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    Bus system for an aircraft
    1.
    发明授权
    Bus system for an aircraft 有权
    一架飞机的总线系统

    公开(公告)号：US07433354B2

    公开(公告)日：2008-10-07

    申请号：US11014284

    申请日：2004-12-16

    申请人： Thomas Scherer ,  Volker Von Doehlen

    发明人： Thomas Scherer ,  Volker Von Doehlen

    IPC分类号： H04L12/28 ,  H04L12/56

    CPC分类号： H04L12/413 ,  H04L2012/40215 ,  H04L2012/40273

    摘要： The present invention relates to a bus system for transmitting a data packet between multiple devices in an aircraft, which is based on the CAN data bus system, but has an expanded identification field, in which a fixed region is designed for identification of the manifold aircraft systems, through which each aircraft system may be addressed uniquely. According to an exemplary embodiment, the data packet may be sent with different priorities, through which “important” data packets have priority on the transmission medium.

    摘要翻译： 本发明涉及一种用于在飞机中的多个设备之间传输数据分组的总线系统，其基于CAN数据总线系统，但具有扩展的识别字段，其中固定区域被设计用于识别多媒体飞行器 系统，每个飞机系统可以通过该系统被唯一地寻址。 根据示例性实施例，可以以不同的优先级发送数据分组，通过该优先级，“重要”数据分组在传输介质上具有优先权。

    Bus system for an aircraft
    2.
    发明申请
    Bus system for an aircraft 有权
    一架飞机的总线系统

    公开(公告)号：US20050190760A1

    公开(公告)日：2005-09-01

    申请号：US11014284

    申请日：2004-12-16

    申请人： Thomas Scherer ,  Volker Von Doehlen

    发明人： Thomas Scherer ,  Volker Von Doehlen

    IPC分类号： H04L12/413 ,  H04L12/28

    CPC分类号： H04L12/413 ,  H04L2012/40215 ,  H04L2012/40273

    摘要： The present invention relates to a bus system for transmitting a data packet between multiple devices in an aircraft, which is based on the CAN data bus system, but has an expanded identification field, in which a fixed region is designed for identification of the manifold aircraft systems, through which each aircraft system may be addressed uniquely. According to an exemplary embodiment, the data packet may be sent with different priorities, through which “important” data packets have priority on the transmission medium.

    摘要翻译： 本发明涉及一种用于在飞机中的多个设备之间传输数据分组的总线系统，其基于CAN数据总线系统，但具有扩展的识别字段，其中固定区域被设计用于识别多媒体飞行器 系统，每个飞机系统可以通过该系统被唯一地寻址。 根据示例性实施例，可以以不同的优先级发送数据分组，通过该优先级，“重要”数据分组在传输介质上具有优先权。

    Cooling system for the cooling of heat-producing devices in an aircraft
    5.
    发明授权
    Cooling system for the cooling of heat-producing devices in an aircraft 有权
    用于冷却飞机中的制热装置的冷却系统

    公开(公告)号：US08061154B2

    公开(公告)日：2011-11-22

    申请号：US10584779

    申请日：2004-12-30

    申请人： Thomas Scherer ,  Matthias Witschke ,  Carsten Colberg

    发明人： Thomas Scherer ,  Matthias Witschke ,  Carsten Colberg

    IPC分类号： B60H1/32

    CPC分类号： F25D17/02 ,  B64D11/04 ,  B64D13/06 ,  B64D2013/0629 ,  Y02T50/56

    摘要： A cooling system for the cooling of heat producing devices in an aircraft is designed with a central cold producing device, at least one cold consumer and a cold conveyance system which connects the cold producing device and the cold consumer. With this cooling system, the cold conveyance system has at least one cooling circuit which supplies a cooled cold carrier medium from the cold producing device to at least one cold consumer and brings the cold carrier medium back to the cold producing device, so that at least one cold consumer is supplied with the cold produced in the cold producing device.

    摘要翻译： 用于冷却飞机中的发热装置的冷却系统设计有中央冷产生装置，至少一个冷消费者和连接冷产生装置和冷消费者的冷输送系统。 通过该冷却系统，冷传送系统具有至少一个冷却回路，该冷却回路将冷却的冷载体介质从冷产生装置提供给至少一个冷消耗装置，并使冷载体介质回到冷产生装置，使得至少 一个冷的消费者被供应在冷产生装置中产生的冷。

    Arrangement and method for utilizing the heat of waste air for heating the bilge area of aircraft
    6.
    发明授权
    Arrangement and method for utilizing the heat of waste air for heating the bilge area of aircraft 有权
    利用废气热量加热飞机舱底的布置和方法

    公开(公告)号：US07980928B2

    公开(公告)日：2011-07-19

    申请号：US11311535

    申请日：2005-12-19

    申请人： Michael Markwart ,  Thomas Scherer ,  Oliver Schaumann

    发明人： Michael Markwart ,  Thomas Scherer ,  Oliver Schaumann

    IPC分类号： B64D13/00 ,  B64D11/00 ,  B60H1/00

    CPC分类号： B64D13/06 ,  B64D2013/0648 ,  Y02T50/56

    摘要： The present application describes an arrangement and a method for utilizing the heat of waste air for heating the bilge area of aircraft, wherein the bilge area is connected to a heat transfer unit via a first air supply pipe, through which a bilge air flow drawn in from the bilge area flows into the heat transfer unit, wherein the heat transfer unit comprises a second air supply pipe, through which a waste air heat flow to be cooled that is created at another location in the aircraft flows into the heat transfer unit in order to heat the drawn-in bilge air flow, wherein the heat transfer unit comprises a first air discharge pipe, through which the cooled waste air heat flow is discharged, and a second air discharge pipe with a bilge inlet section, and wherein at least a portion of the heated bilge flow is returned to the bilge area via the air discharge pipe and the bilge inlet section.

    摘要翻译： 本申请描述了一种用于利用废气的热量来加热飞机舱底区域的布置和方法，其中舱底区域经由第一空气供应管连接到传热单元，通过该第一空气供应管， 从舱底区域流入传热单元，其中传热单元包括第二空气供应管，通过该第二空气供应管，在飞机中的另一位置处产生的待冷却的废气热流按顺序流入传热单元 加热吸入舱底空气流，其中传热单元包括排出冷却的废气热流的第一排气管和具有舱底入口段的第二排气管，并且其中至少一个 加热的舱底流的一部分经由排气管和舱底入口部返回到舱底区域。

    System for producing process air
    7.
    发明授权
    System for producing process air 有权
    生产工艺空气的系统

    公开(公告)号：US07922118B2

    公开(公告)日：2011-04-12

    申请号：US11573531

    申请日：2005-08-10

    申请人： Juergen Kelnhofer ,  Thomas Scherer

    发明人： Juergen Kelnhofer ,  Thomas Scherer

    IPC分类号： B64D11/00

    CPC分类号： B64D13/02 ,  B64D13/06 ,  B64D2013/0677 ,  F28D2021/0021 ,  Y02T50/44

    摘要： A system for the provision of process air comprises a first cooling system (2) with a first heat exchanger, which is arranged in a channel (3) that serves as a cooling sink, and a cooling system (8), integrated in the first cooling system (2), wherein said cooling system (8) comprises a heat exchanger (9) which is integrated in the channel (3) either upstream or downstream of the first heat exchanger.

    摘要翻译： 一种用于提供处理空气的系统包括具有第一热交换器的第一冷却系统（2），其布置在用作冷却槽的通道（3）中，以及冷却系统（8），其集成在第一 冷却系统（2），其中所述冷却系统（8）包括在第一热交换器的上游或下游集成在通道（3）中的热交换器（9）。

    Method For Controlling The Temperature Of Feed Air Injected Into The Cabin Zone Of A Passenger Aircraft
    8.
    发明申请
    Method For Controlling The Temperature Of Feed Air Injected Into The Cabin Zone Of A Passenger Aircraft 有权
    用于控制进入客机客舱区域的进料空气温度的方法

    公开(公告)号：US20100267323A1

    公开(公告)日：2010-10-21

    申请号：US12824898

    申请日：2010-06-28

    申请人： Thomas Scherer ,  Michael Markwart ,  Torsten Schwan

    发明人： Thomas Scherer ,  Michael Markwart ,  Torsten Schwan

    IPC分类号： B64D13/08 ,  B64D13/00

    CPC分类号： B64D13/00 ,  B64D13/08 ,  B64D2013/0655 ,  Y10S62/05

    摘要： With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controlled feed air, the temperature of the injected feed air is controlled for each cabin zone, dependent upon the deviation of an injection temperature actual value for the feed air injected into the cabin zone in question, measured by sensors, in relation to an injection temperature optimum value. If there is no, or at least no usable reading of the ambient temperature of this cabin zone for a cabin zone, an optimum value for the injection temperature of this cabin zone can be established in accordance with a variation, whereby it is determined upon the basis of the injection temperature optimum values and/or the injection temperature actual values of other cabin zones, whereby the measurement by sensors of the cabin temperature works reliably. In accordance with another variation, the injection temperature optimum value of a cabin zone can be established without measuring ambient temperature by sensors or without reliably measuring ambient temperature from the temperature measured for the external surrounds of the aircraft.

    摘要翻译： 使用一种用于控制喷射到客机的客舱区域中的进料空气的温度的方法，其将舱室分成几个舱区，分别提供特别温度控制的进料空气，喷射进料的温度 根据喷射温度最佳值，根据传感器测量的注入到所述舱室区域的进料空气的喷射温度实际值的偏差，对每个舱室进行空气控制。 如果对于客舱区域没有或至少没有可用的该舱室区域的环境温度读数，则可以根据变化确定该舱区域的喷射温度的最佳值，由此根据 喷射温度最佳值和/或其他舱区的喷射温度实际值的基础，由此由客舱温度的传感器进行的测量可靠地工作。 根据另一个变化，可以建立客舱区域的喷射温度最佳值，而不需要通过传感器测量环境温度，或者不会从对飞行器的外部环境测量的温度可靠地测量环境温度。

    Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft
    9.
    发明授权
    Method for controlling the temperature of feed air injected into the cabin zone of a passenger aircraft 有权
    用于控制喷射到客机的客舱区域中的进料空气的温度的方法

    公开(公告)号：US07775447B2

    公开(公告)日：2010-08-17

    申请号：US10582595

    申请日：2004-12-30

    申请人： Thomas Scherer ,  Michael Markwart ,  Torsten Schwan

    发明人： Thomas Scherer ,  Michael Markwart ,  Torsten Schwan

    IPC分类号： F24F11/00 ,  B60H1/00 ,  F24F3/00

    CPC分类号： B64D13/00 ,  B64D13/08 ,  B64D2013/0655 ,  Y10S62/05

    摘要： With a method for controlling the temperature of feed air which is injected into the cabin zone of a passenger aircraft, the cabin of which is sub-divided into several cabin zones supplied respectively with specially temperature-controlled feed air, the temperature of the injected feed air is controlled for each cabin zone, dependent upon the deviation of an injection temperature actual value for the feed air injected into the cabin zone in question, measured by sensors, in relation to an injection temperature optimum value. If there is no, or at least no usable reading of the ambient temperature of this cabin zone for a cabin zone, an optimum value for the injection temperature of this cabin zone can be established in accordance with a variation, whereby it is determined upon the basis of the injection temperature optimum values and/or the injection temperature actual values of other cabin zones, whereby the measurement by sensors of the cabin temperature works reliably. In accordance with another variation, the injection temperature optimum value of a cabin zone can be established without measuring ambient temperature by sensors or without reliably measuring ambient temperature from the temperature measured for the external surrounds of the aircraft.

    摘要翻译： 使用一种用于控制喷射到客机的客舱区域中的进料空气的温度的方法，其将舱室分成几个舱区，分别提供特别温度控制的进料空气，喷射进料的温度 根据喷射温度最佳值，根据传感器测量的注入到所述舱室区域的进料空气的喷射温度实际值的偏差，对每个舱室进行空气控制。 如果对于客舱区域没有或至少没有可用的该舱室区域的环境温度读数，则可以根据变化确定该舱区域的喷射温度的最佳值，由此根据 喷射温度最佳值和/或其他舱区的喷射温度实际值的基础，由此由客舱温度的传感器进行的测量可靠地工作。 根据另一个变化，可以建立客舱区域的喷射温度最佳值，而不需要通过传感器测量环境温度，或者不会从对飞行器的外部环境测量的温度可靠地测量环境温度。