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1. 发明授权

US11435305B2 Thermographic inspection system mounted on motorized apparatus and methods of using same 有权
公开(公告)号：US11435305B2
公开(公告)日：2022-09-06
申请号：US16225044
申请日：2018-12-19
申请人： General Electric Company
发明人： Guanghua Wang , Huan Tan , Bernard Patrick Bewlay
IPC分类号： G01N25/72 , G01N29/22 , G06T7/00 , G01J5/00
摘要： A system for detecting the presence of an anomaly within a component includes a motorized apparatus configured to move around the component. The system also includes an excitation device and a camera mounted to the motorized apparatus. The excitation device is configured to emit an excitation signal toward the component to cause the anomaly within the component to generate a detectable reactionary thermal signal in response to the excitation signal. The camera is configured to capture thermal images of the component. The thermal images include the detectable reactionary thermal signal and indicate the presence of the anomaly within the component. The system further includes a controller communicatively coupled to the excitation device and the camera. The controller is configured to receive and analyze the thermal images to detect the presence of the anomaly within the component. The controller is configured to adjust one or more operating parameters of the system to affect a characteristic of the detectable reactionary signal based on the thermal images.

2. 发明申请

US20220074790A1 SYSTEM AND METHOD FOR DISPOSABLE IMAGING SYSTEM 有权
公开(公告)号：US20220074790A1
公开(公告)日：2022-03-10
申请号：US17530838
申请日：2021-11-19
申请人： General Electric Company
发明人： Guanghua Wang , Naveenan Thiagarajan , Todd Garrett Wetzel , Jason Edward Dees , Bernard Patrick Bewlay
IPC分类号： G01J1/02 , F02C7/12 , G01J5/04 , G01J5/06 , G01J5/00
摘要： An imaging device includes a plurality of electronic components, a phase change material, and a heat transfer structure. The plurality of electronic components is configured to collect data and have a predetermined temperature parameter. The plurality of electronic components is disposed within the phase change material. The phase change material has a first material phase and a second material phase. The phase change material has a first material phase and a second material phase. The phase change material is configured to absorb heat through changing from the first material phase to the second material phase. The heat transfer structure is disposed within the phase change material. The heat transfer structure is configured to conduct heat within the phase change material. The phase change material and the heat transfer structure are further configured to regulate a temperature of the electronic components below the predetermined temperature parameter.

3. 发明授权

US11193820B2 System and method for disposable infrared imaging system 有权
公开(公告)号：US11193820B2
公开(公告)日：2021-12-07
申请号：US15401927
申请日：2017-01-09
申请人： General Electric Company
发明人： Guanghua Wang , Naveenan Thiagarajan , Todd Garrett Wetzel , Jason Edward Dees , Bernard Patrick Bewlay
IPC分类号： G01J1/00 , G01J1/02 , F02C7/12 , G01J5/04 , G01J5/06 , G01J5/00
摘要： An infrared imaging device includes a plurality of electronic components, a phase change material, and a heat transfer structure. The plurality of electronic components is configured to collect data and have a predetermined temperature parameter. The plurality of electronic components is disposed within the phase change material. The phase change material has a first material phase and a second material phase. The phase change material has a first material phase and a second material phase. The phase change material is configured to absorb heat through changing from the first material phase to the second material phase. The heat transfer structure is disposed within the phase change material. The heat transfer structure is configured to conduct heat within the phase change material. The phase change material and the heat transfer structure are further configured to regulate a temperature of the electronic components below the predetermined temperature parameter.

4. 发明授权

US11161128B2 Spray nozzle device for delivering a restorative coating through a hole in a case of a turbine engine 有权
公开(公告)号：US11161128B2
公开(公告)日：2021-11-02
申请号：US15835762
申请日：2017-12-08
申请人： General Electric Company
发明人： Ambarish Jayant Kulkarni , Hrishikesh Keshavan , Mehmet Dede , Bernard Patrick Bewlay , Guanghua Wang , Byron Pritchard , Michael Solomon Idelchik
IPC分类号： B05B7/04 , B05B1/20 , B05B1/30 , B05B7/08 , B05B7/02 , B05B7/14 , B05B7/00 , B05B7/16 , B05B1/04 , B05B1/02 , F01D5/28 , F01D5/00
摘要： An atomizing spray nozzle device includes an atomizing zone housing that receives different phases of materials used to form a coating. The atomizing zone housing mixes the different phases of the materials into a two-phase mixture of ceramic-liquid droplets in a carrier gas. The device also includes a plenum housing fluidly coupled with the atomizing housing and extending from the atomizing housing to a delivery end. The plenum housing includes an interior plenum that receives the two-phase mixture of ceramic-liquid droplets in the carrier gas from the atomizing zone housing. The device also includes one or more delivery nozzles fluidly coupled with the plenum chamber. The delivery nozzles provide outlets from which the two-phase mixture of ceramic-liquid droplets in the carrier gas is delivered onto one or more surfaces of a target object as the coating on the target object.

5. 发明授权

US10830132B2 Micro thermal imaging system for turbine engines 有权
公开(公告)号：US10830132B2
公开(公告)日：2020-11-10
申请号：US15142539
申请日：2016-04-29
申请人： General Electric Company
发明人： Guanghua Wang , Todd Garrett Wetzel , Jason Edward Dees
IPC分类号： F01D17/02 , F02C6/00 , F01D21/00 , H04N5/33
摘要： A turbine engine includes a compressor section, a combustor section fluidly coupled to the compressor section, a turbine section fluidly coupled to the combustor section, and a drive shaft coupled to the turbine section and the compressor section. The turbine engine also includes a plurality of internal components coupled to one of the compressor section, the combustor section, the turbine section, and the drive shaft. The turbine engine also includes at least one micro infrared sensor coupled to at least one of the plurality of internal components. The micro infrared sensor is configured to detect a surface temperature of the plurality of internal components.

6. 发明授权

US09528880B2 Method and system for gas temperature measurement 有权
标题翻译：气体温度测量方法和系统
公开(公告)号：US09528880B2
公开(公告)日：2016-12-27
申请号：US13969186
申请日：2013-08-16
申请人： General Electric Company
发明人： Guanghua Wang , Nirm Velumylum Nirmalan , Ronald Scott Bunker , Todd Garrett Wetzel , Robert Michael Zacharias , Shawn David Wehe , Robert David Briggs
IPC分类号： G01J5/00 , G01K1/14 , G01K13/00 , G01K3/00 , G01J5/10 , G01M15/14 , G01J5/08 , G01J5/60
CPC分类号： G01J5/10 , G01J5/0014 , G01J5/0887 , G01J5/60 , G01M15/14
摘要： A temperature measurement system includes a plurality of filaments. The plurality of filaments are configured to emit thermal radiation in a relatively broad and substantially continuous wavelength band at least partially representative of a temperature of the plurality of filaments. A first and second portion of the filaments has a differing first and a second diameter and/or emissivity, respectively. The system also includes a detector array configured to generate electrical signals at least partially representative of the thermal radiation received from the filaments. The system further includes a controller communicatively coupled to the detector array configured to transform the first electrical signals to a first temperature indication at least partially as a function of the first diameter and/or first emissivity and transform the second electrical signals to a second temperature indication at least partially as a function of the second diameter and/or emissivity.
摘要翻译：温度测量系统包括多个细丝。多根细丝构造成发射至少部分代表多个细丝的温度的相对宽且基本上连续的波长带中的热辐射。长丝的第一和第二部分分别具有不同的第一和第二直径和/或发射率。该系统还包括检测器阵列，该检测器阵列被配置为产生至少部分代表从灯丝接收的热辐射的电信号。所述系统还包括通信地耦合到所述检测器阵列的控制器，所述检测器阵列被配置为至少部分地将所述第一电信号转换为第一温度指示作为所述第一直径和/或第一发射率的函数，并将所述第二电信号转换为第二温度指示至少部分地作为第二直径和/或发射率的函数。

7. 发明申请

US20150147158A1 COOLED AIRFOIL TRAILING EDGE AND METHOD OF COOLING THE AIRFOIL TRAILING EDGE 有权
标题翻译：冷却空气涡轮叶片和冷却空气涡轮叶片的方法
公开(公告)号：US20150147158A1
公开(公告)日：2015-05-28
申请号：US14089920
申请日：2013-11-26
申请人： General Electric Company
发明人： Guanghua Wang , Ronald Scott Bunker , Jeremy Clyde Bailey , James Peter DeLancey , David Benjamin Helmer
IPC分类号： F01D5/18 , F01D9/02
CPC分类号： F01D5/186 , F01D5/187 , F01D9/041 , F01D9/065 , F05D2240/304 , F05D2250/13 , F05D2250/131 , F05D2250/14 , F05D2250/141 , F05D2250/324 , F05D2260/2212 , Y02T50/673 , Y02T50/676
摘要： An airfoil and method of cooling a airfoil including a leading edge, a trailing edge, a suction side, a pressure side and at least one internal cooling channel configured to convey a cooling fluid, is provided. A plurality of trailing edge bleed slots are in fluid communication with the at least one internal cooling channel, wherein a downstream edge of the pressure side of the airfoil lies upstream of a downstream edge of the suction side to expose the plurality of trailing edge bleed slots proximate to the trailing edge of the airfoil. The at least one internal cooling channel is configured to supply the cooling fluid from a source of cooling fluid towards the plurality of trailing edge bleed slots. A plurality of obstruction features are disposed within the at least one internal cooling channel and at a downstream edge of the remaining pressure side. The one or more obstruction features are configured having a predefined substantially polygon shape, to distribute a flow of the cooling fluid and provide distributed cooling to the plurality of trailing edge bleed slots.
摘要翻译：提供了一种用于冷却包括前缘，后缘，吸力侧，压力侧和构造成输送冷却流体的至少一个内部冷却通道的翼型的翼型件和方法。多个后缘排出槽与至少一个内部冷却通道流体连通，其中翼型的压力侧的下游边缘位于吸力侧的下游边缘的上游，以暴露多个后缘排放槽靠近翼型件的后缘。至少一个内部冷却通道构造成将冷却流体从冷却流体源向多个后缘排出槽供应。多个阻塞特征设置在至少一个内部冷却通道内和在剩余压力侧的下游边缘处。一个或多个障碍物特征被构造成具有预定的基本上多边形的形状，以分配冷却流体的流动并且向多个后缘排放槽提供分布式冷却。

8. 发明申请

US20150063412A1 SYSTEMS AND METHODS FOR PLANAR TEMPERATURE MEASUREMENT 有权
标题翻译：用于平面温度测量的系统和方法
公开(公告)号：US20150063412A1
公开(公告)日：2015-03-05
申请号：US14016580
申请日：2013-09-03
申请人： General Electric Company
发明人： Vivek Venugopal Badami , Daniel Francesco Driscoll , Scott Francis Johnson , Paul Joseph Martin , Nilesh Tralshawala , Guanghua Wang
IPC分类号： G01J5/00
CPC分类号： G01J5/0088 , F01D17/085 , F01D25/30 , F05D2270/8041 , G01J5/0014 , G01J2005/0077 , G01J2005/106
摘要： Various embodiments include systems and apparatuses adapted for detecting two-dimensional turbomachine exhaust temperature. In some embodiments, a system includes a two-dimensional grid sized to mount within an exhaust path of a gas turbomachine, a radiation detection device for detecting radiation emitted from the two-dimensional grid at a plurality of points on the two-dimensional grid, the radiation detection device being mountable proximate the exhaust path and the two-dimensional grid and at least one computing device connected with the radiation detection device, the at least one computing device configured to generate a planar map of the temperature of the exhaust from the gas turbomachine based upon the intensity of the radiation emitted from two-dimensional grid detected at the plurality of points on the two-dimensional grid.
摘要翻译：各种实施例包括适于检测二维涡轮机排气温度的系统和装置。在一些实施例中，系统包括尺寸设置成安装在气体涡轮机的排气路径内的二维网格，用于检测在二维网格上的多个点处从二维网格发射的辐射的辐射检测装置，所述辐射检测装置可安装在所述排气路径和所述二维栅格附近，以及与所述辐射检测装置连接的至少一个计算装置，所述至少一个计算装置被配置为生成来自所述气体的排气温度的平面图基于在二维网格上的多个点处检测到的从二维网格发射的辐射的强度的涡轮机。

9. 发明申请

US20140376588A1 SYSTEM AND METHOD FOR ON-LINE OPTICAL MONITORING AND CONTROL OF A GAS TURBINE ENGINE 有权
标题翻译：一种气体涡轮发动机在线光学监测与控制系统与方法
公开(公告)号：US20140376588A1
公开(公告)日：2014-12-25
申请号：US13925635
申请日：2013-06-24
申请人： General Electric Company
发明人： Guanghua Wang , Wontae Hwang , Jeremy Vanderover
IPC分类号： G01J5/00
CPC分类号： G01J5/0088 , G01J5/602 , G01J2005/0077
摘要： A system for on-line optical monitoring of a gas turbine engine includes a viewport into a combustor of the gas turbine engine and an optical filter optically coupled to the viewport. The optical filter is configured to receive broad wavelength band thermal radiation from an interior surface of the combustor while the gas turbine engine is in operation, to substantially block wavelengths of the broad wavelength band thermal radiation emitted and/or absorbed by a flame and/or by exhaust gas within the combustor, and to output narrow wavelength band thermal radiation from the interior surface of the combustor. The system also includes a detector array in optical communication with the optical filter. The detector array is configured to receive the narrow wavelength band thermal radiation and to output signals indicative of a two-dimensional intensity map of the narrow wavelength band thermal radiation.
摘要翻译：用于燃气涡轮发动机的在线光学监测的系统包括进入燃气涡轮发动机的燃烧器的视口和与该视口光学耦合的光学滤波器。光学滤波器被配置为在燃气涡轮发动机运行时从燃烧器的内表面接收宽波长带的热辐射，以基本上阻挡由火焰和/或火焰发射和/或吸收的宽波段的热辐射的波长通过燃烧器内的废气，并且从燃烧器的内表面输出窄波长带的热辐射。该系统还包括与光学滤波器光学通信的检测器阵列。检测器阵列被配置为接收窄波长带的热辐射并输出指示窄波段热辐射的二维强度图的信号。

10. 发明授权

US11492913B2 Cooling hole inspection system 有权
公开(公告)号：US11492913B2
公开(公告)日：2022-11-08
申请号：US16934315
申请日：2020-07-21
申请人： GENERAL ELECTRIC COMPANY
发明人： Guanghua Wang , Bryon Edward Knight , Andrew Lee Trimmer , Jason Edward Dees , Bernard Patrick Bewlay , Sean Robert Farrell
IPC分类号： F01D5/18 , F01D21/00
摘要： An inspection system includes a thermographic sensor configured to capture thermographic data of a component having holes as a fluid is pulsed toward the holes, and one or more processors configured to temporally process the thermographic data to calculate temporal scores and spatial scores for the corresponding holes. The scores can be used to obtain a reference dataset and a test dataset. A performance score can be assigned to the component based on the difference between the datasets.

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