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    Micro gas turbine systems and uses thereof
    1.
    发明授权
    Micro gas turbine systems and uses thereof 有权

    公开(公告)号：US10030580B2

    公开(公告)日：2018-07-24

    申请号：US14684272

    申请日：2015-04-10

    Applicant: Dynamo Micropower Corporation

    Inventor： Jason How-Ring Ethier ,  Ivan Wang ,  Erik Herold ,  Alyssa M. Hatch

    IPC: F01D15/10 ,  F02C6/18 ,  F02C6/00 ,  F02C7/27 ,  F02C3/04 ,  F02C7/264 ,  F02C7/22 ,  F02C7/232 ,  F02C7/04 ,  F02C9/00 ,  F02C7/20 ,  F02C7/06 ,  F02C7/08 ,  F02C7/12 ,  F02C7/224 ,  F02C7/268 ,  F02C3/22 ,  F02C3/24

    Abstract: The present disclosure describes a micro gas turbine flameless heater, in which the heat is generated by burning fuel in a gas turbine engine, and the heater output air mixture is generated by transferring the heat in the gas turbine exhaust to the cold air drawn from the ambient environment. The present disclosure also describes component geometries and system layout for a gas turbine power generation unit that is designed for simple assembly, disassembly, and component replacement. The present disclosure also allows for quick removal of the rotating components of the gas turbine engine in order to reduce assembly and maintenance time. Furthermore, the present disclosure describes features that help to maintain safe operating temperatures for the bearings and structures of the gas turbine engine power turbine. Lastly, the present disclosure describes features of a fuel capture system that allow the injection of wellhead gas, which typically is a mixture of gaseous and liquid fuels, into the combustion chamber, and also describes methods of incorporating afterburners in the gas turbine engine, such that the gas turbine engine system can use wellhead gas to power equipment and reduce emissions from flaring in oil and gas applications.

    Micro gas turbine systems and uses thereof
    4.
    发明授权
    Micro gas turbine systems and uses thereof 有权

    公开(公告)号：US10907543B2

    公开(公告)日：2021-02-02

    申请号：US16016000

    申请日：2018-06-22

    Applicant: Dynamo Micropower Corporation

    Inventor： Erik Herold ,  Jason How-Ring Ethier ,  Alyssa Hatch ,  Ivan Wang

    IPC: F02C7/26 ,  F02C6/18 ,  F02C6/00 ,  F02C7/27 ,  F02C3/04 ,  F02C7/264 ,  F02C7/22 ,  F02C7/232 ,  F02C7/04 ,  F02C9/00 ,  F02C7/20 ,  F02C7/06 ,  F02C7/08 ,  F02C7/12 ,  F02C7/224 ,  F02C7/268 ,  F02C3/22 ,  F02C3/24

    Abstract: The present disclosure describes a micro gas turbine flameless heater, in which the heat is generated by burning fuel in a gas turbine engine, and the heater output air mixture is generated by transferring the heat in the gas turbine exhaust to the cold air drawn from the ambient environment. The present disclosure also describes component geometries and system layout for a gas turbine power generation unit that is designed for simple assembly, disassembly, and component replacement. The present disclosure also allows for quick removal of the rotating components of the gas turbine engine in order to reduce assembly and maintenance time. Furthermore, the present disclosure describes features that help to maintain safe operating temperatures for the bearings and structures of the gas turbine engine power turbine. Lastly, the present disclosure describes features of a fuel capture system that allow the injection of wellhead gas, which typically is a mixture of gaseous and liquid fuels, into the combustion chamber, and also describes methods of incorporating afterburners in the gas turbine engine, such that the gas turbine engine system can use wellhead gas to power equipment and reduce emissions from flaring in oil and gas applications.

    MICRO GAS TURBINE SYSTEMS AND USES THEREOF
    6.
    发明申请
    MICRO GAS TURBINE SYSTEMS AND USES THEREOF 审中-公开

    公开(公告)号：US20190003385A1

    公开(公告)日：2019-01-03

    申请号：US16016000

    申请日：2018-06-22

    Applicant: Dynamo Micropower Corporation

    Inventor： Erik Herold ,  Jason How-Ring Ethier ,  Alyssa Hatch ,  Ivan Wang

    IPC: F02C6/18 ,  F02C7/04 ,  F02C7/12 ,  F02C6/00 ,  F02C7/06 ,  F02C7/268 ,  F02C7/27 ,  F02C7/224 ,  F02C7/232 ,  F02C7/08 ,  F02C7/20 ,  F02C9/00 ,  F02C7/22 ,  F02C7/264 ,  F02C3/24 ,  F02C3/22 ,  F02C3/04

    Abstract: The present disclosure describes a micro gas turbine flameless heater, in which the heat is generated by burning fuel in a gas turbine engine, and the heater output air mixture is generated by transferring the heat in the gas turbine exhaust to the cold air drawn from the ambient environment. The present disclosure also describes component geometries and system layout for a gas turbine power generation unit that is designed for simple assembly, disassembly, and component replacement. The present disclosure also allows for quick removal of the rotating components of the gas turbine engine in order to reduce assembly and maintenance time. Furthermore, the present disclosure describes features that help to maintain safe operating temperatures for the bearings and structures of the gas turbine engine power turbine. Lastly, the present disclosure describes features of a fuel capture system that allow the injection of wellhead gas, which typically is a mixture of gaseous and liquid fuels, into the combustion chamber, and also describes methods of incorporating afterburners in the gas turbine engine, such that the gas turbine engine system can use wellhead gas to power equipment and reduce emissions from flaring in oil and gas applications.

    MICRO GAS TURBINE SYSTEMS AND USES THEREOF
    7.
    发明申请
    MICRO GAS TURBINE SYSTEMS AND USES THEREOF 审中-公开
    微型气体涡轮机系统及其用途

    公开(公告)号：US20150322857A1

    公开(公告)日：2015-11-12

    申请号：US14684272

    申请日：2015-04-10

    Applicant: Dynamo Micropower Corporation

    Inventor： Jason How-Ring Ethier ,  Ivan Wang ,  Erik Herold ,  Alyssa M. Hatch

    IPC: F02C6/18 ,  F02C7/27 ,  F02C3/04 ,  F02C7/264 ,  F02C7/22 ,  F02C7/232 ,  F02C7/04 ,  F02C9/00 ,  F02C7/20 ,  F02C7/06 ,  F02C7/08 ,  F02C7/12 ,  F02C7/224 ,  F02C7/268 ,  F02C6/00

    CPC classification number: F02C6/18 ,  F02C3/04 ,  F02C3/22 ,  F02C3/24 ,  F02C6/00 ,  F02C7/04 ,  F02C7/06 ,  F02C7/08 ,  F02C7/12 ,  F02C7/20 ,  F02C7/22 ,  F02C7/224 ,  F02C7/232 ,  F02C7/264 ,  F02C7/268 ,  F02C7/27 ,  F02C9/00 ,  F05D2220/32 ,  F05D2220/74 ,  F05D2220/76 ,  Y02E20/14 ,  Y10T29/4932

    Abstract: The present disclosure describes a micro gas turbine flameless heater, in which the heat is generated by burning fuel in a gas turbine engine, and the heater output air mixture is generated by transferring the heat in the gas turbine exhaust to the cold air drawn from the ambient environment. The present disclosure also describes component geometries and system layout for a gas turbine power generation unit that is designed for simple assembly, disassembly, and component replacement. The present disclosure also allows for quick removal of the rotating components of the gas turbine engine in order to reduce assembly and maintenance time. Furthermore, the present disclosure describes features that help to maintain safe operating temperatures for the bearings and structures of the gas turbine engine power turbine. Lastly, the present disclosure describes features of a fuel capture system that allow the injection of wellhead gas, which typically is a mixture of gaseous and liquid fuels, into the combustion chamber, and also describes methods of incorporating afterburners in the gas turbine engine, such that the gas turbine engine system can use wellhead gas to power equipment and reduce emissions from flaring in oil and gas applications.

    Abstract translation: 本公开内容描述了一种微型燃气轮机无焰加热器，其中通过在燃气涡轮发动机中燃烧燃料而产生热量，并且通过将燃气轮机排气中的热量传递到从燃气涡轮发动机中抽出的冷空气而产生加热器输出空气混合物 周围环境。 本公开还描述了用于简单组装，拆卸和部件更换的燃气轮机发电单元的部件几何形状和系统布局。 本公开还允许快速去除燃气涡轮发动机的旋转部件，以减少组装和维护时间。 此外，本公开描述了有助于维持燃气涡轮发动机动力涡轮机的轴承和结构的安全工作温度的特征。 最后，本公开描述了燃料捕集系统的特征，其允许将通常是气体和液体燃料的混合物的井口气体喷射到燃烧室中，并且还描述了在燃气涡轮发动机中并入后燃烧器的方法，例如 燃气涡轮发动机系统可以使用井口气体来为设备供电，并减少油气应用中燃烧的排放。

    MICRO GAS TURBINE SYSTEMS AND USES THEREOF
    8.
    发明申请
    MICRO GAS TURBINE SYSTEMS AND USES THEREOF 有权

    公开(公告)号：US20210324792A1

    公开(公告)日：2021-10-21

    申请号：US17164819

    申请日：2021-02-01

    Applicant: Dynamo Micropower Corporation

    Inventor： Erik Herold ,  Jason How-Ring Ethier ,  Alyssa Hatch ,  Ivan Wang

    IPC: F02C6/18 ,  F02C6/00 ,  F02C7/27 ,  F02C3/04 ,  F02C7/264 ,  F02C7/22 ,  F02C7/232 ,  F02C7/04 ,  F02C9/00 ,  F02C7/20 ,  F02C7/06 ,  F02C7/08 ,  F02C7/12 ,  F02C7/224 ,  F02C7/268 ,  F02C3/22 ,  F02C3/24

    Abstract: The present disclosure describes a micro gas turbine flameless heater, in which the heat is generated by burning fuel in a gas turbine engine, and the heater output air mixture is generated by transferring the heat in the gas turbine exhaust to the cold air drawn from the ambient environment. The present disclosure also describes component geometries and system layout for a gas turbine power generation unit that is designed for simple assembly, disassembly, and component replacement. The present disclosure also allows for quick removal of the rotating components of the gas turbine engine in order to reduce assembly and maintenance time. Furthermore, the present disclosure describes features that help to maintain safe operating temperatures for the bearings and structures of the gas turbine engine power turbine. Lastly, the present disclosure describes features of a fuel capture system that allow the injection of wellhead gas, which typically is a mixture of gaseous and liquid fuels, into the combustion chamber, and also describes methods of incorporating afterburners in the gas turbine engine, such that the gas turbine engine system can use wellhead gas to power equipment and reduce emissions from flaring in oil and gas applications.

    GAS TURBINE HEATER AND DUAL FUEL GAS TURBINE ENGINE
    10.
    发明申请
    GAS TURBINE HEATER AND DUAL FUEL GAS TURBINE ENGINE 有权

    公开(公告)号：US20210033024A1

    公开(公告)日：2021-02-04

    申请号：US16945063

    申请日：2020-07-31

    Applicant: Dynamo Micropower Corporation

    Inventor： Jason How-Ring Ethier ,  German Lakov ,  Ivan Wang

    IPC: F02C6/04 ,  F02C9/26

    Abstract: This disclosure teaches a gas turbine heater that can be used in either portable or stationary applications. In one embodiment, a gas turbine heater includes a gas turbine engine that generates hot exhaust gas, an air blower that draws an amount of air flow from ambient, a mixing plenum that allows the gas turbine exhaust and ambient air flow to mix together to create warm air, and an outlet that delivers the warm air to the customer. In another embodiment, a gas turbine heater includes a gas turbine engine that generates hot exhaust gas, an air blower that draws an amount of air flow from ambient, an air-to-air heat exchanger that transfers heat from the gas turbine exhaust to the ambient air flow to create warm air, and an outlet that delivers the warm air to the customer.

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