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    FLUID SEPARATION MODULE FOR USE IN AIRCRAFTS
    1.
    发明申请
    FLUID SEPARATION MODULE FOR USE IN AIRCRAFTS 审中-公开
    用于飞机的流体分离模块

    公开(公告)号：WO2016038138A1

    公开(公告)日：2016-03-17

    申请号：PCT/EP2015/070705

    申请日：2015-09-10

    Applicant: EATON LIMITED

    Inventor： ASHTON, Dominic ,  RUSALI, Rudy Haryanto ,  MASSEY, Alan Ernest

    IPC: B01D53/22 ,  B01D53/26 ,  C01B21/04 ,  C01B13/02 ,  A62C3/06 ,  A62C3/08 ,  B64D37/32

    CPC classification number: B01D53/229 ,  B01D53/22 ,  B01D53/26 ,  B01D2053/224 ,  B01D2256/10 ,  B01D2257/104 ,  B01D2257/80 ,  B01D2259/4575 ,  B64D13/00 ,  B64D13/06 ,  B64D37/32 ,  B64D2013/0662 ,  C01B13/0251 ,  C01B21/0438 ,  C01B2210/001 ,  C01B2210/0045

    Abstract: A fluid system may include an inlet conduit that may be disposed in a fluid flow path between a fluid source and a fluid destination. The fluid conduit may include a fluid mixing portion. The fluid system may include a fluid separation module that may be disposed in the flow path downstream of the constriction between the source and the destination. The fluid separation module including a first fluid separator. The fluid system may include a second fluid separator that may be disposed in the flow path upstream of the first fluid separator. The fluid system may include a feedback conduit that may provide fluid communication between an outlet of the fluid separation module and the fluid mixing portion.

    Abstract translation: 流体系统可以包括可以设置在流体源和流体目的地之间的流体流动路径中的入口管道。 流体导管可包括流体混合部分。 流体系统可以包括流体分离模块，其可以设置在源路径和目的地之间的收缩部的下游的流动路径中。 流体分离模块包括第一流体分离器。 流体系统可以包括第二流体分离器，其可以设置在第一流体分离器的上游的流动路径中。 流体系统可以包括可以在流体分离模块的出口和流体混合部分之间提供流体连通的反馈导管。

    SYSTEM AND METHOD FOR AIR CONDITIONING AT LEAST ONE PARTIAL REGION OF AN AIRPLANE
    3.
    发明申请
    SYSTEM AND METHOD FOR AIR CONDITIONING AT LEAST ONE PARTIAL REGION OF AN AIRPLANE 审中-公开
    系统和方法用于冷却至少一块地的飞机区划

    公开(公告)号：WO2009053002A8

    公开(公告)日：2009-09-17

    申请号：PCT/EP2008008817

    申请日：2008-10-17

    Applicant: AIRBUS OPERATIONS GMBH ,  MARKWART MICHAEL ,  BENDFELDT PEGGY ,  GORES INGO ,  BUCHHOLZ UWE ,  KOEPP CHRISTINA

    Inventor： MARKWART MICHAEL ,  BENDFELDT PEGGY ,  GORES INGO ,  BUCHHOLZ UWE ,  KOEPP CHRISTINA

    IPC: B64D13/00 ,  B64D13/04

    CPC classification number: B64D13/06 ,  B64D13/00 ,  B64D2013/0625 ,  B64D2013/0662 ,  B64D2013/0688 ,  Y02T50/44 ,  Y02T50/56

    Abstract: The invention relates to a system for air conditioning at least one partial region of an airplane, comprising an air supply device (18) for providing a region of the airplane that is to be ventilated with a desired temperature and with a desired pressure of the air to be fed. An air supply duct (20) is connected to the air supply device at a first end. A second end of the air supply duct (20) is connected to an air inlet (24) ending in the region of the airplane to be ventilated, located close to the floor. A control device (26) is provided in order to ensure that the air provided by the air supply device enters the region of the airplane to be ventilated via the air inlet with such a speed that the air is distributed close to the floor in the region of the airplane to be ventilated and rises at heat sources present in the region of the airplane to be ventilated. The air provided from the air supply system enters the region of the airplane to be ventilated with such a temperature via the air inlet that the desired room temperature is achieved in the region of the airplane to be ventilated.

    Abstract translation: 一种用于至少空调的飞行器的局部区域系统包括用于提供飞机的区域以与所希望的温度和要被提供期望的压力的空气被通风的空气供给装置（18）。 供气管道（20）被连接在与所述空气供应装置的第一端。 将气源（20）的第二端连接到靠近地面的开口出来的待被通风飞行器空气入口（24）。 的控制装置（26）适于确保由空气供应装置经由空气入口以这样的速率在所述充气机区域中提供的信息时，空气被分布在地面附近的待通风平面区域并在其中 现有的热源通风飞机区域上升，由空气供给装置经由空气入口在设置于这样的温度下发生通风飞机区域，即被建立在其中的待被通风飞机区域，所希望的室温。

    REFRIGERATING DEVICE
    5.
    发明申请
    REFRIGERATING DEVICE 审中-公开
    制冷装置

    公开(公告)号：WO00066953A1

    公开(公告)日：2000-11-09

    申请号：PCT/JP2000/002307

    申请日：2000-04-07

    IPC: F25B9/00 ,  B01D53/08 ,  B01D53/26 ,  B64D13/06 ,  F24F3/14 ,  F24F5/00

    CPC classification number: F24F3/1423 ,  B01D53/06 ,  B01D53/26 ,  B01D53/261 ,  B01D2253/10 ,  B01D2253/308 ,  B01D2257/80 ,  B01D2259/4009 ,  B01D2259/65 ,  B64D13/06 ,  B64D2013/0662 ,  F24F5/0085 ,  F24F2203/1016 ,  F24F2203/1036 ,  F24F2203/1068 ,  F24F2203/1084 ,  Y02T50/56

    Abstract: A refrigerating device, wherein a cycle circuit (20) comprises an expansion device (22), a heat exchanger (30), and a compressor (21) connected in order to each other, a dehumidifying mechanism (60) is provided so as to dehumidify heat-absorbed air taken in through an inlet duct (23), an internal heat exchanger (15) is provided so as to supply the dehumidified heat-absorbed air, after cooling, to the expansion device (22), the heat-absorbed air is expanded in the expansion device (22) causing a temperature to lower, moisture is not condensed at the time of expansion because the heat-absorbed air is dehumidified beforehand, the heat-absorbed air reduced in temperature by expansion flows into the heat exchanger (30) and absorbs heat from indoor air, and then the heat-absorbed air is compressed by the compressor (21) and exhausted to the outside after regenerating a rotor member (61).

    Abstract translation: 一种制冷装置，其中循环回路（20）包括膨胀装置（22），热交换器（30）和彼此连接的压缩机（21），除湿机构（60）设置成 对通过入口管道（23）吸入的吸热空气进行除湿，设置有内部热交换器（15），以将冷却后的除湿吸热空气供给到膨胀装置（22），吸热空气 空气在膨胀装置（22）中膨胀，导致温度降低，由于吸热空气预先被除湿，所以膨胀时的水分不会凝结，所以被膨胀的温度降低的吸热空气流入热交换器 （30）吸收室内空气中的热量，然后通过压缩机（21）将受热空气压缩并再生转子部件（61）后排出到外部。

    SYSTEMS AND METHODS FOR PROVIDING AIRFLOW IN AN AEROSPACE VEHICLE
    8.
    发明申请
    SYSTEMS AND METHODS FOR PROVIDING AIRFLOW IN AN AEROSPACE VEHICLE 审中-公开
    用于在航空器车辆中提供气流的系统和方法

    公开(公告)号：WO2008144295A3

    公开(公告)日：2013-04-11

    申请号：PCT/US2008063499

    申请日：2008-05-13

    Applicant: BOEING CO ,  SPACE DAVID R ,  MATERA JANE V ,  ATKEY WARREN A ,  FITERMAN CHARLES J ,  GRAY JOHN C ,  ARNAUD TIMOTHY J

    Inventor： SPACE DAVID R ,  MATERA JANE V ,  ATKEY WARREN A ,  FITERMAN CHARLES J ,  GRAY JOHN C ,  ARNAUD TIMOTHY J

    IPC: B64D13/06

    CPC classification number: B64D13/06 ,  B64D2013/0618 ,  B64D2013/0651 ,  B64D2013/0655 ,  B64D2013/0662 ,  B64D2013/0681 ,  B64D2013/0688 ,  Y02T50/56

    Abstract: Systems and methods for providing airflow in an aerospace vehicle are disclosed. A system in accordance with one embodiment includes an aerospace vehicle having an interior volume with a first portion and a second portion. The system can further include an external air supply device positioned to provide supply air to the interior volume at a variable supply flow rate and a recirculation fan configured to move air positioned within the interior volume between the first portion of the interior volume and the second portion of the interior volume. The system can still further include a controller operably coupled to the recirculation fan and configured to vary a rotation speed of the recirculation fan. Variations in the rotation speed of the recirculation fan can be associated with variations in a recirculation flow rate. In selected embodiments, the system can include sensors and/or data link devices operably coupled to the controller.

    Abstract translation: 公开了在航空航天车辆中提供气流的系统和方法。 根据一个实施例的系统包括具有带有第一部分和第二部分的内部容积的航空航天车辆。 该系统还可以包括外部空气供应装置，其定位成以可变的供应流量向内部空间供应空气;以及再循环风扇，所述再循环风扇被配置成移动位于内部空间的第一部分之间的位于内部空间内的空气， 的内部体积。 该系统还可以包括可操作地耦合到再循环风扇并被配置为改变再循环风扇的转速的控制器。 再循环风扇的转速变化可能与再循环流量的变化有关。 在所选择的实施例中，系统可以包括可操作地耦合到控制器的传感器和/或数据链路装置。

    AIR CONDITIONING SYSTEM FOR AIRCRAFT CABINS
    9.
    发明申请
    AIR CONDITIONING SYSTEM FOR AIRCRAFT CABINS 审中-公开
    航空客舱空调系统

    公开(公告)号：WO2009007094A4

    公开(公告)日：2009-09-11

    申请号：PCT/EP2008005564

    申请日：2008-07-08

    Applicant: AIRBUS OPERATIONS GMBH ,  CREMERS JOERG ,  DERLIEN HENRIK ,  KRICKE KLAUS-DIETER ,  WILKE KATJA-MARIA

    Inventor： CREMERS JOERG ,  DERLIEN HENRIK ,  KRICKE KLAUS-DIETER ,  WILKE KATJA-MARIA

    IPC: B64D13/06 ,  B64D41/00

    CPC classification number: B64D13/06 ,  B64D2013/0611 ,  B64D2013/0618 ,  B64D2013/0648 ,  B64D2013/0662 ,  B64D2013/0688 ,  Y02T50/44 ,  Y02T50/56

    Abstract: The present invention relates to an air conditioning system (10) for an aircraft cabin (12) with at least one air inlet (14) for supplying air to the cabin (12), at least one air outlet (16) for discharging air from the cabin (12) and at least one compressed-air source (52, 54, 56), which is adapted to provide pressurised fresh air for supplying to the cabin (12) via the at least one air inlet (14). The air conditioning system (10) further comprises a heat exchanger (42) supplied with ram air from a ram air inlet (92) for cooling air from the compressed-air source (52, 54, 56), wherein the heat exchanger (42) is disposed upstream of the air inlet (14) of the cabin (12). It is intended that the air conditioning system (10) comprises a cabin air heat exchanger (100) which is designed to be supplied with air discharged from the cabin (12), wherein the cabin air heat exchanger (100) is disposed downstream of the at least one air outlet (16) and upstream of a point (N) at which fresh air is mixed with air from the cabin (12).

    Abstract translation: 本发明涉及一种用于飞机机舱（12）的空调系统（10），所述空调系统具有至少一个用于向所述机舱（12）供应空气的空气入口（14），至少一个空气出口（16），用于从 所述舱室（12）和至少一个压缩空气源（52,54,56），其适于提供加压的新鲜空气，用于经由所述至少一个空气入口（14）供应到所述舱室（12）。 空调系统（10）还包括一个从冲压空气入口（92）供应冲压空气的热交换器（42），用于冷却来自压缩空气源（52,54,56）的空气，其中热交换器 ）设置在机舱（12）的进气口（14）的上游。 目的是空调系统（10）包括舱室空气热交换器（100），其被设计成供应从舱（12）排出的空气，其中客舱空气热交换器（100）设置在客舱空气热交换器 至少一个空气出口（16）和点（N）的上游，新鲜空气与来自舱室（12）的空气混合。

    SYSTEMS AND METHODS FOR PROVIDING AIRFLOW IN AN AEROSPACE VEHICLE
    10.
    发明申请
    SYSTEMS AND METHODS FOR PROVIDING AIRFLOW IN AN AEROSPACE VEHICLE 审中-公开
    用于在航空器车辆中提供气流的系统和方法

    公开(公告)号：WO2008144295A2

    公开(公告)日：2008-11-27

    申请号：PCT/US2008/063499

    申请日：2008-05-13

    Applicant: THE BOEING COMPANY ,  SPACE, David R. ,  MATERA, Jane V. ,  ATKEY, Warren A. ,  FITERMAN, Charles J. ,  GRAY, John C. ,  ARNAUD, Timothy J.

    Inventor： SPACE, David R. ,  MATERA, Jane V. ,  ATKEY, Warren A. ,  FITERMAN, Charles J. ,  GRAY, John C. ,  ARNAUD, Timothy J.

    CPC classification number: B64D13/06 ,  B64D2013/0618 ,  B64D2013/0651 ,  B64D2013/0655 ,  B64D2013/0662 ,  B64D2013/0681 ,  B64D2013/0688 ,  Y02T50/56

    Abstract: Systems and methods for providing airflow in an aerospace vehicle are disclosed. A system in accordance with one embodiment includes an aerospace vehicle having an interior volume with a first portion and a second portion. The system can further include an external air supply device positioned to provide supply air to the interior volume at a variable supply flow rate and a recirculation fan configured to move air positioned within the interior volume between the first portion of the interior volume and the second portion of the interior volume. The system can still further include a controller operably coupled to the recirculation fan and configured to vary a rotation speed of the recirculation fan. Variations in the rotation speed of the recirculation fan can be associated with variations in a recirculation flow rate. In selected embodiments, the system can include sensors and/or data link devices operably coupled to the controller.

    Abstract translation: 公开了在航空航天车辆中提供气流的系统和方法。 根据一个实施例的系统包括具有内部容积的航空航天车辆，其具有第一部分和第二部分。 该系统还可以包括外部空气供应装置，该外部空气供应装置定位成以可变的供应流量向内部空间供应空气;以及再循环风扇，其被配置成将位于内部容积内的空气移动到内部空间的第一部分与第二部分之间 的内部体积。 该系统还可以包括可操作地耦合到再循环风扇并被配置为改变再循环风扇的转速的控制器。 再循环风扇的转速变化可能与再循环流量的变化有关。 在所选择的实施例中，系统可以包括可操作地耦合到控制器的传感器和/或数据链路设备。

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