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    Intercooled gas turbine with closed combined power cycle
    11.
    发明授权
    Intercooled gas turbine with closed combined power cycle 有权
    具有闭合组合动力循环的中间燃气轮机

    公开(公告)号：US09410478B2

    公开(公告)日：2016-08-09

    申请号：US14134427

    申请日：2013-12-19

    Applicant: Rolls-Royce North American Technologies, Inc.

    Inventor： James C. Loebig ,  Robert Manning

    IPC: F02C7/143 ,  F02C3/04 ,  F02C7/12 ,  F02K3/06

    CPC classification number: F02C3/04 ,  F02C7/12 ,  F02C7/143 ,  F02K3/06 ,  F05D2210/14 ,  F05D2220/62 ,  F05D2220/72 ,  F05D2220/76 ,  Y02T50/675 ,  Y10T29/49229

    Abstract: A turbine engine includes a fan that provides an air flow to the turbine engine as compressor intake air and as compressor bypass air, a first stage compressor positioned to receive the compressor intake air and output a first stage compressed air, and a boiler positioned to cool the first stage compressed air using a fluid. A second stage compressor is positioned to receive the cooled first stage compressed air. A pump is configured to pump the fluid as a liquid into the boiler, extract energy from the first stage compressed air, and cause the cooling of the first stage compressed air.

    Abstract translation: 涡轮发动机包括风扇，其作为压缩机进气和作为压缩机旁路空气向涡轮发动机提供空气流，定位成接收压缩机进气并输出第一级压缩空气的第一级压缩机和定位成冷却的锅炉 使用流体的第一级压缩空气。 第二级压缩机定位成接收冷却的第一级压缩空气。 泵被配置为将流体作为液体泵送到锅炉中，从第一级压缩空气中提取能量，并使第一级压缩空气冷却。

    Vortex tube particle separators with coatings for rebound control
    12.
    发明授权
    Vortex tube particle separators with coatings for rebound control 有权

    公开(公告)号：US12258903B1

    公开(公告)日：2025-03-25

    申请号：US18371812

    申请日：2023-09-22

    Applicant: Rolls-Royce North American Technologies Inc.

    Inventor： James C. Loebig

    IPC: F02C7/052 ,  B01D45/16 ,  B04C3/00

    Abstract: A vortex particle separator adapted for use with a gas turbine engine includes a vortex tube, a plurality of swirl vanes, and an outlet tube. The vortex tube receives atmospheric air laden with particles. The plurality of swirl vanes are arranged within the vortex tube and separate the atmospheric air into a first flow of air having the particles and a second flow of air that is relatively free of the particles. The outlet tube extends into the vortex tube to define a scavenge passageway between the outlet tube and the vortex tube that receives the first flow of air. The outlet tube defines an intake passageway that receives the second flow of air. The vortex particle separator further includes a layer of material having a low coefficient of restitution on at least one of an interior surface of the vortex tube and a surface of the swirl vanes.

    Check valve for propulsive engine combustion chamber
    14.
    发明授权
    Check valve for propulsive engine combustion chamber 有权
    推进式发动机燃油室用止回阀

    公开(公告)号：US09551299B2

    公开(公告)日：2017-01-24

    申请号：US14202397

    申请日：2014-03-10

    Applicant: Rolls-Royce North American Technologies, Inc. ,  Rolls-Royce Corporation

    Inventor： James C. Loebig ,  Christopher D. DeBruhl ,  John D. Holdcraft

    IPC: F02K7/02 ,  F23R3/04 ,  F23R3/06

    CPC classification number: F02K7/02 ,  F23R3/04 ,  F23R3/06 ,  F23R2900/03041 ,  F23R2900/03042 ,  F23R2900/03341 ,  F23R2900/03342 ,  Y10T29/49229

    Abstract: A combustion chamber includes an inner wall, an outer wall surrounding the inner wall, and a flow passage between the inner wall and outer wall that permits forward flow and restricts reverse flow. The inner wall has a plurality of effusion holes in fluid communication with the inside of the combustion chamber. The outer wall has a plurality of cooling side holes in fluid communication with a cooling source. The inner wall and the outer wall define a flow passage therebetween that fluidly connects one or more of the cooling side holes with one or more of the effusion holes. The flow passage has a geometric configuration to permit forward flow of gases through the flow passage from the cooling source to the inside of the combustion chamber and to restrict reverse flow of gases through the flow passage from the inside of the combustion chamber to the cooling source. The permitted flow rate is greater than the restricted flow rate.

    Abstract translation: 燃烧室包括内壁，围绕内壁的外壁以及允许向前流动并限制反向流动的内壁和外壁之间的流动通道。 内壁具有与燃烧室内部流体连通的多个排出孔。 外壁具有与冷却源流体连通的多个冷却侧孔。 内壁和外壁在其间限定了一个流动通道，其将一个或多个冷却侧孔与一个或多个渗出孔流体连接。 流动通道具有几何构型，以允许气体通过从冷却源到燃烧室内部的流动通道向前流动，并且限制气体从燃烧室内部到冷却源的流动通道的反向流动 。 允许的流量大于限制流量。

    INTERCOOLED GAS TURBINE WITH CLOSED COMBINED POWER CYCLE
    16.
    发明申请
    INTERCOOLED GAS TURBINE WITH CLOSED COMBINED POWER CYCLE 有权
    具有闭合组合功率循环的混合气体涡轮机

    公开(公告)号：US20140352317A1

    公开(公告)日：2014-12-04

    申请号：US14134427

    申请日：2013-12-19

    Applicant: Rolls-Royce North American Technologies, Inc.

    Inventor： James C. Loebig ,  Robert Manning

    IPC: F02C3/04 ,  F02C7/12

    CPC classification number: F02C3/04 ,  F02C7/12 ,  F02C7/143 ,  F02K3/06 ,  F05D2210/14 ,  F05D2220/62 ,  F05D2220/72 ,  F05D2220/76 ,  Y02T50/675 ,  Y10T29/49229

    Abstract: A turbine engine includes a fan that provides an air flow to the turbine engine as compressor intake air and as compressor bypass air, a first stage compressor positioned to receive the compressor intake air and output a first stage compressed air, and a boiler positioned to cool the first stage compressed air using a fluid. A second stage compressor is positioned to receive the cooled first stage compressed air. A pump is configured to pump the fluid as a liquid into the boiler, extract energy from the first stage compressed air, and cause the cooling of the first stage compressed air.

    Abstract translation: 涡轮发动机包括风扇，其作为压缩机进气和作为压缩机旁路空气向涡轮发动机提供空气流，定位成接收压缩机进气并输出第一级压缩空气的第一级压缩机和定位成冷却的锅炉 使用流体的第一级压缩空气。 第二级压缩机定位成接收冷却的第一级压缩空气。 泵被配置为将流体作为液体泵送到锅炉中，从第一级压缩空气中提取能量，并使第一级压缩空气冷却。

    CHECK VALVE FOR PROPULSIVE ENGINE COMBUSTION CHAMBER
    17.
    发明申请
    CHECK VALVE FOR PROPULSIVE ENGINE COMBUSTION CHAMBER 有权
    检查阀用于推进发动机燃烧室

    公开(公告)号：US20140260256A1

    公开(公告)日：2014-09-18

    申请号：US14202397

    申请日：2014-03-10

    Applicant: ROLLS-ROYCE CORPORATION ,  ROLLS-ROYCE NORTH AMERICAN TECHNOLOGIES, INC.

    Inventor： James C. Loebig ,  Christopher D. DeBruhl ,  John D. Holdcraft

    IPC: F02K7/02

    CPC classification number: F02K7/02 ,  F23R3/04 ,  F23R3/06 ,  F23R2900/03041 ,  F23R2900/03042 ,  F23R2900/03341 ,  F23R2900/03342 ,  Y10T29/49229

    Abstract: A combustion chamber includes an inner wall, an outer wall surrounding the inner wall, and a flow passage between the inner wall and outer wall that permits forward flow and restricts reverse flow. The inner wall has a plurality of effusion holes in fluid communication with the inside of the combustion chamber. The outer wall has a plurality of cooling side holes in fluid communication with a cooling source. The inner wall and the outer wall define a flow passage therebetween that fluidly connects one or more of the cooling side holes with one or more of the effusion holes. The flow passage has a geometric configuration to permit forward flow of gases through the flow passage from the cooling source to the inside of the combustion chamber and to restrict reverse flow of gases through the flow passage from the inside of the combustion chamber to the cooling source. The permitted flow rate is greater than the restricted flow rate.

    Abstract translation: 燃烧室包括内壁，围绕内壁的外壁以及允许向前流动并限制反向流动的内壁和外壁之间的流动通道。 内壁具有与燃烧室内部流体连通的多个排出孔。 外壁具有与冷却源流体连通的多个冷却侧孔。 内壁和外壁在其间限定了一个流动通道，其将一个或多个冷却侧孔与一个或多个渗出孔流体连接。 流动通道具有几何构型，以允许气体通过从冷却源到燃烧室内部的流动通道向前流动，并且限制气体从燃烧室内部到冷却源的流动通道的反向流动 。 允许的流量大于限制流量。

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