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公开(公告)号:US20230271723A1
公开(公告)日:2023-08-31
申请号:US18144050
申请日:2023-05-05
发明人: Todd William Danko , Ambarish Jayant Kulkarni , Margeaux Wallace , Hrishikesh Keshavan , Bernard Patrick Bewlay , Byron Andrew Pritchard, JR. , Michael Dean Fullington , Andrew Crispin Graham , Trevor Owen Hawke , Julian Matthew Foxall , Ahmed M. ELKady
CPC分类号: B64F5/40 , B05B15/68 , B05B15/70 , B05B12/124 , G01N21/8851 , G01N21/954
摘要: A method for inspecting and repairing a surface of a component of a gas turbine engine, the method including: inserting an inspection and repair tool into an interior of the gas turbine engine; inspecting the surface of the component with the inspection and repair tool; performing a repair of the surface of the component with the inspection and repair tool from within the interior of the gas turbine engine, the inspection and repair tool remaining within the interior of the gas turbine engine between inspecting the component and performing the repair of the surface of the component.
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公开(公告)号:US20190107005A1
公开(公告)日:2019-04-11
申请号:US15727269
申请日:2017-10-06
发明人: Ambarish Jayant Kulkarni , Keith Anthony Lauria , Michael Edward Eriksen , Nicole Jessica Tibbetts , Bernard Patrick Bewlay , Byron Andrew Pritchard, JR. , Shantanu M. Sane
摘要: A turbine engine cleaning system includes a foaming nozzle. The foaming nozzle includes a wall having a thickness between an outer surface of the wall and an inner surface of the wall. The outer surface of the wall is configured to contact a detergent in which the foaming nozzle is configured to be disposed. The inner surface of the wall surrounds an inner plenum of the foaming nozzle, and the inner plenum is configured to receive an aerating gas. The foaming nozzle also includes a first row of first through holes fluidly coupled to, and extending between, a first row of first through hole inlets at the inner surface of the wall and a first row of first through hole outlets at the outer surface of the wall. The foaming nozzle also includes a second row of second through holes disposed axially adjacent to the first row of second through holes with respect to a longitudinal axis of the inner plenum, where the second row of second through holes is fluidly coupled to, and extending between, a second row of second through hole inlets at the inner surface of the wall and a second row of second through hole outlets at the outer surface of the wall. The foaming nozzle also includes cross-sections of the first through holes and the second through holes having regular shapes.
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公开(公告)号:US20180245477A1
公开(公告)日:2018-08-30
申请号:US15443048
申请日:2017-02-27
发明人: Ambarish Jayant Kulkarni , Bernard Patrick Bewlay , Byron Andrew Pritchard, JR. , Nicole Jessica Tibbetts , Michael Edward Eriksen , Eric John Telfeyan
摘要: A method for cleaning components of a gas turbine engine is presented. The method includes introducing a working fluid into a gas flow path or a cooling circuit defined by the one or more components of the gas turbine engine such that the working fluid impinges upon a surface of the one or more components of the gas turbine engine, wherein the working fluid includes a plurality of detergent droplets entrained in a flow of steam. A system for cleaning components of a gas turbine engine are also presented.
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公开(公告)号:US20240159162A1
公开(公告)日:2024-05-16
申请号:US18420402
申请日:2024-01-23
发明人: Mandar Diwakar Godbole , Byron Andrew Pritchard, JR. , Kirti Arvind Petkar , Vamshi Krishna Reddy Kommareddy , Sandeep Kumar , Andrew Crispin Graham
CPC分类号: F01D21/003 , G01M15/14 , G06T7/001 , G06T7/60 , F05D2260/80 , F05D2270/8041 , G06T2207/30164
摘要: A system and method of using a tool assembly is provided. The system includes a body, a first camera and a second camera fixed to the body, and a controller. The controller is configured to receive data indicative of images of a reference feature from the first camera, determine data indicative of a first spatial position of the first camera based at least in part on the received data indicative of the images of the reference feature, and determine data indicative of a second spatial position of the second camera based on the first spatial position, a known spatial relationship between the first location and the second location, or both. Further, the controller may be configured to receive data indicative of images of a target feature using the second camera, derive dimensions of the target feature based on the images, and generate a three-dimensional representation of the target feature.
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公开(公告)号:US20220389834A1
公开(公告)日:2022-12-08
申请号:US17889629
申请日:2022-08-17
发明人: Byron Andrew Pritchard, JR. , Keith Anthony Lauria , Erica Elizabeth Sampson , Bernard Patrick Bewlay , Ambarish Jayant Kulkarni , Michael Robert Millhaem , William Francis Navojosky , Nicole Jessica Tibbetts , Gongguan Wang , Andrew Crispin Graham
摘要: Systems and methods for treating a component of an installed and assembled gas turbine engine are provided. Accordingly, the method includes operably coupling a delivery assembly to an annular inlet of a core gas turbine engine. A portion of treating fluid is atomized with the delivery assembly to develop a treating mist having a plurality of atomized droplets. The atomized droplets are suspended within any path of the core gas turbine engine from the annular inlet to an axial position downstream of a compressor of the core gas turbine engine. A portion of the treating mist is impacted or precipitated onto the component so as to wet the component, and a portion of the deposits on the component is dissolved by the treating mist.
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公开(公告)号:US20220138699A1
公开(公告)日:2022-05-05
申请号:US17083600
申请日:2020-10-29
发明人: Andrew Crispin Graham , David Scott Diwinsky , Byron Andrew Pritchard, JR. , Julian Matthew Foxall
摘要: A method of servicing aviation equipment including at least partially-autonomously inspecting components of the equipment using an environmental capture device, wherein at least partially-autonomous inspection includes: capturing information associated with the equipment using the environmental capture device; identifying the components of the equipment using one or more computing devices; determining, by the one or more computing devices, whether each identified component is properly positioned relative to the equipment using reference information; and for components not properly positioned relative to the equipment, determining if there is damage to the component or equipment.
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公开(公告)号:US20200248583A1
公开(公告)日:2020-08-06
申请号:US16855795
申请日:2020-04-22
发明人: Ambarish Jayant Kulkarni , Bernard Patrick Bewlay , Byron Andrew Pritchard, JR. , Nicole Jessica Tibbetts , Michael Edward Eriksen , Stephen Wilton
摘要: Embodiments in accordance with the present disclosure include a meta-stable detergent based foam generating device of a turbine cleaning system includes a manifold configured to receive a liquid detergent and an expansion gas, a gas supply source configured to store the expansion gas, and one or more aerators fluidly coupled with, and between, the gas supply source and the manifold. Each aerator of the one or more aerators comprises an orifice through which the expansion gas enters the manifold, and wherein the orifice of each aerator is sized to enable generation of a meta-stable detergent based foam having bubbles with bubble diameters within a range of 10 microns (3.9×10−4 inches inches) and 5 millimeters (0.2 inches), having a half-life within a range of 5 minutes and 180 minutes, or a combination thereof.
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公开(公告)号:US20180313225A1
公开(公告)日:2018-11-01
申请号:US15498141
申请日:2017-04-26
发明人: Michael Robert Millhaem , Nicole Jessica Tibbetts , Byron Andrew Pritchard, JR. , Bernard Patrick Bewlay , Keith Anthony Lauria , Ambarish Jayant Kulkarni , Mark Rosenzweig , Martin Matthew Morra , Timothy Mark Sambor , Andrew Jenkins
CPC分类号: F01D25/002 , B08B9/00 , B64F5/30 , F01D25/00
摘要: A method of cleaning a component within a turbine that includes disassembling the turbine engine to provide a flow path to an interior passageway of the component from an access point. The component has coked hydrocarbons formed thereon. The method further includes discharging a flow of cleaning solution towards the interior passageway from the access point, wherein the cleaning solution is configured to remove the coked hydrocarbons from the component.
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公开(公告)号:US20170254218A1
公开(公告)日:2017-09-07
申请号:US15057179
申请日:2016-03-01
发明人: Bernard Patrick Bewlay , Brian Alan Kalb , Nicole Jessica Tibbetts , Ambarish Jayant Kulkarni , Byron Andrew Pritchard, JR.
CPC分类号: F01D25/002 , B08B7/02 , B08B9/00 , B08B9/08 , B24B31/006 , B24C1/00 , B24C3/327 , B24C11/00 , F04D19/00 , F05D2220/32 , F05D2240/128 , F05D2240/24 , F05D2240/30 , F05D2240/35 , F05D2260/20
摘要: The present disclosure is directed to a system and method for in-situ (e.g. on-wing) cleaning of gas turbine engine components. The method includes injecting a dry cleaning medium into the gas turbine engine at one or more locations. The dry cleaning medium includes a plurality of abrasive microparticles. Thus, the method also includes circulating the dry cleaning medium through at least a portion of the gas turbine engine such that the abrasive microparticles abrade a surface of the one or more components so as to clean the surface.
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公开(公告)号:US20170167290A1
公开(公告)日:2017-06-15
申请号:US14967043
申请日:2015-12-11
发明人: Ambarish Jayant Kulkarni , Bernard Patrick Bewlay , Byron Andrew Pritchard, JR. , Nicole Jessica Tibbetts , Michael Edward Eriksen , Stephen Wilton
CPC分类号: F01D25/002 , B01F3/04446 , B01F3/04992 , B01F5/0406 , B01F5/0411 , B01F2215/004 , B08B3/003 , B08B9/00 , F01D21/003 , F02C7/22 , F02C7/264 , F05D2220/32 , Y02E20/14
摘要: Embodiments in accordance with the present disclosure include a meta-stable detergent based foam generating device of a turbine cleaning system includes a manifold configured to receive a liquid detergent and an expansion gas, a gas supply source configured to store the expansion gas, and one or more aerators fluidly coupled with, and between, the gas supply source and the manifold. Each aerator of the one or more aerators comprises an orifice through which the expansion gas enters the manifold, and wherein the orifice of each aerator is sized to enable generation of a meta-stable detergent based foam having bubbles with bubble diameters within a range of 10 microns (3.9×10−4 inches) and 5 millimeters (0.2 inches), having a half-life within a range of 5 minutes and 180 minutes, or a combination thereof.
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