的第一段和具有第二直径的第二段的销延伸穿过内壳和外壳并相对于外壳支撑内壳。销具有大于第二直径的第一直径，并且沿着凸缘的轴线位于两个螺栓之间。

10. 发明申请

US20140017076A1 Turbine Shell Support Arm 有权
标题翻译：涡轮壳支撑臂
公开(公告)号：US20140017076A1
公开(公告)日：2014-01-16
申请号：US13547146
申请日：2012-07-12
申请人： Bradley Edwin Wilson , Kenneth Damon Black
发明人： Bradley Edwin Wilson , Kenneth Damon Black
IPC分类号： F01D25/28
CPC分类号： F01D25/28
摘要： The present application and the resultant patent provide an example of a turbine casing. The turbine casing may include an outer shell, an inner shell, and a support arm supporting the inner shell within the outer shell. The inner shell and the support arm may include a scallop therein for reduced stress.
摘要翻译：本申请和所得到的专利提供了涡轮机壳体的示例。涡轮机壳体可以包括外壳，内壳和支撑外壳内的内壳。内壳和支撑臂可以包括其中的扇贝以减轻应力。

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