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公开(公告)号：US20240377060A1
公开(公告)日：2024-11-14
申请号：US18659061
申请日：2024-05-09
Applicant: Air Products and Chemicals, Inc.
Inventor： Mark Daniel D'Agostini , Henry Choisun Chan , Shihong Yan , Zhong Zhou
Abstract: A method for heating reactor using a multi-function burner comprising feeding primary fuel through an annular channel, feeding oxygen through a central channel within the annular channel, and feeding an auxiliary fuel through a central lance within the central channel to produce a flame extending into a furnace having a temperature and a pressure; wherein the flow rate of the auxiliary fuel and oxygen are increased while maintaining an equivalence ratio below 1 to increase the temperature of the furnace; wherein after the furnace temperature exceeds the auto-ignition temperature of the primary fuel, increasing the flow rate of the primary fuel to increase the equivalence ratio to be greater than 1.
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公开(公告)号：US12085282B2
公开(公告)日：2024-09-10
申请号：US18229319
申请日：2023-08-02
Applicant: Air Products and Chemicals, Inc.
Inventor： Mark Daniel D'Agostini , Anup Vasant Sane
Abstract: A hydrogen injection scheme can be employed via use of one or more injectors for injecting hydrogen to help entrain local mass while also generating local turbulence that can enhance mixing with a mixture of air and fuel to facilitate enhanced lean combustion, lower peak flame temperatures of combustion, and reduce nitrous oxide (NOx) emissions from the combustion of fuel. In some embodiments, the hydrogen can be injected to help transport heat released during combustion away from the injector to help avoid injector overheating as well. Different injectors can be utilized to provide a desired hydrogen injection scheme for a particular set of design and operational criteria for a gas turbine system or at least one combustion system that can be utilized in a gas turbine system.
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公开(公告)号：US20220268444A1
公开(公告)日：2022-08-25
申请号：US17678134
申请日：2022-02-23
Applicant: Air Products and Chemicals, Inc.
Inventor： Mark Daniel D'Agostini , Anup Vasant Sane
Abstract: A hydrogen injection scheme can be employed via use of one or more injectors for injecting hydrogen to help entrain local mass while also generating local turbulence that can enhance mixing with a mixture of air and fuel to facilitate enhanced lean combustion, lower peak flame temperatures of combustion, and reduce nitrous oxide (NOx) emissions from the combustion of fuel. In some embodiments, the hydrogen can be injected to help transport heat released during combustion away from the injector to help avoid injector overheating as well. Different injectors can be utilized to provide a desired hydrogen injection scheme for a particular set of design and operational criteria for a gas turbine system or at least one combustion system that can be utilized in a gas turbine system.
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公开(公告)号：US10584051B2
公开(公告)日：2020-03-10
申请号：US15865911
申请日：2018-01-09
Applicant: Air Products and Chemicals, Inc.
Inventor： Mark Daniel D'Agostini , Aleksandar Georgi Slavejkov , Michael David Buzinski , William J. Horan
Abstract: An oxy-fuel burner including a central burner element having a central conduit terminating in a central nozzle and an annular conduit terminating in an annular nozzle surrounding the central conduit, the central conduit flowing a first reactant and the annular conduit flowing a second reactant; a first staging conduit spaced apart from a side of the central burner element and terminating in a first staging nozzle; a second staging conduit spaced apart from an opposite side the central burner element and terminating in a second staging nozzle; a first mechanism to apportion a flow of the second reactant into a non-zero primary flow of the second reactant directed to the annular conduit and a non-zero secondary flow of the second reactant; and a second mechanism to selectively apportion the secondary flow of the second reactant between the staging conduits; wherein one reactant is fuel and the other reactant is oxygen.
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公开(公告)号：US10571121B2
公开(公告)日：2020-02-25
申请号：US15320572
申请日：2015-06-23
Applicant: Air Products and Chemicals, Inc.
Inventor： Mark Daniel D'Agostini , Anup Vasant Sane , Avishek Guha
Abstract: An oxy-gaseous fuel burner (400, 500) or a solid fuel burner (700) having an annular cavity (404, 504, 704) upstream from and proximate to an outlet plane (416, 516, 716) and a converging (434, 734) or converging-diverging nozzle (537) located upstream from and proximal to the cavity (404, 504, 704). The solid fuel burner (700) also is preferably operated so that the velocity of gas exiting a second annulus (730) is less than the velocity of gas exiting a central conduit (710).
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Patent Agency Ranking
公开(公告)号：US20240019123A1
公开(公告)日：2024-01-18
申请号：US18229319
申请日：2023-08-02
Applicant: Air Products and Chemicals, Inc.
Inventor： Mark Daniel D'Agostini , Anup Vasant Sane
Abstract: A hydrogen injection scheme can be employed via use of one or more injectors for injecting hydrogen to help entrain local mass while also generating local turbulence that can enhance mixing with a mixture of air and fuel to facilitate enhanced lean combustion, lower peak flame temperatures of combustion, and reduce nitrous oxide (NOx) emissions from the combustion of fuel. In some embodiments, the hydrogen can be injected to help transport heat released during combustion away from the injector to help avoid injector overheating as well. Different injectors can be utilized to provide a desired hydrogen injection scheme for a particular set of design and operational criteria for a gas turbine system or at least one combustion system that can be utilized in a gas turbine system.
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公开(公告)号：US11592178B2
公开(公告)日：2023-02-28
申请号：US17055445
申请日：2019-05-15
Applicant: Air Products and Chemicals, Inc.
Inventor： Mark Daniel D'Agostini , Anup Vasant Sane
Abstract: A combustor for a gas turbine engine having a compressor upstream of the combustor and a turbine downstream of the combustor. The combustor also includes a combustor chamber, an oxy-fuel pilot burner (104) centrally positioned at an end of the combustor chamber, and an air-fuel premix burner configured to at least partially premix air and fuel. The air-fuel premix burner surrounds the oxy-fuel pilot burner (104) in an annular configuration.
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公开(公告)号：US20210372611A1
公开(公告)日：2021-12-02
申请号：US16884418
申请日：2020-05-27
Applicant: Air Products and Chemicals, Inc.
Inventor： Mark Daniel D'Agostini , Michael J. Gallagher , Ashwin Vinod
Abstract: A burner gas supply apparatus for increasing flame turbulence, the apparatus comprising a conduit having a characteristic width, W, defined by an inner surface having a circumferential direction and an axial direction, the axial direction terminating in a nozzle defining a nozzle exit plane and having a characteristic dimension, d, where d
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公开(公告)号：US10295184B2
公开(公告)日：2019-05-21
申请号：US15026309
申请日：2015-04-29
Applicant: Air Products and Chemicals, Inc.
Inventor： Christopher Michael Albright , Reed Jacob Hendershot , Michael J. Gallagher , Thomas David Matthew Lee , Aleksandar Georgi Slavejkov , Mark Daniel D'Agostini , Tunc Goruney
Abstract: An oxy-fuel burner (10) with monitoring including a fuel passage (320) terminating in a fuel nozzle (322), a primary oxidant passage (330) terminating in an oxidant nozzle (333), one or more sensors including a nozzle temperature sensor (372) for sensing at least one of an oxidant nozzle temperature and a fuel nozzle temperature, and a data processor (66, 166,266) programmed to receive data from the sensors and to determine based on at least a portion of the received data the presence or absence of an abnormal burner condition including a potential partial obstruction of at least one of the primary oxidant passage (330) and the fuel passage (320) based on an increase or decrease in at least one of the oxidant nozzle temperature and the fuel nozzle temperature.
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公开(公告)号：US20140305356A1
公开(公告)日：2014-10-16
申请号：US14224696
申请日：2014-03-25
Applicant: Air Products and Chemicals, Inc.
Inventor： Mark Daniel D'Agostini , Stephane Bernard Poussou
CPC classification number: F23L7/007 , F23D1/00 , F23D2201/10 , F23D2201/20 , Y02E20/344
Abstract: A wide-flame solid fuel/oxygen burner including a fuel nozzle having an aspect ratio of at least about 2 defined by the ratio of a fuel nozzle width, W, measured along a major axis centerline, to a fuel nozzle height, H, measured along a minor axis centerline, and long walls spaced substantially symmetrically from the major axis centerline, the fuel nozzle having an inlet width, WN; and a pair of guide vanes positioned on either side of the major axis centerline between that centerline and an adjacent long wall, the guide vanes diverging from the major axis centerline in the flow direction by an angle such that the guide vanes are closer together at an upstream end and farther apart at a downstream end, thereby forming a central diffuser between the guide vanes and an outer converging nozzle between each guide vane and one of the long walls.
Abstract translation: 一种宽火焰固体燃料/氧气燃烧器，包括具有至少约2的纵横比的燃料喷嘴，该燃料喷嘴的长轴中心线所测量的燃料喷嘴宽度W与燃料喷嘴高度之比H确定 沿着短轴中心线以及与主轴中心线基本上对称分开的长壁，燃料喷嘴具有入口宽度WN; 以及一对导向叶片，其位于该中心线和相邻长壁之间的长轴中心线的任一侧上，导向叶片沿主流轴中心线沿流动方向发散一定角度，使得导向叶片在一个 上游端和下游端分开更远，由此在导向叶片与每个导叶与其中一个长壁之间的外部会聚喷嘴之间形成中心扩散器。
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