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1. 发明申请

US20130083187A1 SYSTEMS AND METHODS FOR HANDS FREE INSPECTION 有权
标题翻译：用于免费检查的系统和方法
公开(公告)号：US20130083187A1
公开(公告)日：2013-04-04
申请号：US13617801
申请日：2012-09-14
申请人： Binglong Xie , Yakup Genc , Clifford Hatcher, JR. , Himanshu Bhatnagar , Forrest R. Ruhge
发明人： Binglong Xie , Yakup Genc , Clifford Hatcher, JR. , Himanshu Bhatnagar , Forrest R. Ruhge
IPC分类号： G06K9/00
CPC分类号： G06K9/00624 , G01N21/9515 , G01N21/954 , G06Q10/20 , G06Q50/06
摘要： Systems and methods for inspecting a device are disclosed. The method includes arranging the device in a known position relative to a plurality of movable cameras. The plurality of movable cameras is mounted on a controllable actuator. The plurality of cameras is pointed at the device by controlling the controllable actuator to position the camera with a user interface. An image of the device generated by the camera is displayed on a mobile and wireless display. The computing device also causes a rendered virtual image of the device to be displayed on the mobile and wireless display. A stream of interest and a region of interest is selected at the mobile and wireless display from the images generated by the cameras.
摘要翻译：公开了用于检查设备的系统和方法。该方法包括将装置相对于多个可移动相机布置在已知位置。多个可移动照相机安装在可控制的致动器上。通过控制可控致动器以使用用户界面定位相机来将多个相机指向设备。相机产生的设备的图像显示在移动和无线显示器上。计算设备还使得设备的渲染虚拟映像显示在移动和无线显示器上。在移动和无线显示器上从相机生成的图像中选择感兴趣的流和感兴趣区域。

2. 发明申请

US20150090882A1 SITU BLADE MOUNTED TIP GAP MEASUREMENT FOR TURBINES 有权
标题翻译：用于涡轮机的SITU叶片安装螺栓间隙测量
公开(公告)号：US20150090882A1
公开(公告)日：2015-04-02
申请号：US14043913
申请日：2013-10-02
申请人： Forrest R. Ruhge , Clifford Hatcher, JR.
发明人： Forrest R. Ruhge , Clifford Hatcher, JR.
IPC分类号： G01B21/16 , G01B11/14
CPC分类号： G01B21/16 , F01D21/003 , F05D2270/80 , F05D2270/821 , G01B11/14 , G01M15/02 , G01N21/8803
摘要： Turbine blade tip clearance is measured in a fully assembled turbine casing by mounting a contact or non-contact displacement probe on a turbine blade that generates data indicative of probe distance from the turbine casing that circumferentially surrounds the blade. Variations in probe distance data are recorded as the blade circumferentially sweeps the turbine casing when the turbine is operated in turning gear mode. Blade rotational position data are collected by a rotational position sensor. A data processing system correlates the distance and rotational position data with localized blade tip gap at angular positions about the turbine casing circumference. An optical camera inspection system may be coupled to a turbine blade to obtain visual inspection information within the turbine casing. This method and apparatus provide an accurate and cost effective solution for accessing turbine casing deformation impact on blade tip clearance and rotor/casing alignment.
摘要翻译：在完全组装的涡轮机壳体中通过将接触或非接触位移探头安装在涡轮机叶片上来测量涡轮叶片顶端间隙，该涡轮叶片产生指示涡轮机壳体周向围绕叶片的探测距离的数据。记录探头距离数据的变化，当涡轮机在转向齿轮模式下操作时刀片周向地扫掠涡轮机壳体。刀片旋转位置数据由旋转位置传感器收集。数据处理系统将距离和旋转位置数据与围绕涡轮机壳体周边的角位置处的局部叶片尖端间隙相关联。光学照相机检查系统可以联接到涡轮机叶片以获得涡轮机壳体内的视觉检查信息。该方法和装置提供了准确和成本有效的解决方案，用于访问涡轮机壳体变形对叶片顶端间隙和转子/壳体对准的影响。

3. 发明申请

US20140053568A1 SYSTEM AND METHOD FOR ON LINE MONITORING WITHIN A GAS TURBINE COMBUSTOR SECTION 有权
标题翻译：用于在气体涡轮搅拌机部分进行在线监测的系统和方法
公开(公告)号：US20140053568A1
公开(公告)日：2014-02-27
申请号：US13856673
申请日：2013-04-04
申请人： Clifford Hatcher, JR. , Richard Hatley , Yakup Genc , Forrest R. Ruhge
发明人： Clifford Hatcher, JR. , Richard Hatley , Yakup Genc , Forrest R. Ruhge
IPC分类号： F02C9/00
CPC分类号： F02C9/00 , F02C7/00 , F05D2260/80 , G01H9/00 , G01J5/0088 , G01J2005/0077 , G01M11/081 , G01M15/14 , G01N21/8806 , G01N21/8851 , G01N21/9515 , G01N21/954 , G01N25/72 , G01N2021/8893
摘要： An on-line optical inspection and monitoring system is externally mounted to existing man way service access within the combustor housing. A replacement man way cover having an optical window is mounted to the combustor housing. One or more optical cameras are oriented so that the camera field of view (FOV) is directed through the man way cover optical window. The camera FOV is moved to plural positions within the combustion section, such as under control of an automated motion control system, and images are captured. Multiple images are combined to form a composite image, which may include an image of an entire transition within the combustion section. Visual images and/or infrared (IR) thermal images may be captured. Thermal image information is correlated with component temperature. Image information is utilized to determine vibration characteristics of the imaged components.
摘要翻译：在线光学检查和监视系统外部安装在燃烧器壳体内的现有人员通道上。具有光学窗口的更换人的盖子安装到燃烧器壳体。一个或多个光学照相机被定向成使得照相机视场（FOV）被引导通过人的方式覆盖光学窗口。摄像机FOV被移动到燃烧部内的多个位置，例如在自动运动控制系统的控制下，捕获图像。多个图像被组合以形成合成图像，其可以包括在燃烧部分内的整个过渡的图像。可以捕获视觉图像和/或红外（IR）热图像。热图像信息与组件温度相关。利用图像信息来确定成像部件的振动特性。

4. 发明申请

US20130335549A1 SYSTEM AND METHOD FOR OPTICAL INSPECTION OF OFF-LINE INDUSTRIAL GAS TURBINES AND OTHER POWER GENERATION MACHINERY WHILE IN TURNING GEAR MODE 有权
标题翻译：离线工业气体涡轮机和其他发电机器在旋转齿轮模式下进行光学检测的系统和方法
公开(公告)号：US20130335549A1
公开(公告)日：2013-12-19
申请号：US13971938
申请日：2013-08-21
申请人： Clifford Hatcher, JR. , Richard Hatley
发明人： Clifford Hatcher, JR. , Richard Hatley
IPC分类号： H04N7/18
CPC分类号： H04N7/18 , F01D21/003 , G01N21/954 , G02B23/2484
摘要： Internal components of gas and steam turbines are inspected with an optical camera inspection system that is capable of automatically and/or manually positioning the camera field of view (FOV) to an area of interest within the turbine along a pre-designated navigation path and capturing images with or without human intervention. Camera positioning and image capture can be initiated automatically or after receipt of operator permission. The inspection system includes an articulated multi-axis inspection scope with an optical camera that is inserted through a combustor nozzle access port, combustor and transition, so that the camera FOV captures the leading edge of Row 1 rotating turbine blades while the rotor is spinning at up to 1000 RPM. An illumination system strobe light and the camera image capture are synchronized with the blade rotation speed so that images of multiple or all blades may be obtained from a single inspection scope insertion point.
摘要翻译：气体和蒸汽涡轮机的内部组件用光学相机检查系统进行检查，该系统能够沿着预先指定的导航路径自动和/或手动将照相机视场（FOV）定位到涡轮内的感兴趣区域并捕获有或没有人为干预的图像。相机定位和图像捕获可以自动启动或在收到操作者许可后启动。检查系统包括铰接式多轴检查镜，其具有通过燃烧器喷嘴入口，燃烧器和过渡部插入的光学摄像机，使得摄像机FOV在转子旋转时捕获行1旋转涡轮叶片的前缘高达1000 RPM。照明系统闪光灯和相机图像捕获与刀片旋转速度同步，使得可以从单个检查范围插入点获得多个或所有刀片的图像。

5. 发明申请

US20130335530A1 SYSTEM AND METHOD FOR VISUAL INSPECTION AND 3D WHITE LIGHT SCANNING OF OFF-LINE INDUSTRIAL GAS TURBINES AND OTHER POWER GENERATION MACHINERY 有权
标题翻译：离线工业气体涡轮机和其他发电机的视觉检测和3D白光扫描系统与方法
公开(公告)号：US20130335530A1
公开(公告)日：2013-12-19
申请号：US13972000
申请日：2013-08-21
申请人： Clifford Hatcher, JR. , Yakup Genc , Richard Hatley , Anton Schick
发明人： Clifford Hatcher, JR. , Yakup Genc , Richard Hatley , Anton Schick
IPC分类号： G01M15/02
CPC分类号： G01M15/02 , F01D21/003 , G01N21/954 , G02B23/2484
摘要： Internal components of gas or steam turbines are inspected with a 3D scanning camera inspection system that is inserted and positioned within the turbine, for example through a gas turbine combustor nozzle port. Three dimensional internal component measurements are performed using projected light patterns generated by a stripe projector and a 3D white light matrix camera. Real time dimensional information is gathered without physical contact, which is helpful for extracting off-line engineering information about the scanned structures. Exemplary 3D scans, preferably with additional visual images, are performed of the gas path side of a gas turbine combustor support housing, combustor basket and transition with or without human intervention.
摘要翻译：气体或蒸汽轮机的内部组件用3D扫描照相机检查系统进行检查，该3D扫描照相机检查系统例如通过燃气轮机燃烧器喷嘴端口插入并定位在涡轮机内。使用由条形投影仪和3D白光矩阵相机产生的投影光图案来执行三维内部部件测量。实时尺寸信息在没有物理接触的情况下被收集，这有助于提取关于扫描结构的离线工程信息。在具有或不具有人为干预的情况下，执行燃气轮机燃烧器支撑壳体，燃烧器筐和转换的气体路径侧的示例性3D扫描，优选地具有附加的视觉图像。

6. 发明申请

US20150125267A1 STANDARDIZED GAS TURBINE INSPECTION PORT SYSTEM 有权
标题翻译：标准气体涡轮检查口系统
公开(公告)号：US20150125267A1
公开(公告)日：2015-05-07
申请号：US14070610
申请日：2013-11-04
申请人： Clifford Hatcher, JR. , James P. Williams
发明人： Clifford Hatcher, JR. , James P. Williams
IPC分类号： F01D21/00 , B23P6/00
CPC分类号： F01D21/003 , F01D25/24 , Y10T29/49238
摘要： A standardized inspection port system with common inspection port bodies and port plugs are incorporated in plural inspection locations within a gas turbine engine casing to facilitate internal engine inspection. The inspection ports preferably have identical internal diameter, stub flange dimensions and axial length from the gas turbine casing inspection seat to the stub flange for standardized mounting of inspection instruments at different locations about the turbine. The inspection port system components are preferably axially and radially aligned along the turbine casing for establishing a common reference position along all turbine blade/vane rows. The port plug incorporates a magnetically attractive pole piece for concentration or redirection of an attractive magnetic field circuit generated by an inspection port plug service tool during plug insertion or retrieval. Magnetic attraction to a service tool enhances controlled plug guidance and reduces likelihood of inadvertent plug loss within the turbine casing.
摘要翻译：在燃气涡轮发动机壳体内的多个检查位置并入有具有通用检查口体和端口塞的标准检查口系统，以便内部发动机检查。检查口优选地具有相同的内径，短柱法兰尺寸和从燃气涡轮机壳体检查座到柱塞法兰的轴向长度，用于在涡轮机周围的不同位置标准安装检验仪器。检查端口系统部件优选地沿着涡轮机壳体轴向和径向对准，以沿着所有涡轮机叶片/叶片行建立共同的参考位置。端口插头包括一个吸引磁极的极片，用于在插头插入或检索期间集中或重定向由检查端口插头服务工具产生的有吸引力的磁场电路。对服务工具的吸引力增强了受控的插头引导，并降低了涡轮机壳体内无意的插头损失的可能性。

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