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    SECTIONED GAS TURBINE ENGINE DRIVEN BY SCO2 CYCLE
    3.
    发明申请
    SECTIONED GAS TURBINE ENGINE DRIVEN BY SCO2 CYCLE 审中-公开
    由SCO2循环驱动的分段气体涡轮发动机

    公开(公告)号：US20170022844A1

    公开(公告)日：2017-01-26

    申请号：US15214423

    申请日：2016-07-19

    申请人： Rolls-Royce Corporation ,  Rolls-Royce North American Technologies, Inc.

    发明人： Thomas E. Bastnagel ,  Igor Vaisman ,  Donald W. Burns ,  Michael J. Armstrong

    IPC分类号： F01K23/08 ,  F01K7/32 ,  F02C3/04 ,  F01K25/10

    CPC分类号： F01K23/08 ,  F01K7/32 ,  F01K25/103 ,  F02C1/005 ,  F02C3/04 ,  F05D2210/12 ,  F05D2210/20 ,  F05D2220/32 ,  F05D2260/213 ,  F05D2270/09 ,  F28D7/005 ,  F28D7/0066 ,  F28D21/001 ,  F28D2021/0026 ,  F28F27/00 ,  F28F27/02 ,  F28F2265/16 ,  Y02T50/675

    摘要： An apparatus, system, and method for a gas turbine engine may include a sectioned heat exchanger. A heat exchanger may include an inlet manifold configured to receive a working fluid. A plurality of circuits including at least first and second circuits configured to transfer heat with respect to the working fluid. Each of the circuits may have a circuit inlet valve, a circuit heat exchange channel, and a circuit outlet valve. The heat exchanger may further include an outlet manifold configured to pass the working fluid to an outlet. The heat exchanger may include a first sensor configured to measure of first parameter of the first circuit and a second sensor configured to measure a second parameter of at least one of the outlet and the second circuit. A controller may be configured to selectively isolate at least one of the plurality of circuits based on a pressure difference between the first and second parameters.

    摘要翻译： 用于燃气涡轮发动机的装置，系统和方法可以包括分段热交换器。 热交换器可以包括配置成接收工作流体的入口歧管。 多个电路包括至少第一和第二电路，其被配置为相对于工作流体传递热量。 每个电路可以具有电路入口阀，回路热交换通道和电路出口阀。 热交换器还可以包括配置成使工作流体通过出口的出口歧管。 热交换器可以包括构造成测量第一电路的第一参数的第一传感器和被配置成测量出口和第二电路中的至少一个的第二参数的第二传感器。 控制器可以被配置为基于第一和第二参数之间的压力差选择性地隔离多个电路中的至少一个。

    ALL CO2 AIRCRAFT
    6.
    发明申请
    ALL CO2 AIRCRAFT 审中-公开

    公开(公告)号：US20170101931A1

    公开(公告)日：2017-04-13

    申请号：US15289267

    申请日：2016-10-10

    申请人： Rolls-Royce North American Technologies, Inc. ,  Rolls-Royce Corporation

    发明人： Michael J. Armstrong ,  Igor Vaisman

    IPC分类号： F02C6/18 ,  F02K3/06 ,  F02C3/04 ,  F02C7/18 ,  B64D27/10 ,  B64D41/00

    摘要： An aircraft power and propulsion system includes an air compressor, a heat rejection heat exchanger, a combustor positioned to receive compressed air from the air compressor as a core stream and provide thrust to the aircraft, and a closed-loop s-CO2 system. The closed-loop s-CO2 system includes carbon dioxide as a working fluid, receives power from the combustor, and rejects heat via the heat rejection heat exchanger to a cooling stream. The closed-loop system s-CO2 configured to provide power to a fan that provides the cooling stream and thrust, and power to the air compressor and at least one auxiliary load.

    Adaptive trans-critical CO2 cooling system
    7.
    发明授权
    Adaptive trans-critical CO2 cooling system 有权

    公开(公告)号：US11448432B2

    公开(公告)日：2022-09-20

    申请号：US16163161

    申请日：2018-10-17

    申请人： Rolls-Royce Corporation ,  Rolls-Royce North American Technologies, Inc.

    发明人： Igor Vaisman ,  Steve T. Gagne ,  Kyle Burkholder

    IPC分类号： F25B9/00 ,  F25B1/10 ,  F25B49/02 ,  F25B11/02 ,  F25B25/00 ,  F25B41/00 ,  F25B5/02 ,  F25B40/00

    摘要： A cooling system includes a heat exchanger through which a refrigerant flows, the heat exchanger having a fluid passing therethrough such that heat is rejected to the fluid, an evaporator, a refrigerant piping split point that receives the refrigerant at a given pressure from the heat exchanger and splits the refrigerant flow into a first circuit and a second circuit, the first circuit having an expansion valve that receives the refrigerant at the given pressure, and the second circuit having a first turbine coupled to a first compressor, wherein the first turbine receives the refrigerant at the given pressure, and a set of valves arranged to direct the refrigerant through the first circuit, the second circuit, or both the first and second circuits based on ambient conditions of the cooling system.