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公开(公告)号：US10995666B2
公开(公告)日：2021-05-04
申请号：US16186834
申请日：2018-11-12
Applicant: General Electric Company
Inventor： Satoshi Atsuchi , Corey Bourassa , James R. Noel , Erich Alois Krammer , Byron Andrew Pritchard , Mehmet Dede
Abstract: A particle separator includes a separator body in a primary fluid passageway of a machine. The primary fluid passageway includes one or more bleed holes through which a diverted portion of the fluid flowing in the primary fluid passageway toward a volume of the machine is diverted into an auxiliary flow passageway that bypasses the volume and directs the diverted portion of the fluid toward one or more other components of the machine. The separator body is coupled with the inner wall and/or outer wall of the primary fluid passageway. The separator body includes an upstream edge positioned to separate at least some particles carried by the fluid from the fluid as the diverted portion of the fluid bends around and flows over the at least one upstream edge of the separator body and into the auxiliary flow passageway.
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公开(公告)号：US10690055B2
公开(公告)日：2020-06-23
申请号：US15314490
申请日：2015-05-27
Applicant: General Electric Company
Inventor： Curtis Walton Stover , Jonathan Michael Rausch , Satoshi Atsuchi , Gulcharan Singh Brainch , Robert David Briggs , Ronald Scott Bunker , Ambarish Jayant Kulkarni , Michael Alan Meade , Byron Andrew Pritchard , Robert Proctor
Abstract: Gas turbine engine components are provided which utilize an insert to provide cooling air along a cooled surface of an engine component. The insert provides cooling holes or apertures which face the cool side surface of the engine component and direct cooling air onto that cool side surface. The apertures may be formed in arrays and directed at an oblique or a non-orthogonal angle to the surface of the insert and may be at an angle to the surface of the engine component being cooled. An engine component assembly is provided with counterflow impingement cooling, comprising an engine component cooling surface having a cooling fluid flow path on one side and a second component adjacent to the first component. The second component may have a plurality of openings forming an array wherein the openings extend through the second component at a non-orthogonal angle to the surface of the second component.
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公开(公告)号：US20190078515A1
公开(公告)日：2019-03-14
申请号：US16186834
申请日：2018-11-12
Applicant: General Electric Company
Inventor： Satoshi Atsuchi , Corey Bourassa , James R. Noel , Erich Alois Krammer , Byron Andrew Pritchard , Mehmet Dede
Abstract: A particle separator includes a separator body in a primary fluid passageway of a machine. The primary fluid passageway includes one or more bleed holes through which a diverted portion of the fluid flowing in the primary fluid passageway toward a volume of the machine is diverted into an auxiliary flow passageway that bypasses the volume and directs the diverted portion of the fluid toward one or more other components of the machine. The separator body is coupled with the inner wall and/or outer wall of the primary fluid passageway. The separator body includes an upstream edge positioned to separate at least some particles carried by the fluid from the fluid as the diverted portion of the fluid bends around and flows over the at least one upstream edge of the separator body and into the auxiliary flow passageway.
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公开(公告)号：US20150139775A1
公开(公告)日：2015-05-21
申请号：US14086683
申请日：2013-11-21
Applicant: General Electric Company
Inventor： Anurag Kumar , Byron Andrew Pritchard , Chiong Siew Tan
IPC: B01D45/08
Abstract: A system for extracting foreign matter in a gas turbine includes multiple variable bleed valve (VBV) doors disposed on the outer engine casing between a low pressure compressor and a high pressure compressor for bleeding a portion of flow from a core engine flow path into a bypass flow path. The system includes an outlet guide vane (OGV) assembly having multiple guide vanes disposed within the core flow path and multiple support struts positioned downstream from the multiple guide vanes. Each pairs of adjacent support struts comprises at least one VBV door therebetween and a section of the OGV assembly located at an upstream side of the fan hub frame before the each pairs of adjacent support struts. Each section of the OGV assembly includes a first side with one or more guide vanes with trimmed trailing edges configured for directing flow into the at least one VBV door.
Abstract translation: 一种用于在燃气轮机中提取异物的系统包括多个可变排放阀（VBV）门，其设置在外部发动机壳体之间的低压压缩机和高压压缩机之间，用于将来自核心发动机流动路径的一部分流量排出到旁路 流路。 该系统包括出口导叶（OGV）组件，其具有设置在芯流道内的多个导向叶片和位于多个导向叶片下游的多个支撑支柱。 每对相邻的支撑支柱在它们之间包括至少一个VBV门，并且在每对相邻的支撑支柱之间的OGV组件的一部分位于风扇毂框架的上游侧。 OGV组件的每个部分包括具有一个或多个导向叶片的第一侧面，该导向叶片被修剪后缘构造成用于引导流入至少一个VBV门。
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公开(公告)号：US20150114006A1
公开(公告)日：2015-04-30
申请号：US14065840
申请日：2013-10-29
Applicant: General Electric Company
Inventor： Chiong Siew Tan , Byron Andrew Pritchard , Shourya Prakash Otta
IPC: F02C7/20
CPC classification number: F02C7/20 , F01D5/146 , F01D17/08 , F01D21/003 , F01D25/162 , F05D2240/126 , F05D2250/71 , F05D2260/607 , F05D2270/20 , F05D2270/3061 , F05D2270/312 , F05D2270/313 , F05D2270/80 , Y02T50/673 , Y02T50/675 , Y10T29/49229
Abstract: An engine strut for providing fan hub frame structural support and monitoring an air flow within an aircraft engine includes an airfoil coupled to the aircraft engine and has a first portion and a second portion. The first portion is positioned upstream of the second portion with respect to the air flow. A shield is coupled to the engine and positioned between the first portion and the second portion. The shield includes a first side spaced from the first portion and defining a first flow path with the first portion. The shield further includes a second side spaced from the second portion and defining a second flow path with the second portion. At least one sensor is coupled to the aircraft engine and positioned in flow communication with the second flow path.
Abstract translation: 用于提供风扇轮毂框架结构支撑和监测飞行器发动机内的空气流的发动机支柱包括联接到飞行器发动机并具有第一部分和第二部分的翼型件。 第一部分相对于空气流定位在第二部分的上游。 屏蔽件联接到发动机并且定位在第一部分和第二部分之间。 屏蔽包括与第一部分间隔开并且限定具有第一部分的第一流动路径的第一侧。 屏蔽还包括与第二部分间隔开并与第二部分限定第二流路的第二侧。 至少一个传感器耦合到飞行器引擎并且与第二流动路径流动连通地定位。
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Patent Agency Ranking
公开(公告)号：US20240163537A1
公开(公告)日：2024-05-16
申请号：US17985459
申请日：2022-11-11
Applicant: General Electric Company , OLIVER CRISPIN ROBOTICS LIMITED
Inventor： Vamshi Krishna Reddy Kommareddy , Biswajit Medhi , Sandeep Kumar , Byron Andrew Pritchard , Andrew Crispin Graham , Peter John Nisbet
IPC: H04N5/225 , G01N21/954
CPC classification number: H04N5/22525 , G01N21/954 , H04N5/2256 , H04N2005/2255
Abstract: An inspection system and related methods that employ directional light for enhanced imaging are provided. The inspection system includes an inspection camera and at least one directional light source positionable in an offset position from a field of view of the inspection camera. The at least one directional light source is configured to emit directional light from the offset position into the field of view of the inspection camera so as to produce shadows on a surface of interest. Further, the inspection system includes a display device coupled to the inspection camera and the inspection camera is configured to capture one or more images of the shadows produced on the surface of interest. The display device is configured to receive and display the one or more images.
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公开(公告)号：US11815019B2
公开(公告)日：2023-11-14
申请号：US17230095
申请日：2021-04-14
Applicant: General Electric Company
Inventor： Satoshi Atsuchi , Corey Bourassa , James R. Noel , Erich Alois Krammer , Byron Andrew Pritchard , Mehmet Dede
CPC classification number: F02C7/052 , F02C3/06 , F02C9/18 , B01D45/08 , F05D2220/32 , F05D2260/607
Abstract: A particle separator includes a separator body in a primary fluid passageway of a machine. The primary fluid passageway includes one or more bleed holes through which a diverted portion of the fluid flowing in the primary fluid passageway toward a volume of the machine is diverted into an auxiliary flow passageway that bypasses the volume and directs the diverted portion of the fluid toward one or more other components of the machine. The separator body is coupled with the inner wall and/or outer wall of the primary fluid passageway. The separator body includes an upstream edge positioned to separate at least some particles carried by the fluid from the fluid as the diverted portion of the fluid bends around and flows over the at least one upstream edge of the separator body and into the auxiliary flow passageway.
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28.发明公开公开(公告)号：US20230228199A1
公开(公告)日：2023-07-20
申请号：US18180988
申请日：2023-03-09
Applicant: General Electric Company
Inventor： Hrishikesh Keshavan , Byron Andrew Pritchard , Cathleen Ann Hoel , Ambarish Jayant Kulkarni , Michael Solomon Idelchik , Bernard Patrick Bewlay
CPC classification number: F01D5/288 , B23K26/364 , C23C4/11 , C23C28/3215 , C23C28/3455 , F01D5/005 , F01D5/284 , F01D25/007 , F05D2230/90 , F05D2300/611
Abstract: A coated component including a slotted ceramic coating with a reactive phase coating disposed thereon for improved resistance to environmental contaminant compositions, along with methods of its formation, is provided. The coated component may include a substrate defining a surface, a ceramic coating disposed on the surface of the substrate, and a reactive phase coating disposed on the layer of environmental contaminant compositions. The ceramic coating includes a plurality of slots disposed in the ceramic coating forming segments of ceramic coating material.
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公开(公告)号：US20210388763A1
公开(公告)日：2021-12-16
申请号：US17230095
申请日：2021-04-14
Applicant: General Electric Company
Inventor： Satoshi Atsuchi , Corey Bourassa , James R. Noel , Erich Alois Krammer , Byron Andrew Pritchard , Mehmet Dede
Abstract: A particle separator includes a separator body in a primary fluid passageway of a machine. The primary fluid passageway includes one or more bleed holes through which a diverted portion of the fluid flowing in the primary fluid passageway toward a volume of the machine is diverted into an auxiliary flow passageway that bypasses the volume and directs the diverted portion of the fluid toward one or more other components of the machine. The separator body is coupled with the inner wall and/or outer wall of the primary fluid passageway. The separator body includes an upstream edge positioned to separate at least some particles carried by the fluid from the fluid as the diverted portion of the fluid bends around and flows over the at least one upstream edge of the separator body and into the auxiliary flow passageway.
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30.发明授权公开(公告)号：US10692388B1
公开(公告)日：2020-06-23
申请号：US16220431
申请日：2018-12-14
Applicant: General Electric Company
Inventor： Andrew Scott Kessie , Michael H. Fisher , Daniel Maggard , Byron Andrew Pritchard
Abstract: Provided is an engine health management system and method for determining health of an engine of an aircraft, that includes a data source interface which transmits data from internal and external data sources, a control module that includes a processor and a memory and receives data via the data source interface, creates evaluation methods for evaluating the data received to determine suitable data and storing the suitable data within the memory, and creates a controlled historical airport information repository to process historical data via the processor and generate airport information reports based on the historical data. The system also includes a central computing system communicatively coupled with the control module and the data source interface, which performs data enhancement techniques including linking environmental counts and accumulations with engine data.
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