专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US10142565B2 Flash thermography borescope 有权
公开(公告)号：US10142565B2
公开(公告)日：2018-11-27
申请号：US15354004
申请日：2016-11-17
申请人： Siemens Energy, Inc.
发明人： Dustin C. Boudin , Clifford Hatcher, Jr. , Anand A. Kulkarni
IPC分类号： H04N5/33 , H04N7/18 , G02B23/24 , H04N5/225 , A61B1/00
摘要： A flash thermography device for generating an infrared image of each of a plurality of rotating turbine components located inside a turbine. The device includes an infrared sensor for detecting thermal energy radiated by each component. The device also includes a borescope having a viewing end located on a longitudinal axis of the borescope. The borescope is positioned in an inspection port to locate the viewing end inside the turbine such that at least one component is within a field of view of the viewing end. In addition, the device includes a flash source that generates a plurality of light pulses corresponding to the number of components that rotate during a single rotation of the rotor, wherein the light pulses are oriented substantially transverse to the longitudinal. Thermal energy radiated from each component is transmitted through the borescope to the infrared sensor to enable generation infrared images.

2. 发明授权

US10057513B2 Flash thermography device for inspecting turbine components 有权
公开(公告)号：US10057513B2
公开(公告)日：2018-08-21
申请号：US15180364
申请日：2016-06-13
申请人： Siemens Energy, Inc.
发明人： Dustin C. Boudin , Clifford Hatcher, Jr. , Anand A. Kulkarni , Kevin Licata
IPC分类号： H04N5/33 , H04N5/225
CPC分类号： H04N5/332 , G01J5/0088 , G01J5/041 , G01J5/0896 , G01J5/522 , G01J2005/0077 , G01M15/14 , G01N25/20 , G01N25/72 , H04N5/2256
摘要： A flash thermography device for generating an infrared image of a turbine component located inside a turbine. The device includes a flash enclosure having an aperture. A flash source is located in the aperture wherein the flash source generates a light pulse that heats the turbine component. The device also includes an infrared sensor for detecting thermal energy radiated by the turbine component wherein the radiated thermal energy is transmitted through the aperture to the infrared sensor to enable generation of an infrared image of the turbine component.

3. 发明授权

US09618424B2 Gas turbine inspection apparatus and method and system for inspecting a gas turbine 有权
公开(公告)号：US09618424B2
公开(公告)日：2017-04-11
申请号：US14335043
申请日：2014-07-18
申请人： Siemens Energy, Inc.
发明人： Joshua DeAscanis , Clifford Hatcher, Jr. , James P. Williams
IPC分类号： G01M15/14 , G01M15/02
CPC分类号： G01M15/14 , G01M15/02
摘要： A method and a system for inspection of gas turbine are presented. An inspection tool is attached on a track which is permanently positioned on site with respect to the gas turbine. The inspection tool includes an extendible shaft with a proximal end attached on the track and a distal end carrying a sensor. The inspection tool moves along the track for accessing an inspection port of the gas turbine by the shaft. A control system is coupled to the inspection tool for controlling the inspection tool for the inspection of the gas turbine. The method and system enable an automated engine inspection which allows for the engine to have been inspected and reviewed by an engineer without having to send the engineer on site.

4. 发明授权

US09599537B2 Internal inspection of machinery by stitched surface imaging 有权
公开(公告)号：US09599537B2
公开(公告)日：2017-03-21
申请号：US14526609
申请日：2014-10-29
申请人： Siemens Energy, Inc.
发明人： Joshua DeAscanis , William D. Clark , Clifford Hatcher, Jr. , Forrest R. Ruhge
IPC分类号： G01M15/14 , G06T7/00 , F01D21/00 , G02B23/24 , G01N21/954 , G02B13/06 , H04N5/225 , G01M15/02
CPC分类号： G01M15/14 , F01D21/003 , G01M15/02 , G01N21/954 , G02B13/06 , G02B23/2484 , G06T7/0004 , G06T2207/10004 , G06T2207/20221 , G06T2207/30136 , H04N2005/2255
摘要： A method of generating a comprehensive image (87) of interior surfaces (78, 80) of machine components such as a gas turbine combustor basket (59) and transition duct (34) by digitally stitching together multiple photographs (82) thereof, and analyzing the comprehensive image by contouring (91, 95A-B) of colors and shadings thereon, and quantifying and tracking aspects of the contours (A, B, C) over time for indications of degradation (89) of the interior surfaces. A scope (58) may be inserted into a port (56) in the combustor with a camera (72, 74) in a rotatable end (70) of the scope for obtaining a circumferential set (84) of photos at each axial position along a length of the combustor and transition duct. A 3D surface scanning device (76) in the scope may define the geometry of the interior surface for 3D photographic modeling thereof providing a virtual walk-through inspection.

5. 发明授权

US09494487B2 Method for inspecting a turbine engine rotor with a thru bolt threads inspection apparatus 有权
标题翻译：用螺栓螺纹检查装置检查涡轮发动机转子的方法
公开(公告)号：US09494487B2
公开(公告)日：2016-11-15
申请号：US14190781
申请日：2014-02-26
申请人： Siemens Energy, Inc.
发明人： Joshua DeAscanis , James P. Williams , Robert G. Shannon , Forrest R. Ruhge , Clifford Hatcher, Jr.
IPC分类号： H04N5/225 , G01M15/02 , H04N5/247 , H04N5/232 , F01D5/06 , F01D21/00 , F04D19/02 , F04D29/26
CPC分类号： G01M15/02 , F01D5/066 , F01D21/003 , F04D19/02 , F04D29/266 , F05D2230/72 , F05D2260/80 , H04N5/2253 , H04N5/23229 , H04N5/247 , H04N2005/2255
摘要： Turbine engine rotor corresponding thru-bolts and disc cavities are inspected with a camera inspection system that includes one or both of a thru-bolt male threads inspection apparatus and a rotor disc cavity inspection apparatus. The thru-bolts threads inspection apparatus engages the male threads and advances along the bolt threads pattern, selectively capturing camera images at desired spatial positions along the threads pattern. The plural camera threads images are desirably combined to form a composite image of a desired portion of or the entire thru-bolt male threads profiles, which aids their inspection evaluation and provides an archived composite image of the profiles.
摘要翻译：涡轮发动机转子对应的贯穿螺栓和圆盘腔用相机检查系统进行检查，该系统包括一个或两个螺栓外螺纹检查装置和转子盘腔检查装置。螺栓螺纹检查装置与阳螺纹接合并沿着螺栓螺纹图案前进，沿着螺纹图案选择性地捕获在所需空间位置处的摄像机图像。多个相机线程图像期望地组合以形成所需部分或全部贯穿螺栓外螺纹轮廓的合成图像，这有助于其检查评估并提供轮廓的归档合成图像。

6. 发明申请

US20180209296A1 IN-SITU MEASUREMENT OF BLADE TIP-TO-SHROUD GAP IN TURBINE ENGINE 审中-公开
公开(公告)号：US20180209296A1
公开(公告)日：2018-07-26
申请号：US14615487
申请日：2015-02-06
申请人： Siemens Energy, Inc.
发明人： Joshua DeAscanis , David Letter , Alejandro Bancalari , Clifford Hatcher, Jr.
IPC分类号： F01D21/00 , H04N7/18 , H04N5/33 , G01M15/14
CPC分类号： F01D21/00 , G01M15/14 , H04N5/33 , H04N7/18
摘要： A robotically articulated inspection scope (56, 69) inserted into a pilot fuel nozzle port (58) of a turbine engine (20) for in-situ measurement of gaps (59) between tips of turbine blades (40A) and the surrounding shroud (44). A non-contact gap measuring device (52) on a distal end (79) of the scope may be navigated through a combustor (28) and transition duct (34) into a position proximate a blade tip gap. The scope may be controlled via computer (68) via a robotic drive (66) affixed to the pilot fuel nozzle port. Multiple scopes may be used to measure gaps (59A-D) at multiple azimuths of the turbine simultaneously. The turbine disk (37) may be rotated on its operating turning gear to sequentially measure each blade at each azimuth. The computer may memorize an interactively navigated path for subsequent automated positioning.

7. 发明授权

US09948835B2 Single-axis inspection scope with spherical camera and method for internal inspection of power generation machinery 有权
公开(公告)号：US09948835B2
公开(公告)日：2018-04-17
申请号：US15212370
申请日：2016-07-18
申请人： Siemens Energy, Inc.
发明人： Joshua DeAscanis , David Letter , Isaac Piersall , Clifford Hatcher, Jr.
IPC分类号： G01M15/14 , H04N5/225 , H04N5/232 , F01D21/00 , G01M15/02 , G02B23/24 , G01N21/954 , G06T7/00 , G02B13/06
CPC分类号： H04N5/2251 , F01D21/003 , F05D2220/32 , F05D2260/83 , F05D2270/80 , G01M15/02 , G01M15/14 , G01N21/954 , G01N2021/9544 , G02B13/06 , G02B23/2484 , G06T7/97 , G06T2207/20221 , H04N5/2257 , H04N5/23238 , H04N2005/2255
摘要： Internal components of power generation machinery, such as gas turbine engines, are inspected with a spherical optical camera inspection system mounted on a compact diameter, single-axis inspection scope that is capable of insertion within an inspection port or other accessible insertion site. The inspection scope includes nested, non-rotatable telescoping tubes, which define an extension axis. Circumscribing, telescoping tubes have anti-rotation collars, which are in sliding engagement with a mating axial groove on an outer circumferential surface of a circumscribed tube. The camera is advanced and/or retracted along a scope extension axis by nested, drive tubes, which incorporate at least one external drive screw on a circumscribed drive tube and corresponding female threads formed in a circumscribing drive tube. The spherical camera has a 360-degree field of view, and captures images without rotation about the scope extension axis.

8. 发明授权

US09709463B2 Method and system for surface profile inspection of off-line industrial gas turbines and other power generation machinery 有权
公开(公告)号：US09709463B2
公开(公告)日：2017-07-18
申请号：US14732982
申请日：2015-06-08
申请人： Siemens Energy, Inc.
发明人： Joshua DeAscanis , Clifford Hatcher, Jr. , David Letter
IPC分类号： G01M15/14 , G01N21/954 , F01D21/00 , G02B23/24 , G01M15/02
CPC分类号： G01M15/14 , F01D21/003 , G01M15/02 , G01N21/954 , G02B23/2484 , G02B23/2492
摘要： Internal components of power generation machines, such as gas or steam turbines, are inspected with a laser profilometer inspection system that is inserted and positioned within the turbine, for example through an inspection port that is in communication with an open inter-row spacing volume between an opposing turbine vane and turbine blade row. Component surface profile scans are performed to determine relative profile heights along a two-dimensional scan line generated by the profilometer. Three-dimensional profile information is obtained by translating the scan line across the surface. Real time profile information is gathered without physical contact, which is helpful for extracting off-line engineering information about component surface conditions, including surface spallation, perforation, and gaps between components. The system is capable of determining blade tip gap between a turbine blade tip and its opposing abradable surface in the turbine casing.

9. 发明授权

US09681107B2 Flexible tether position tracking camera inspection system for visual inspection of off line industrial gas turbines and other power generation machinery 有权
公开(公告)号：US09681107B2
公开(公告)日：2017-06-13
申请号：US14284437
申请日：2014-05-22
申请人： SIEMENS ENERGY, INC.
发明人： Clifford Hatcher, Jr. , Forrest R. Ruhge
IPC分类号： H04N7/18 , H04N5/225 , F01D21/00 , G02B23/24 , G01N21/954
CPC分类号： H04N7/183 , F01D21/003 , G01N21/954 , G02B23/2476 , G02B23/2484 , H04N5/2251 , H04N2005/2255
摘要： A camera scope inspection system with a flexible, tether mounted camera head that is maneuverable in confined internal cavities of power generation machinery. A camera head position sensing system inferentially determines the three dimension (3D) position of the camera head within the inspected machinery. Camera head position data are correlated with camera image data by a controller. In this manner correlated internal inspection image data and corresponding position data are available for future analysis and image tracking.

10. 发明授权

US09154743B2 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：离合式工业燃气轮机及其他发电机械在转弯档时的光学检测系统及方法
公开(公告)号：US09154743B2
公开(公告)日：2015-10-06
申请号：US13971938
申请日：2013-08-21
申请人： Siemens Energy, Inc.
发明人： Clifford Hatcher, Jr. , Richard Hatley
IPC分类号： G01M15/14 , H04N7/18 , F01D21/00 , G01N21/954 , G02B23/24
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。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式