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公开(公告)号：US11649735B2
公开(公告)日：2023-05-16
申请号：US17010309
申请日：2020-09-02
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
IPC分类号： F01D25/00 , B08B3/00 , B08B3/08 , B08B3/14 , B08B9/00 , B08B9/032 , F01D25/32 , F02C7/22 , F23R3/28 , B64F5/30
CPC分类号： F01D25/002 , B08B3/003 , B08B3/08 , B08B3/14 , B08B9/00 , B08B9/0326 , F01D25/32 , F02C7/222 , F23R3/28 , B64F5/30 , F05D2220/32 , F05D2230/70 , F05D2230/72 , F23R2900/00019
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：US11261797B2
公开(公告)日：2022-03-01
申请号：US16180459
申请日：2018-11-05
摘要： A vapor-based system and method for treating one or more components of a gas turbine engine. The system includes a treatment compound contained in a storage vessel. The storage vessel being operably coupled to a delivery module. The delivery module delivering the treatment compound at one or more locations of the gas turbine engine such that the treatment compound is a vapor when exposed to an engine air-path.
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公开(公告)号：US10428683B2
公开(公告)日：2019-10-01
申请号：US14987883
申请日：2016-01-05
发明人： Michael Edward Eriksen , David E. Caldwell , Nicole Jessica Tibbetts , Ambarish Jayant Kulkarni , Byron Andrew Pritchard, Jr.
IPC分类号： B24C3/32 , F01D25/00 , B24C1/00 , C11D3/20 , C11D3/38 , C11D11/00 , C11D17/00 , B24C11/00 , C11D3/14
摘要： The present disclosure is directed to a method for in-situ cleaning one or more components of a gas turbine engine using an abrasive gel detergent. More specifically, the gel detergent includes a plurality of abrasive particles suspended in a gel composition. Further, the abrasive particles include organic material. Moreover, the gel composition is formed of a mixture of detergent particles dissolved in a gel reactant. Thus, the method includes injecting the gel detergent into at least a portion of the gas turbine engine at a predetermined pressure. In addition, the method includes allowing the gel detergent to flow across or within one or more of the components of the gas turbine engine so as to clean one or more of the components.
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公开(公告)号：US10227891B2
公开(公告)日：2019-03-12
申请号：US15472456
申请日：2017-03-29
发明人： Michael Edward Eriksen , Keith Anthony Lauria , Ambarish Jayant Kulkarni , Byron Andrew Pritchard, Jr. , David Geoffrey Dauenhauer , Bernard Patrick Bewlay , Nicole Jessica Tibbetts
摘要： A wash system for a gas turbine engine includes a foam generating device configured for receiving and aerating a flow of wash fluid to generate a flow of foamed wash fluid having particular foam characteristics. The flow of foamed wash fluid passes through a distribution manifold where it is selectively directed through a plurality of wash lines to desired portions of the gas turbine engine. The wash system further includes a controller configured for manipulating the foam characteristics of the flow of foamed wash fluid and using the distribution manifold to selectively direct the flow of foamed wash fluid to desired portions of the gas turbine engine for optimal cleaning and improved engine efficiency.
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公开(公告)号：US11702956B2
公开(公告)日：2023-07-18
申请号：US17095396
申请日：2020-11-11
发明人： Ambarish Jayant Kulkarni , Byron Andrew Pritchard, Jr. , Bernard Patrick Bewlay , Michael Edward Eriksen , Nicole Jessica Tibbetts
IPC分类号： F01D25/00 , B01F23/235 , B01F25/31 , B01F25/314 , B01F25/312 , B01F25/313 , B01F101/00
CPC分类号： F01D25/002 , B01F23/235 , B01F25/3111 , B01F25/3143 , B01F25/31243 , B01F25/31331 , B01F2101/4505 , F05D2220/323 , F05D2230/72 , F05D2260/00 , F05D2260/607
摘要： A turbine system includes a foam generating assembly having an in situ foam generating device at least partially positioned within the fluid passageway of the turbine engine, such that the in situ foam generating device is configured to generate foam within the fluid passageway of the turbine engine.
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公开(公告)号：US11591928B2
公开(公告)日：2023-02-28
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
IPC分类号： F01D25/00 , B08B3/00 , B01F23/235 , B01F23/20 , B01F25/31 , B08B9/00 , F01D21/00 , F02C7/22 , F02C7/264 , B01F101/24
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：US11415019B2
公开(公告)日：2022-08-16
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
IPC分类号： F01D25/00 , B08B3/00 , B01F23/235 , B01F23/20 , B01F25/31 , B08B9/00 , F01D21/00 , F02C7/22 , F02C7/264 , B01F101/24
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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公开(公告)号：US10731508B2
公开(公告)日：2020-08-04
申请号：US15451836
申请日：2017-03-07
发明人： Nicole Jessica Tibbetts , Bernard Patrick Bewlay , Ambarish Jayant Kulkarni , Byron Andrew Pritchard, Jr. , Keith Anthony Lauria , Michael Edward Eriksen
摘要： The present disclosure provides methods and systems of generating flows of detergent through a turbine engine to effectuate cleaning of components thereof. The methods include introducing a foamed, acid-including detergent with a pH range of between 2 and 7 into a gas flowpath of the turbine engine. The methods also include creating a pressure differential in an aft portion of the gas flowpath with respect to a forward portion of the gas flowpath to generate a flow of the detergent therethrough. The methods further include creating a pressure differential in a forward portion of the gas flowpath with respect to an aft portion of the gas flowpath to generate a counterflow of the detergent therethrough. The flow and counterflow of the detergent through the gas flowpath interact with components of the turbine engine having foreign material thereon to at least partially remove the foreign material therefrom.
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公开(公告)号：US09915176B2
公开(公告)日：2018-03-13
申请号：US14715700
申请日：2015-05-19
发明人： Robert Carl Murray , Gregory Michael Laskowski , Corey Bourassa , Byron Andrew Pritchard, Jr. , Curtis Walton Stover
CPC分类号： F01D25/24 , F01D25/14 , F02C7/18 , F05D2240/11 , F05D2260/607 , Y02T50/675
摘要： A shroud assembly for a turbine engine includes a shroud having a front side confronting the blades of a turbine and a back side opposite the front side, a hanger configured to couple the shroud to with casing of the turbine, a cooling conduit extending through the hanger to supply a cooling fluid stream to the back side of the shroud, and a particle separator having a through passage forming part of the cooling conduit and a scavenge conduit branching from the through passage.
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公开(公告)号：US12115679B2
公开(公告)日：2024-10-15
申请号：US18384805
申请日：2023-10-27
CPC分类号： B25J9/1669 , B23P6/002 , B25J9/1661 , B25J11/008 , B25J18/00 , B25J19/0062 , B25J19/023 , F01D5/005 , G06Q10/20 , B25J9/1679 , F05D2230/80
摘要： Systems and methods of servicing engines including a method of servicing an engine, the method including navigating at least a portion of a robotic assembly to a location associated with the engine; applying, from the robotic assembly, a medium to one or more adjustable components of the engine while the engine is at an elevated temperature; waiting a duration of time; and with the robotic assembly, operating on the one or more adjustable components.
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