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    PROCESS FOR CONTROLLING OXIDANT FLOWS IN OPERATION OF A POWER GENERATION PLANT
    21.
    发明申请
    PROCESS FOR CONTROLLING OXIDANT FLOWS IN OPERATION OF A POWER GENERATION PLANT 审中-公开

    公开(公告)号：US20200284194A1

    公开(公告)日：2020-09-10

    申请号：US16825892

    申请日：2020-03-20

    Applicant: 8 RIVERS CAPITAL, LLC

    Inventor： Yasunori IWAI ,  Masao ITOH ,  Shinju SUZUKI ,  Jeremy Eron FETVEDT ,  Rodney John ALLAM

    IPC: F02C7/057 ,  F02C3/34 ,  F02C7/08

    Abstract: A gas turbine facility 10 of an embodiment has a combustor 20 combusting fuel and oxidant, a turbine 28 rotated by combustion gas exhausted from the combustor 20, a heat exchanger 25 cooling the combustion gas from the turbine 28, a pipe 46 guiding a part of the combustion gas to the combustor 20 via the heat exchanger 25, and a pipe 45 exhausting a remaining part of the combustion gas to an outside. Further, the facility has a pipe 40 supplying fuel to the combustor 20, a pipe 41 supplying oxidant to the combustor 20 via the heat exchanger 25, and a pipe 42 branched from the pipe 41, bypassing the heat exchanger 25, and coupled to the pipe 41, so as to introduce the oxidant into the pipe 41.

    Liquid air power and storage with carbon capture
    22.
    发明授权
    Liquid air power and storage with carbon capture 有权

    公开(公告)号：US10738696B2

    公开(公告)日：2020-08-11

    申请号：US15823020

    申请日：2017-11-27

    Applicant: William M. Conlon

    Inventor： William M. Conlon

    IPC: F02C6/14 ,  F02C9/26 ,  F02C6/00 ,  F02C3/22 ,  F02C6/18 ,  F01K23/10 ,  F02C1/02 ,  F02C6/16 ,  F02C7/08 ,  F01K23/18 ,  F25J1/02 ,  F25J1/00

    Abstract: Apparatus, systems, and methods store energy by liquefying a gas such as air, for example, and then recover the energy by regasifying the cryogenic liquid and combusting or otherwise reacting the gas with a fuel to drive a heat engine. Carbon may be captured from the heat engine exhaust by using the cryogenic liquid to freeze carbon dioxide out of the exhaust. The process of liquefying the gas may be powered with electric power from the grid, for example, and the heat engine may be used to generate electricity. Hence, in effect these apparatus, systems, and methods may provide for storing electric power from the grid and then subsequently delivering it back to the grid.

    EFFICIENT AIRCRAFT ENGINE
    25.
    发明申请
    EFFICIENT AIRCRAFT ENGINE 审中-公开

    公开(公告)号：US20200049070A1

    公开(公告)日：2020-02-13

    申请号：US16411862

    申请日：2019-05-14

    Applicant: ROLLS-ROYCE plc

    Inventor： Roderick M. TOWNES ,  Michael J. WHITTLE ,  Pascal DUNNING

    IPC: F02C7/08 ,  F02K3/06 ,  F02C9/16

    Abstract: A highly efficient gas turbine engine is a system wherein the fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.

    Gas turbine engine recuperator with floating connection
    26.
    发明授权
    Gas turbine engine recuperator with floating connection 有权

    公开(公告)号：US10550767B2

    公开(公告)日：2020-02-04

    申请号：US15188277

    申请日：2016-06-21

    Applicant: Pratt & Whitney Canada Corp.

    Inventor： Andreas Eleftheriou ,  David Menheere ,  Daniel Alecu

    IPC: F02C7/08 ,  F28F9/02 ,  F28F9/26 ,  F28D9/00 ,  F28D21/00 ,  F28F21/08

    Abstract: A method of installing a segment of a recuperator within an exhaust duct of a gas turbine engine, including positioning the segment such that its exhaust inlet is in fluid flow communication with the turbine section and its exhaust outlet is adapted to deliver an exhaust flow to atmosphere, engaging its air inlet to a plenum in fluid flow communication with the compressor discharge, and engaging its air outlet to another plenum containing the combustor. One of engaging the air inlet and engaging the air outlet includes forming a rigid connection providing sealed fluid flow communication with the corresponding plenum, and the other of engaging the air inlet and engaging the air outlet includes forming a floating connection providing sealed fluid flow communication with the corresponding plenum. The floating connection allows relative movement of the segment within the exhaust duct.

    MODULAR TURBINE, IN PARTICULAR TURBINE WITH HEAT EXCHANGER FOR PRODUCING ENERGY, IN PARTICULAR ELECTRICAL ENERGY
    27.
    发明申请
    MODULAR TURBINE, IN PARTICULAR TURBINE WITH HEAT EXCHANGER FOR PRODUCING ENERGY, IN PARTICULAR ELECTRICAL ENERGY 审中-公开

    公开(公告)号：US20190234614A1

    公开(公告)日：2019-08-01

    申请号：US16329079

    申请日：2017-07-11

    Applicant: IFP Energies nouvelles

    Inventor： Hubert BAYA TODA ,  Jean-Baptiste MICHEL ,  Julien THIRIOT

    IPC: F23R3/00 ,  F02C7/08

    CPC classification number: F23R3/005 ,  F02C7/08

    Abstract: The present invention is a turbine, particularly a turbine with heat exchanger for the production of energy, particularly electrical energy, comprising at least one compression stage (12) with at least one gas compressor (14), a cross-flow heat exchanger (16) comprising a compressed gas inlet header (60), a compressed gas outlet header (62), a superheated compressed gas inlet header (64), a cooled expanded gas outlet header (66), a combustion chamber (18), at least one expansion stage (20) with at least one expansion turbine (22) connected by a shaft (24) to the compressor, and a means (26) of producing energy.According to the invention, the compressed gas outlet header (62) comprises the combustion chamber (18).

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