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    • 1. 发明申请
    • System And Method For Pumping Recirculation Air From An Aircraft Cabin
    • 从飞机舱抽出再循环空气的系统和方法
    • US20110171896A1
    • 2011-07-14
    • US13056255
    • 2009-07-23
    • Holger BrunnbergDariusz Krakowski
    • Holger BrunnbergDariusz Krakowski
    • B64D13/00
    • B64D13/00B64D2013/0655B64D2013/0688Y02T50/44Y02T50/56
    • A system (10) for conveying recirculation air from an aircraft cabin comprises a plurality of conveying devices (12a-12j) which are arranged in a manner distributed along an aircraft cabin region (14). A control device (16) is configured to control the conveying devices (12a-12j) in the normal operation of the system (10) in such a manner that each conveying device (12a-12j) removes a predetermined air volume flow from the aircraft cabin region (14). The control device (16) is furthermore configured to control, in the event of a failure of a conveying device (12c), at least some of the remaining still functional conveying devices (12a, 12b, 12d-12j) in such a manner that the entire air volume flow removed from the aircraft cabin region (14) by the remaining still functional conveying devices (12a, 12b, 12d-12j) is increased by an amount corresponding to an air volume flow amount removed from the aircraft cabin region (14) by the failed conveying device (12c) in the normal operation of the system (10).
    • 用于从飞机机舱输送再循环空气的系统(10)包括沿着飞机机舱区域(14)分布的方式布置的多个输送装置(12a-12j)。 控制装置(16)被构造成在系统(10)的正常操作中控制输送装置(12a-12j),使得每个输送装置(12a-12j)从飞机上移除预定的空气体积流量 舱区(14)。 控制装置(16)还被配置为在输送装置(12c)发生故障的情况下控制至少一些剩余的功能性输送装置(12a,12b,12d-12j),使得 通过剩余的功能性输送装置(12a,12b,12d-12j)从飞机机舱区域(14)移除的整个空气体积流量增加与从飞机机舱区域(14)去除的空气体积流量相对应的量 )通过系统(10)的正常操作中的故障输送装置(12c)。
    • 2. 发明授权
    • System and method for air-conditioning an aircraft cabin
    • 空调机舱的系统和方法
    • US09011219B2
    • 2015-04-21
    • US13056215
    • 2009-07-23
    • Holger BrunnbergDariusz Krakowski
    • Holger BrunnbergDariusz Krakowski
    • B64D13/00B64D13/02F25B9/00F25D17/06B64C1/00B64D13/06
    • B64D13/00B64C2001/0027B64D2013/0688Y02T50/56
    • A system for air-conditioning an aircraft cabin includes an air conditioning unit connected to a central mixer, a first recirculation system designed to remove exhaust air from a first aircraft cabin region and connected to the central mixer, and a second recirculation system designed to remove exhaust air from a second aircraft cabin region and connected to a local mixer. A control device is designed to control the second recirculation system to reduce an air volume flow being removed from the second aircraft cabin region when shifting from a first operating state (e.g., normal operation) to a second operating state (e.g., defined operating situations such as when quick cooling is desired). The air volume being removed from the first aircraft cabin region may be increased accordingly in the second operating state.
    • 一种用于空调飞机机舱的系统包括连接到中央混合器的空调单元,设计成从第一飞机机舱区域排出并连接到中央混合器的排气的第一再循环系统,以及设计成移除的第二再循环系统 从第二飞机机舱区域排出空气并连接到本地混合器。 控制装置设计成控制第二再循环系统,以便当从第一操作状态(例如,正常操作)转换到第二操作状态(例如,所定义的操作状态 当需要快速冷却时)。 在第二操作状态下,可以相应地增加从第一飞机机舱区域移除的空气量。
    • 3. 发明申请
    • System And Method For Air-Conditioning An Aircraft Cabin
    • 空调机组系统及方法
    • US20110212678A1
    • 2011-09-01
    • US13056215
    • 2009-07-23
    • Holger BrunnbergDariusz Krakowski
    • Holger BrunnbergDariusz Krakowski
    • B64D13/06
    • B64D13/00B64C2001/0027B64D2013/0688Y02T50/56
    • A system (10) for air-conditioning an aircraft cabin (12) comprises an air conditioning unit (14) connected to a central mixer (16) in order to supply the central mixer (16) with air at a desired low temperature. A first recirculation system (18) is designed to remove exhaust air from a first aircraft cabin region (12a) and is connected to the central mixer (16) in order to lead the exhaust air from the first aircraft cabin region (12a) into the central mixer (16). A second recirculation system (24) is designed to remove exhaust air from a second aircraft cabin region (12b) and is connected to a local mixer (20, 22) in order to lead the exhaust air from the second aircraft cabin (12b) into the local mixer (20, 22). The local mixer (20, 22) is connected to the central mixer (16) in order to supply mixed air from the central mixer (16) into the local mixer (20, 22). A control device (28) is designed to control the second recirculation system (24) in the normal operation of the air conditioning system (10) in such a way that the second recirculation system (24) removes a predefined air volume flow from the second aircraft cabin region (12b). The control device (28) is also designed to control the second recirculation system (24) in defined operating situations of the air conditioning system (10) in such a way that the air volume flow removed from the second aircraft cabin region (12b) by the second recirculation system (24) is reduced in relation to the predefined air volume flow removed from the second aircraft cabin region (12b) by the second recirculation system (24) in the normal operation of the air conditioning system (10).
    • 用于空调飞机机舱(12)的系统(10)包括连接到中央混合器(16)的空调单元(14),以便在期望的低温下向中央混合器(16)供应空气。 第一再循环系统(18)被设计成从第一飞机机舱区域(12a)去除排气并且连接到中央混合器(16),以将来自第一飞机机舱区域(12a)的排出空气引导到 中央混合器(16)。 第二再循环系统(24)被设计成从第二飞机机舱区域(12b)去除排出的空气,并且连接到局部混合器(20,22),以将排出的空气从第二飞机机舱(12b)引入 本地混合器(20,22)。 局部混合器(20,22)连接到中央混合器(16),以将来自中央混合器(16)的混合空气供应到本地混合器(20,22)中。 控制装置(28)被设计成在空调系统(10)的正常操作中控制第二再循环系统(24),使得第二再循环系统(24)从第二再循环系统 飞机舱区域(12b)。 控制装置(28)还被设计成在空调系统(10)的确定的操作情况下以这样的方式控制第二再循环系统(24),使得从第二飞机机舱区域(12b)移除的空气体积流由 在空调系统(10)的正常操作中,第二再循环系统(24)相对于由第二再循环系统(24)从第二飞机机舱区域(12b)移除的预定的空气体积流量减小。