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公开(公告)号：US09810098B2
公开(公告)日：2017-11-07
申请号：US14588144
申请日：2014-12-31
发明人： Lawrence James Moore , Fredrick Levi Fuller , Jason Michael Boss , Bernard Baran Zabek , Gerald Marco Geraci , Michael Richard Pomykai
IPC分类号： F01D25/28 , F01D21/00 , G01L9/00 , G01N25/00 , G01M15/14 , G01N21/954 , B23Q3/155 , B64D47/08
CPC分类号： F01D25/285 , B23Q3/1554 , B64D47/08 , F01D21/003 , F05D2260/80 , F05D2260/83 , G01L9/00 , G01M15/14 , G01N21/954 , G01N25/00 , G01N2021/9542 , G05B2219/40607 , Y10S901/44
摘要： A system for inspecting a turbomachine is provided. The system includes a traverse actuator system and a pressure isolation system connected to the traverse actuator system. The pressure isolation system is configured to maintain a pressure resistant seal around a probe. A gimbal mount is connected to the pressure isolation system. The system is configured to move the probe into and out of the turbomachine.
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公开(公告)号：US20160011080A1
公开(公告)日：2016-01-14
申请号：US14588157
申请日：2014-12-31
发明人： Lawrence James Moore , Fredrick Levi Fuller , Jason Michael Boss , Bernard Baran Zabek , Gerald Marco Geraci , Michael Richard Pomykai
IPC分类号： G01M15/14
CPC分类号： F01D25/285 , B23Q3/1554 , B64D47/08 , F01D21/003 , F05D2260/80 , F05D2260/83 , G01L9/00 , G01M15/14 , G01N21/954 , G01N25/00 , G01N2021/9542 , G05B2219/40607 , Y10S901/44
摘要： A system for inspecting a turbomachine includes a traverse actuator system having a carriage configured to move a probe into and out of the turbomachine. The traverse actuator system has a track with a plurality of linearly arranged teeth. The track is configured for operation with the carriage. A motor is operably connected with the carriage and track, and the motor is configured to engage the plurality of linearly arranged teeth so that operation of the motor forces the carriage to move along the track.
摘要翻译： 用于检查涡轮机的系统包括横动致动器系统，其具有被配置成将探头移入和移出涡轮机的托架。 横动执行器系统具有多个线性排列的齿的轨道。 轨道配置为与托架一起操作。 电动机与滑架和轨道可操作地连接，并且电动机构造成与多个线性排列的齿接合，使得电动机的操作迫使滑架沿轨道移动。
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公开(公告)号：US20160010505A1
公开(公告)日：2016-01-14
申请号：US14588173
申请日：2014-12-31
发明人： Lawrence James Moore , Fredrick Levi Fuller , Jason Michael Boss , Bernard Baran Zabek , Gerald Marco Geraci , Michael Richard Pomykai
CPC分类号： F01D25/285 , B23Q3/1554 , B64D47/08 , F01D21/003 , F05D2260/80 , F05D2260/83 , G01L9/00 , G01M15/14 , G01N21/954 , G01N25/00 , G01N2021/9542 , G05B2219/40607 , Y10S901/44
摘要： A method for inspecting a turbomachine is provided. The method includes the steps of, attaching a gimbal mount to the turbomachine, inserting a probe into the turbomachine through the gimbal mount, and adjusting a position of the probe via the gimbal mount. A removing step removes the probe from the turbomachine. An attaching step attaches a traverse actuator system to the gimbal mount. The traverse actuator system is connected to the gimbal mount through a pressure isolation system. A reinserting step is used to reinsert the probe back into the turbomachine. An inspecting step is used to inspect or test the turbomachine.
摘要翻译： 提供了一种用于检查涡轮机的方法。 该方法包括以下步骤：将万向架安装件附接到涡轮机，通过万向架安装将探头插入涡轮机中，以及通过万向节安装座调节探头的位置。 去除步骤从涡轮机中移除探针。 安装步骤将横动执行器系统附接到万向架安装座。 横动执行器系统通过压力隔离系统连接到万向架。 重新插入步骤用于将探头重新插入涡轮机。 检查步骤用于检查或测试涡轮机。
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公开(公告)号：US09683460B2
公开(公告)日：2017-06-20
申请号：US14588173
申请日：2014-12-31
发明人： Lawrence James Moore , Fredrick Levi Fuller , Jason Michael Boss , Bernard Baran Zabek , Gerald Marco Geraci , Michael Richard Pomykai
IPC分类号： F01D25/28 , F01D21/00 , G01L9/00 , G01N25/00 , G01M15/14 , G01N21/954 , B23Q3/155 , B64D47/08
CPC分类号： F01D25/285 , B23Q3/1554 , B64D47/08 , F01D21/003 , F05D2260/80 , F05D2260/83 , G01L9/00 , G01M15/14 , G01N21/954 , G01N25/00 , G01N2021/9542 , G05B2219/40607 , Y10S901/44
摘要： A method for inspecting a turbomachine is provided. The method includes the steps of, attaching a gimbal mount to the turbomachine, inserting a probe into the turbomachine through the gimbal mount, and adjusting a position of the probe via the gimbal mount. A removing step removes the probe from the turbomachine. An attaching step attaches a traverse actuator system to the gimbal mount. The traverse actuator system is connected to the gimbal mount through a pressure isolation system. A reinserting step is used to reinsert the probe back into the turbomachine. An inspecting step is used to inspect or test the turbomachine.
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公开(公告)号：US20160010506A1
公开(公告)日：2016-01-14
申请号：US14588187
申请日：2014-12-31
发明人： Lawrence James Moore , Fredrick Levi Fuller , Jason Michael Boss , Bernard Baran Zabek , Gerald Marco Geraci , Michael Richard Pomykai
CPC分类号： F01D25/285 , B23Q3/1554 , B64D47/08 , F01D21/003 , F05D2260/80 , F05D2260/83 , G01L9/00 , G01M15/14 , G01N21/954 , G01N25/00 , G01N2021/9542 , G05B2219/40607 , Y10S901/44
摘要： A system for inspecting a turbomachine is provided. The system includes a pressure isolation system configured to maintain a pressure resistant seal around a probe. The pressure isolation system has a probe bearing located adjacent to a pressure seal. The probe bearing is configured to facilitate back and forth movement of the probe by reducing friction. A gimbal mount is connected to the pressure isolation system. The pressure isolation system has a valve seal located between the gimbal mount and the pressure seal. The valve seal is configured to isolate the pressure seal from the gimbal mount when the probe is not in the valve seal. The system is configured to move the probe into and out of the turbomachine.
摘要翻译： 提供了一种用于检查涡轮机的系统。 该系统包括压力隔离系统，其被配置成在探针周围保持耐压密封。 压力隔离系统具有邻近压力密封的探针轴承。 探针轴承构造成通过减少摩擦力来促进探头的前后运动。 万向支架连接到压力隔离系统。 压力隔离系统具有位于万向节安装座和压力密封件之间的阀密封。 阀密封件被配置为当探头不在阀密封中时将压力密封件与万向架安装件隔离开。 该系统配置成将探头移入和移出涡轮机。
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公开(公告)号：US09708934B2
公开(公告)日：2017-07-18
申请号：US14588157
申请日：2014-12-31
发明人： Lawrence James Moore , Fredrick Levi Fuller , Jason Michael Boss , Bernard Baran Zabek , Gerald Marco Geraci , Michael Richard Pomykai
IPC分类号： F01D25/28 , F01D21/00 , G01L9/00 , G01N25/00 , G01M15/14 , G01N21/954 , B23Q3/155 , B64D47/08
CPC分类号： F01D25/285 , B23Q3/1554 , B64D47/08 , F01D21/003 , F05D2260/80 , F05D2260/83 , G01L9/00 , G01M15/14 , G01N21/954 , G01N25/00 , G01N2021/9542 , G05B2219/40607 , Y10S901/44
摘要： A system for inspecting a turbomachine includes a traverse actuator system having a carriage configured to move a probe into and out of the turbomachine. The traverse actuator system has a track with a plurality of linearly arranged teeth. The track is configured for operation with the carriage. A motor is operably connected with the carriage and track, and the motor is configured to engage the plurality of linearly arranged teeth so that operation of the motor forces the carriage to move along the track.
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公开(公告)号：US09657597B2
公开(公告)日：2017-05-23
申请号：US14588187
申请日：2014-12-31
发明人： Lawrence James Moore , Fredrick Levi Fuller , Jason Michael Boss , Bernard Baran Zabek , Gerald Marco Geraci , Michael Richard Pomykai
IPC分类号： F01D25/28 , F01D21/00 , G01L9/00 , G01N25/00 , G01M15/14 , G01N21/954 , B23Q3/155 , B64D47/08
CPC分类号： F01D25/285 , B23Q3/1554 , B64D47/08 , F01D21/003 , F05D2260/80 , F05D2260/83 , G01L9/00 , G01M15/14 , G01N21/954 , G01N25/00 , G01N2021/9542 , G05B2219/40607 , Y10S901/44
摘要： A system for inspecting a turbomachine is provided. The system includes a pressure isolation system configured to maintain a pressure resistant seal around a probe. The pressure isolation system has a probe bearing located adjacent to a pressure seal. The probe bearing is configured to facilitate back and forth movement of the probe by reducing friction. A gimbal mount is connected to the pressure isolation system. The pressure isolation system has a valve seal located between the gimbal mount and the pressure seal. The valve seal is configured to isolate the pressure seal from the gimbal mount when the probe is not in the valve seal. The system is configured to move the probe into and out of the turbomachine.
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公开(公告)号：US20160011079A1
公开(公告)日：2016-01-14
申请号：US14588144
申请日：2014-12-31
发明人： Lawrence James Moore , Fredrick Levi Fuller , Jason Michael Boss , Bernard Baran Zabek , Gerald Marco Geraci , Michael Richard Pomykai
IPC分类号： G01M15/14
CPC分类号： F01D25/285 , B23Q3/1554 , B64D47/08 , F01D21/003 , F05D2260/80 , F05D2260/83 , G01L9/00 , G01M15/14 , G01N21/954 , G01N25/00 , G01N2021/9542 , G05B2219/40607 , Y10S901/44
摘要： A system for inspecting a turbomachine is provided. The system includes a traverse actuator system and a pressure isolation system connected to the traverse actuator system. The pressure isolation system is configured to maintain a pressure resistant seal around a probe. A gimbal mount is connected to the pressure isolation system. The system is configured to move the probe into and out of the turbomachine.
摘要翻译： 提供了一种用于检查涡轮机的系统。 该系统包括横移致动器系统和连接到横动执行器系统的压力隔离系统。 压力隔离系统被配置成在探针周围保持耐压密封。 万向支架连接到压力隔离系统。 该系统配置成将探头移入和移出涡轮机。
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