-
公开(公告)号：US11970969B2
公开(公告)日：2024-04-30
申请号：US17809633
申请日：2022-06-29
摘要： An exhaust device for a compressor bypass bleed system of a ducted fan engine includes a housing having an inlet end and an outlet end and defining a centerline axis from the inlet end to the outlet end, an inlet flow conditioner arranged at the inlet end, the inlet flow conditioner including a plurality of inlet openings for conducting a flow of compressed air therethrough into the housing, and an exit screen arranged at the outlet end of the housing. The exit screen includes a plurality of exit openings therethrough arranged at an acute angle with respect to the centerline axis so as to provide a flow of compressed air therethrough into a bypass flow passage at least partially in a same direction as a bypass airflow through the bypass flow passage.
-
公开(公告)号：US11927142B2
公开(公告)日：2024-03-12
申请号：US17872241
申请日：2022-07-25
发明人： Eric R. Westervelt , Stefan Joseph Cafaro , James R. Reepmeyer , Arthur W. Sibbach , Constantinos Minas
CPC分类号： F02C9/52 , F02C7/30 , F05D2260/606 , F05D2270/3015 , F05D2270/303 , F05D2270/306 , F05D2270/804
摘要： Systems and methods are disclosed for estimating or determining a rate or an amount of fuel coke formation in a fuel system, such as of a gas turbine engine. The system is operable to control a rate of fuel coke formation. The system may include a sensor that measures an operating parameter associated with fuel coke formation in the fuel system. A controller is in communication with the sensor to receive the signal therefrom for determining an amount or a rate of fuel coking in the fuel system. Based on this determination the controller may adjust the rate of fuel coke formation by adjusting the operation of the turbine engine, a thermal management system of the turbine engine, or the fuel system.
-
公开(公告)号：US20240026831A1
公开(公告)日：2024-01-25
申请号：US17872241
申请日：2022-07-25
发明人： Eric R. Westervelt , Stefan Joseph Cafaro , James R. Reepmeyer , Arthur W. Sibbach , Constantinos Minas
CPC分类号： F02C9/52 , F02C7/30 , F05D2260/606 , F05D2270/3015 , F05D2270/303 , F05D2270/306 , F05D2270/804
摘要： Systems and methods are disclosed for estimating or determining a rate or an amount of fuel coke formation in a fuel system, such as of a gas turbine engine. The system is operable to control a rate of fuel coke formation. The system may include a sensor that measures an operating parameter associated with fuel coke formation in the fuel system. A controller is in communication with the sensor to receive the signal therefrom for determining an amount or a rate of fuel coking in the fuel system. Based on this determination the controller may adjust the rate of fuel coke formation by adjusting the operation of the turbine engine, a thermal management system of the turbine engine, or the fuel system.
-
4.发明公开公开(公告)号：US20230340910A1
公开(公告)日：2023-10-26
申请号：US18216954
申请日：2023-06-30
发明人： James Robert JARVO , Cedric SAINTIGNAN , Joseph Daniel Maxim CIRTWILL , Kian MCCALDON , Marc-Andre TREMBLAY , David WADDLETON
IPC分类号： F02C7/30 , F02C7/236 , F02C7/232 , F02C7/22 , F02C9/32 , F02C9/42 , F02C7/228 , F02C6/00 , F02C6/16
CPC分类号： F02C7/30 , F02C6/00 , F02C6/16 , F02C7/222 , F02C7/228 , F02C7/232 , F02C7/236 , F02C9/32 , F02C9/42
摘要： Methods and systems of operating a gas turbine engine in a low-power condition are provided. In one embodiment, the method includes supplying fuel to a combustor by supplying fuel to a first fuel manifold and a second fuel manifold of the gas turbine engine. The method also includes, while supplying fuel to the combustor by supplying fuel to the first fuel manifold: stopping supplying fuel to the second fuel manifold; and supplying pressurized air to the second fuel manifold to flush fuel in the second fuel manifold into the combustor and hinder coking in the second fuel manifold and associated fuel nozzles.
-
公开(公告)号：US11661891B1
公开(公告)日：2023-05-30
申请号：US17814334
申请日：2022-07-22
发明人： Narayanan Janakiraman , Paul Mathew , Sreerama Prasad Ramaswamy , Hiranya Nath , Ravindra Shankar Ganiger
CPC分类号： F02C7/30 , F02C7/222 , F05D2220/323 , F05D2260/95 , F05D2300/505 , F05D2300/6111
摘要： A component susceptible to the formation of deposits, such as a component of a hydrocarbon system in a gas turbine engine. The component includes a substrate having a surface susceptible to the formation of a deposit thereon. A shape memory alloy coating is formed on the surface of the substrate. The shape memory alloy coating is a plurality of particles formed on the surface, and each particle of the plurality of particles is formed from a shape memory alloy.
-
公开(公告)号：US20230060569A1
公开(公告)日：2023-03-02
申请号：US17460755
申请日：2021-08-30
申请人： Delavan Inc.
发明人： Jason Ryon , Lev A. Prociw
摘要： A method of operating and cleaning a torch ignitor for continuous ignition includes issuing a fuel-lean flow through a combustion chamber of a torch ignitor. The method also includes heating interior surfaces of the torch ignitor, wherein the fuel-lean flow reacts with carbon deposits on the interior surfaces to remove the carbon deposits.
-
公开(公告)号：US11268449B2
公开(公告)日：2022-03-08
申请号：US16045049
申请日：2018-07-25
IPC分类号： F02C7/30 , G07C5/00 , G05B23/02 , F04D27/00 , F01D21/10 , F01D25/00 , G06Q10/00 , B08B3/02 , B08B13/00 , B08B9/00 , F01D21/00 , F04D29/70
摘要： A wash optimization system and related methods are provided that increase the efficiency and the effectiveness of engine washes. A system comprising at least one processor receives sensor data representing one or more measured parameters of a turbine engine and determines at least one performance parameter based on the sensor data. The at least one performance parameter represents one or more particulate values associated with the turbine engine. The system generates a health state for the turbine engine based on the at least one performance parameter and generates a wash identifier based on the health state of the turbine engine.
-
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.
-
公开(公告)号：US20220056812A1
公开(公告)日：2022-02-24
申请号：US17518901
申请日：2021-11-04
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.
-
公开(公告)号：US11162383B2
公开(公告)日：2021-11-02
申请号：US16678476
申请日：2019-11-08
摘要： Systems and methods are provided for cleaning one or more cooling passages associated with a combustion chamber of a gas turbine engine. The gas turbine engine has a compressor section upstream from the combustion section. The method includes receiving a pressurized fluid from a source and directing the pressurized fluid through an inlet of a chamber such that a portion of a plurality of particles within the chamber is entrained within the pressurized fluid. The method includes injecting the pressurized fluid with the entrained portion of the plurality of particles downstream from the compressor section through an end wall of a diffuser and deswirl system upstream from a combustor plenum of the combustion section to clean the one or more cooling passages associated with the combustion chamber.
-
-
-
-
-
-
-
-
-
搜索结果
236 条记录 (耗时 0.015 秒)
