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公开(公告)号：US08636449B2
公开(公告)日：2014-01-28
申请号：US13095498
申请日：2011-04-27
IPC分类号： B23B47/34
CPC分类号： F01D25/243 , B23B35/00 , B23B41/00 , B23B2215/76 , B23B2270/30 , B23B2270/62 , B23Q11/0046 , F05D2230/80 , F05D2260/607 , Y10T408/03 , Y10T408/50
摘要： A method of drilling one or more holes, substantially in situ, in a turbomachine casing includes locating piping including at least one vacuum head within the turbomachine casing in proximity to a hole to be drilled; drilling at least one hole in the casing such that drill chips or shavings caused by the drilling are collected in the vacuum head; and applying a vacuum through the piping to the at least one vacuum head to thereby remove the drill chips or shavings collected in the vacuum head to a location outside the turbomachine casing.
摘要翻译： 在涡轮机壳体中基本上原位钻一个或多个孔的方法包括将涡轮机壳体内的至少一个真空头定位在靠近待钻孔的位置， 在壳体中钻出至少一个孔，使得由钻孔引起的钻屑或刨屑被收集在真空头中; 以及通过所述管道将真空施加到所述至少一个真空头，从而将收集在所述真空头中的钻屑或切屑除去到所述涡轮机壳体外部的位置。
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公开(公告)号：US20130171611A1
公开(公告)日：2013-07-04
申请号：US13342655
申请日：2012-01-03
IPC分类号： G09B25/00
CPC分类号： G09B25/02
摘要： This disclosure describes a training apparatus, wherein embodiments of the training apparatus simulate operation of fan blades in a turbine engine. An advantage that practice of some disclosed embodiments of the training apparatus is to provide a platform to train skills for maintaining and servicing turbine engines without placing the individual and/or customer hardware in jeopardy.
摘要翻译： 本公开描述了训练装置，其中训练装置的实施例模拟涡轮发动机中的风扇叶片的操作。 培训设备的一些公开的实施例的实践的优点是提供一个平台来训练维护和维修涡轮发动机的技能，而不会使个人和/或客户硬件处于危险之中。
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公开(公告)号：US09108829B2
公开(公告)日：2015-08-18
申请号：US12964312
申请日：2010-12-09
IPC分类号： B66F3/08
CPC分类号： B66F3/08
摘要： A machine casing section lift system includes a first attachment member configured to attach to a machine casing section, the first attachment member including a first jacking mechanism connection portion. The system also includes a second attachment member configured to attach to a lower casing section that, in operation, is positioned below the machine casing section, the second attachment member including a second jacking mechanism connection portion. The system also includes a jacking mechanism to raise the machine casing section and having a collar configured to couple with the first jacking mechanism connection portion and a base configured to rest in the second jacking mechanism connection portion.
摘要翻译： 机壳部分提升系统包括构造成附接到机器壳体部分的第一附接构件，第一附接构件包括第一顶起机构连接部分。 该系统还包括第二附接构件，其构造成附接到下壳体部分，其在操作中位于机壳部分下方，所述第二附接构件包括第二顶起机构连接部分。 该系统还包括顶起机构，用于升高机壳部分并具有被配置为与第一顶起机构连接部分联接的轴环和被配置为搁置在第二顶起机构连接部分中的底座。
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公开(公告)号：US08451459B2
公开(公告)日：2013-05-28
申请号：US13073724
申请日：2011-03-28
申请人： Andrew Thomas Hynous
发明人： Andrew Thomas Hynous
IPC分类号： G01B11/14
CPC分类号： G01B11/14 , G01B11/026 , Y10T29/49826
摘要： A method for use in inspecting a blade tip clearance is provided. The method includes providing a plurality of rotor blades including tips, wherein the plurality of rotor blades are rotatably mounted within a casing such that a blade tip clearance is defined between the rotor blade tips and the casing. The method also includes providing a system for use in inspecting the blade tip clearance by emitting electromagnetic energy toward the tips and detecting electromagnetic energy reflected by the tips. The method further includes positioning the system to facilitate inspection of the blade tip clearance, rotating the plurality of rotor blades within the casing, and simultaneously blending the tips using a blending apparatus and inspecting the blade tip clearance using the system.
摘要翻译： 提供了一种用于检查叶片顶端间隙的方法。 该方法包括提供包括尖端的多个转子叶片，其中多个转子叶片可旋转地安装在壳体内，使得在转子叶片尖端和壳体之间限定叶片顶端间隙。 该方法还包括提供一种用于通过向尖端发射电磁能量并检测由尖端反射的电磁能量来检查叶片顶端间隙的系统。 该方法还包括定位系统以便于检查叶片顶端间隙，使壳体内的多个转子叶片旋转，并且使用混合装置同时混合顶端并使用系统检查叶片顶端间隙。
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公开(公告)号：US20100110450A1
公开(公告)日：2010-05-06
申请号：US12262815
申请日：2008-10-31
IPC分类号： G01B11/14
CPC分类号： G01B11/14
摘要： A method for inspecting blade tip clearance between at least one rotor blade and a case spaced radially outward from the rotor blade is provided. The method includes inserting a probe into an aperture defined in the case and emitting electromagnetic energy into the case using the probe. The method also includes detecting electromagnetic energy reflected from a blade tip portion of the rotor blade and determining a blade tip clearance defined between the blade tip and the case based on the detected electromagnetic energy.
摘要翻译： 提供了一种用于检查至少一个转子叶片与从转子叶片径向向外间隔开的壳体之间的叶片顶端间隙的方法。 该方法包括将探针插入到壳体中限定的孔中，并使用探针将电磁能发射到壳体内。 该方法还包括检测从转子叶片的叶片尖端部分反射的电磁能量，并且基于检测到的电磁能量确定限定在叶片尖端和壳体之间的叶片顶端间隙。
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公开(公告)号：US20130292229A1
公开(公告)日：2013-11-07
申请号：US13463044
申请日：2012-05-03
申请人： Michael Alan Davi , Paul Robert Fernandez , John William Herbold , Andrew Thomas Hynous , Sean O'Meara
发明人： Michael Alan Davi , Paul Robert Fernandez , John William Herbold , Andrew Thomas Hynous , Sean O'Meara
IPC分类号： B65G35/06
摘要： Solutions for minimizing the impact of servicing a turbo machine are disclosed. In one embodiment, an apparatus for conveying a turbo machine component can include: a motive system for moving the apparatus along a surface; a platform system operably connected to the motive system, the platform system for supporting the component of the turbo machine, the platform system can include: a first portion fixed to the motive system; and a second portion moveably coupled to the first portion, the second portion for modifying a position of the turbo machine component; and a control system operably connected to the platform system, the control system for controlling at least one of a rate of movement or a direction of the second portion of the platform system.
摘要翻译： 公开了用于最小化维修涡轮机的影响的解决方案。 在一个实施例中，用于传送涡轮机部件的装置可以包括：用于沿着表面移动设备的动力系统; 可操作地连接到动力系统的平台系统，用于支撑涡轮机组件的平台系统，平台系统可以包括：固定到动力系统的第一部分; 以及可移动地联接到所述第一部分的第二部分，所述第二部分用于修改所述涡轮机部件的位置; 以及可操作地连接到平台系统的控制系统，所述控制系统用于控制平台系统的第二部分的移动速度或方向中的至少一个。
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公开(公告)号：US20120145976A1
公开(公告)日：2012-06-14
申请号：US12964312
申请日：2010-12-09
IPC分类号： B66F3/08
CPC分类号： B66F3/08
摘要： A machine casing section lift system includes a first attachment member configured to attach to a machine casing section, the first attachment member including a first jacking mechanism connection portion. The system also includes a second attachment member configured to attach to a lower casing section that, in operation, is positioned below the machine casing section, the second attachment member including a second jacking mechanism connection portion. The system also includes a jacking mechanism to raise the machine casing section and having a collar configured to couple with the first jacking mechanism connection portion and a base configured to rest in the second jacking mechanism connection portion.
摘要翻译： 机壳部分提升系统包括构造成附接到机器壳体部分的第一附接构件，第一附接构件包括第一顶起机构连接部分。 该系统还包括第二附接构件，其构造成附接到下壳体部分，其在操作中位于机壳部分下方，所述第二附接构件包括第二顶起机构连接部分。 该系统还包括顶起机构，用于升高机壳部分并具有被配置为与第一顶起机构连接部分联接的轴环和被配置为搁置在第二顶起机构连接部分中的底座。
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公开(公告)号：US08956100B2
公开(公告)日：2015-02-17
申请号：US13463044
申请日：2012-05-03
申请人： Michael Alan Davi , Paul Robert Fernandez , John William Herbold , Andrew Thomas Hynous , Sean O'Meara
发明人： Michael Alan Davi , Paul Robert Fernandez , John William Herbold , Andrew Thomas Hynous , Sean O'Meara
IPC分类号： B60P3/40
摘要： Solutions for minimizing the impact of servicing a turbo machine are disclosed. In one embodiment, an apparatus for conveying a turbo machine component can include: a motive system for moving the apparatus along a surface; a platform system operably connected to the motive system, the platform system for supporting the component of the turbo machine, the platform system can include: a first portion fixed to the motive system; and a second portion moveably coupled to the first portion, the second portion for modifying a position of the turbo machine component; and a control system operably connected to the platform system, the control system for controlling at least one of a rate of movement or a direction of the second portion of the platform system.
摘要翻译： 公开了用于最小化维修涡轮机的影响的解决方案。 在一个实施例中，用于传送涡轮机部件的装置可以包括：用于沿着表面移动设备的动力系统; 可操作地连接到动力系统的平台系统，用于支撑涡轮机组件的平台系统，平台系统可以包括：固定到动力系统的第一部分; 以及可移动地联接到所述第一部分的第二部分，所述第二部分用于修改所述涡轮机部件的位置; 以及可操作地连接到平台系统的控制系统，所述控制系统用于控制平台系统的第二部分的移动速度或方向中的至少一个。
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公开(公告)号：US20120069355A1
公开(公告)日：2012-03-22
申请号：US13073724
申请日：2011-03-28
申请人： Andrew Thomas Hynous
发明人： Andrew Thomas Hynous
CPC分类号： G01B11/14 , G01B11/026 , Y10T29/49826
摘要： A method for use in inspecting a blade tip clearance is provided. The method includes providing a plurality of rotor blades including tips, wherein the plurality of rotor blades are rotatably mounted within a casing such that a blade tip clearance is defined between the rotor blade tips and the casing. The method also includes providing a system for use in inspecting the blade tip clearance by emitting electromagnetic energy toward the tips and detecting electromagnetic energy reflected by the tips. The method further includes positioning the system to facilitate inspection of the blade tip clearance, rotating the plurality of rotor blades within the casing, and simultaneously blending the tips using a blending apparatus and inspecting the blade tip clearance using the system.
摘要翻译： 提供了一种用于检查叶片顶端间隙的方法。 该方法包括提供包括尖端的多个转子叶片，其中多个转子叶片可旋转地安装在壳体内，使得在转子叶片尖端和壳体之间限定叶片顶端间隙。 该方法还包括提供一种用于通过向尖端发射电磁能量并检测由尖端反射的电磁能量来检查叶片顶端间隙的系统。 该方法还包括定位系统以便于检查叶片顶端间隙，使壳体内的多个转子叶片旋转，并且使用混合装置同时混合顶端并使用系统检查叶片顶端间隙。
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公开(公告)号：US07916311B2
公开(公告)日：2011-03-29
申请号：US12262815
申请日：2008-10-31
IPC分类号： G01B11/14
CPC分类号： G01B11/14
摘要： A method for inspecting blade tip clearance between at least one rotor blade and a case spaced radially outward from the rotor blade is provided. The method includes inserting a probe into an aperture defined in the case and emitting electromagnetic energy into the case using the probe. The method also includes detecting electromagnetic energy reflected from a blade tip portion of the rotor blade and determining a blade tip clearance defined between the blade tip and the case based on the detected electromagnetic energy.
摘要翻译： 提供了一种用于检查至少一个转子叶片与从转子叶片径向向外间隔开的壳体之间的叶片顶端间隙的方法。 该方法包括将探针插入壳体中限定的孔中，并使用探头将电磁能发射到壳体内。 该方法还包括检测从转子叶片的叶片尖端部分反射的电磁能量，并且基于检测到的电磁能量确定限定在叶片尖端和壳体之间的叶片顶端间隙。
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