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    ENERGY FLOW
    93.
    发明申请
    ENERGY FLOW 审中-公开

    公开(公告)号：US20170341759A1

    公开(公告)日：2017-11-30

    申请号：US15604526

    申请日：2017-05-24

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Louis J. Bruno ,  Harold W. Hipsky

    IPC: B64D13/02 ,  B64D13/08 ,  B64D13/06

    CPC classification number: B64D13/02 ,  B64D13/08 ,  B64D2013/0618 ,  B64D2013/0644 ,  B64D2013/0648 ,  F02C1/02 ,  F02C6/08 ,  F05D2220/323 ,  F05D2220/62

    Abstract: An airplane is provided. The airplane includes a compressing device including a turbine and a compressor. The turbine includes first and second inlets and provides energy by expanding one or more mediums. The first inlet is receives a first medium of the one or more mediums. The second inlet receives a second medium of the one or more mediums. The compressor receives a first energy derived from the first and second mediums being expanded across the turbine during a first mode of the compressing device, receives a second energy derived from the first medium being expanded across the turbine during a second mode of the compressing device, and compresses the second medium in accordance with the first mode or the second mode.

    HEAT EXCHANGING VALVE ARRANGEMENT
    97.
    发明申请
    HEAT EXCHANGING VALVE ARRANGEMENT 有权
    热交换阀装置

    公开(公告)号：US20170045155A1

    公开(公告)日：2017-02-16

    申请号：US14825925

    申请日：2015-08-13

    Applicant: HAMILTON SUNDSTRAND CORPORATION

    Inventor： Donald E. Army, JR. ,  Louis J. Bruno

    IPC: F16K49/00 ,  F01D17/14 ,  B64D13/00 ,  F16K11/085

    CPC classification number: F16K49/007 ,  B64D13/00 ,  F01D17/145 ,  F16K11/0853

    Abstract: A heat exchanging valve arrangement includes, a manifold defining a chamber, a first passageway, a second passageway, a third passageway, and a fourth passageway, and a member movable relative to the manifold configured to define fluidic communication between the first passageway and the second passageway when in a first position and between the first passageway and the third passageway when in a second position, fluid is flowable into the chamber through the fourth passageway such that fluid is exposed to surfaces of the member regardless of whether the member is in the first position or the second position.

    Abstract translation: 热交换阀装置包括：限定腔室的歧管，第一通道，第二通道，第三通道和第四通道，以及可相对于歧管移动的构件，其构造成限定第一通道和第二通道之间的流体连通 当处于第一位置时，在第一通道和第三通道之间的通道当处于第二位置时，流体可以通过第四通道流入室中，使得流体暴露于构件的表面，而不管构件是否处于第一位置 位置或第二位置。

    ENVIRONMENTAL AIR CONDITIONING SYSTEM
    98.
    发明申请
    ENVIRONMENTAL AIR CONDITIONING SYSTEM 有权
    环境空调系统

    公开(公告)号：US20160146114A1

    公开(公告)日：2016-05-26

    申请号：US14553335

    申请日：2014-11-25

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Louis J. Bruno

    IPC: F02C9/18 ,  F02C3/04

    CPC classification number: F02C9/18 ,  B64D13/06 ,  B64D2013/0611 ,  B64D2013/0618 ,  B64D2013/0648 ,  B64D2013/0688 ,  F02C3/04 ,  Y02T50/56

    Abstract: An environmental air conditioning system is described for conditioning compressed air for supply as conditioned air. The system includes an airflow path to which the compressed air for ultimate distribution as conditioned air (i.e., airflow path compressed air) is supplied. Then airflow path has various components of an air cycle system, and also includes a power turbine outside of the air cycle that receives compressed air and discharges it as exhaust. The power turbine transfers power to a compressor in the air cycle system.

    Abstract translation: 描述了一种环境空调系统，用于调节作为调节空气供应的压缩空气。 该系统包括气流路径，用于作为调节空气（即，气流路径压缩空气）的最终分配的压缩空气被供应到该气流路径。 然后，气流路径具有空气循环系统的各种部件，并且还包括接收压缩空气并将其作为排气排出的空气循环外的动力涡轮机。 动力涡轮机将动力传送到空气循环系统中的压缩机。

    ENVIRONMENTAL CONTROL SYSTEM UTILIZING SHOESTRING CYCLE TO MAXIMIZE EFFICIENCY
    99.
    发明申请
    ENVIRONMENTAL CONTROL SYSTEM UTILIZING SHOESTRING CYCLE TO MAXIMIZE EFFICIENCY 有权
    环境控制系统利用鞋袜周期实现最大化效率

    公开(公告)号：US20150307195A1

    公开(公告)日：2015-10-29

    申请号：US14695576

    申请日：2015-04-24

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Louis J. Bruno

    IPC: B64D13/06 ,  F02C6/08

    CPC classification number: B64D13/06 ,  B64D2013/0618 ,  B64D2013/0648 ,  B64D2013/0688 ,  F02C6/08 ,  Y02T50/56

    Abstract: An environmental control system comprising that utilizes recirculation air. The environmental control system includes an inlet configured to supply bleed air at a first energy from a source to the environmental control system, where the environmental control system supplies the bleed air at a second energy to a chamber. The environmental control system also includes an air cycle machine comprising a compressor and a turbine, where the air cycle machine receives the recirculation air from the chamber and the recirculation air is bleed air at a third energy flowing from the chamber to the air cycle machine.

    Abstract translation: 包括利用再循环空气的环境控制系统。 环境控制系统包括入口，该入口构造成以从源到环境控制系统的第一能量提供排放空气，其中环境控制系统将排出的空气以第二能量供应到室。 环境控制系统还包括一个包括压缩机和涡轮机的空气循环机，其中空气循环机器从腔室接收再循环空气，再循环空气以从腔室到空气循环机器的第三能量排出空气。

    HYBRID POWER SYSTEM ARCHITECTURE FOR AN AIRCRAFT
    100.
    发明申请
    HYBRID POWER SYSTEM ARCHITECTURE FOR AN AIRCRAFT 有权
    混合动力系统架构的飞机

    公开(公告)号：US20130306790A1

    公开(公告)日：2013-11-21

    申请号：US13953164

    申请日：2013-07-29

    Applicant: Hamilton Sundstrand Corporation

    Inventor： Louis J. Bruno ,  Anthony C. Jones ,  Todd A. Spierling ,  Gregory L. DeFrancesco

    IPC: B64D41/00

    CPC classification number: B64D41/00 ,  B64C13/40 ,  B64C13/42 ,  B64D2221/00

    Abstract: A hybrid power distribution system for an aircraft generates hydraulic power from one of a plurality of power sources based on which power source provides energy most efficiently. Power sources includes an electric power distribution bus that distributes electrical energy onboard the aircraft, a pneumatic distribution channel that distributes pneumatic energy onboard the aircraft, and mechanical power provided by one or more engines associated with the aircraft.

    Abstract translation: 用于飞机的混合动力配电系统基于哪个电源最有效地提供能量从多个电源之一产生液压动力。 电源包括分配飞机上的电能的电力分配总线，在飞机上分配气动能量的气动分配通道以及由与飞机相关联的一个或多个发动机提供的机械动力。

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