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    SIMPLIFIED ENGINE BLEED SUPPLY WITH LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM FOR AIRCRAFT
    235.
    发明申请
    SIMPLIFIED ENGINE BLEED SUPPLY WITH LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM FOR AIRCRAFT 有权
    用于飞机的低压环境控制系统的简化发动机供应

    公开(公告)号：US20170022899A1

    公开(公告)日：2017-01-26

    申请号：US14120450

    申请日：2014-06-27

    Applicant: United Technologies Corporation

    Inventor： Frederick M. Schwarz ,  Gabriel L. Suciu

    IPC: F02C6/08 ,  F02C7/32 ,  F02C9/18

    CPC classification number: F02C6/08 ,  B64D13/04 ,  B64D2013/0644 ,  F02C7/32 ,  F02C9/18 ,  F05D2220/323

    Abstract: A gas turbine engine assembly for an aircraft includes a fan section delivering air into a main compressor section. The main compressor section includes a first compressor section and a second compressor section operating at a higher pressure than the first compressor section. The main compressor section compresses air and delivers air into a combustion section where the air is mixed with fuel and ignited to generate products of combustion that are passed over a turbine section to drive the fan section and main compressor sections. An environmental control system includes a low pressure tap at a location on the first compressor section of the main compressor section. The low pressure tap communicates airflow to a first passage leading to a downstream outlet. A compressor is driven by an electric motor. A combined outlet intermixes airflow from the first passage and from the compressor driven by the electric motor and passes the airflow downstream to be delivered to an aircraft use. An environmental control system is also disclosed.

    Abstract translation: 用于飞机的燃气涡轮发动机组件包括将空气输送到主压缩机部分中的风扇部分。 主压缩机部分包括在比第一压缩机部分更高的压力下操作的第一压缩机部分和第二压缩机部分。 主压缩机部分压缩空气并将空气输送到空气与燃料混合并点燃的燃烧部分中，以产生通过涡轮部分驱动风扇部分和主压缩机部分的燃烧产物。 环境控制系统包括在主压缩机部分的第一压缩机部分上的位置处的低压抽头。 低压龙头将气流连通到通向下游出口的第一通道。 压缩机由电动机驱动。 组合的出口将来自第一通道和来自由电动机驱动的压缩机的气流混合，并将下游的气流传递给飞行器使用。 还公开了一种环境控制系统。

    NON-CONTACT SEAL ASSEMBLY FOR ROTATIONAL EQUIPMENT WITH LINKAGE BETWEEN ADJACENT ROTORS
    236.
    发明申请
    NON-CONTACT SEAL ASSEMBLY FOR ROTATIONAL EQUIPMENT WITH LINKAGE BETWEEN ADJACENT ROTORS 审中-公开
    非接触式密封组件用于旋转设备与相邻转子之间的连接

    公开(公告)号：US20170009596A1

    公开(公告)日：2017-01-12

    申请号：US14794516

    申请日：2015-07-08

    Applicant: United Technologies Corporation

    Inventor： Frederick M. Schwarz ,  William K. Ackermann

    IPC: F01D11/08 ,  F04D29/54 ,  F04D29/32 ,  F16J15/44 ,  B64D27/10

    Abstract: An assembly is provided for rotational equipment such as a gas turbine engine for an aircraft propulsion system. This assembly includes a stator, a rotor and a seal assembly. The rotor extends axially along a centerline. The rotor includes a linkage, a first rotor disk, and a second rotor disk. The linkage extends axially from the first rotor disk to the second rotor disk. The linkage is removably attached to the second rotor disk. The seal assembly is configured for sealing a gap radially between the stator and the linkage. The seal assembly includes a hydrostatic non-contact seal.

    Abstract translation: 为旋转设备提供组件，例如用于飞行器推进系统的燃气涡轮发动机。 该组件包括定子，转子和密封组件。 转子沿中心线轴向延伸。 转子包括联动装置，第一转子盘和第二转子盘。 连杆从第一转子盘轴向延伸到第二转子盘。 连杆可拆卸地连接到第二转子盘。 密封组件被构造用于在定子和连接件之间径向密封间隙。 密封组件包括静压非接触式密封。

    SEGMENTED NON-CONTACT SEAL ASSEMBLY FOR ROTATIONAL EQUIPMENT
    237.
    发明申请
    SEGMENTED NON-CONTACT SEAL ASSEMBLY FOR ROTATIONAL EQUIPMENT 审中-公开
    SEGMENTED非接触式密封组件用于旋转设备

    公开(公告)号：US20160376904A1

    公开(公告)日：2016-12-29

    申请号：US14754161

    申请日：2015-06-29

    Applicant: United Technologies Corporation

    Inventor： Frederick M. Schwarz ,  William K. Ackermann

    IPC: F01D11/02 ,  F01D11/00 ,  F16J15/44

    CPC classification number: F01D11/02 ,  F01D11/001 ,  F01D11/025 ,  F05D2220/323 ,  F05D2240/55 ,  F05D2240/56 ,  F05D2260/36 ,  F16J15/44 ,  F16J15/442

    Abstract: An assembly is provided for rotational equipment. The assembly includes a circumferentially segmented stator and a rotor radially within the stator. The assembly also includes a seal assembly configured for substantially sealing a gap radially between the stator and the rotor. The seal assembly includes a carrier and a non-contact seal seated with the carrier. The carrier includes a plurality of discrete carrier segments circumferentially arranged around the non-contact seal.

    Abstract translation: 为旋转设备提供组件。 组件包括周向分段的定子和径向在定子内的转子。 组件还包括密封组件，其被配置为基本上密封定子和转子之间径向的间隙。 密封组件包括载体和与载体一起安置的非接触式密封件。 载体包括围绕非接触式密封件周向布置的多个离散载体片段。

    GEARED TURBOFAN ENGINE WITH TARGETED MODULAR EFFICIENCY
    239.
    发明申请
    GEARED TURBOFAN ENGINE WITH TARGETED MODULAR EFFICIENCY 审中-公开
    具有目标模块效率的齿轮涡轮发动机

    公开(公告)号：US20160265430A1

    公开(公告)日：2016-09-15

    申请号：US14651923

    申请日：2014-09-24

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Frederick M. Schwarz

    IPC: F02C3/107

    CPC classification number: F02C3/107 ,  F01D5/142 ,  F02K3/06 ,  F05D2220/327 ,  F05D2220/36 ,  F05D2260/40311 ,  Y02T50/671 ,  Y02T50/673

    Abstract: A turbofan engine includes a fan section including a fan blade having a leading edge and hub to tip ratio of less than about 0.34 and greater than about 0.020 measured at the leading edge and a speed change mechanism with gear ratio greater than about 2.6 to 1. A first compression section includes a last blade trailing edge radial tip length that is greater than about 67% of the radial tip length of a leading edge of a first stage of the first compression section. A second compression section includes a last blade trailing edge radial tip length that is greater than about 57% of a radial tip length of a leading edge of a first stage of the first compression section.

    Abstract translation: 涡轮风扇发动机包括风扇部分，风扇部分包括风扇叶片，风扇叶片具有在前缘处测量的小于约0.34且大于约0.020的前缘和毂与尖端比率以及齿轮比大于约2.6至1的变速机构。 第一压缩部分包括最大刀片后缘径向尖端长度，其大于第一压缩部分的第一级的前缘的径向尖端长度的约67％。 第二压缩部分包括最大刀片后缘径向尖端长度，其大于第一压缩部分的第一级的前缘的径向尖端长度的约57％。

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