INSULATION ARRANGEMENT WITH VENTILATION OPENINGS FOR AIRCRAFT
    2.
    发明申请
    INSULATION ARRANGEMENT WITH VENTILATION OPENINGS FOR AIRCRAFT 审中-公开
    用于航空器通风口的绝缘装置

    公开(公告)号:WO2012069289A1

    公开(公告)日:2012-05-31

    申请号:PCT/EP2011/069167

    申请日:2011-10-31

    CPC classification number: B64C1/40 B64C1/067 B64D2013/0625

    Abstract: The invention pertains to an insulation arrangement with two or more insulation packages (18) that overlap such that at least one overlapping region is formed and are arrangeable on a fuselage wall (8), wherein said insulation packages consist of an insulating material and welded cover films (20, 22). The cover films (20, 22) are realized in an airtight and waterproof fashion and comprise ventilation openings on a side that is directed toward the fuselage wall (8) in an overlapping region (24). In this way, pressure variations in the insulation packages (18) can be compensated with relatively dry air that originates from a gap (16) between the insulation packages (18) and the fuselage wall (8) in order to thusly reduce the accumulation of condensation water in the insulation packages (18).

    Abstract translation: 本发明涉及具有两个或更多个绝缘封套(18)的绝缘装置,该绝缘套管重叠使得形成至少一个重叠区域并且可布置在机身壁(8)上,其中所述绝缘封装由绝缘材料和焊接盖 电影(20,22)。 覆盖膜(20,22)以气密和防水的方式实现,并且包括在重叠区域(24)中朝向机身壁(8)的一侧上的通风开口。 以这种方式,绝缘包装(18)中的压力变化可以由来自绝缘包装(18)和机身壁(8)之间的间隙(16)的相对干燥的空气补偿,以便因此减少 绝缘包装(18)中的冷凝水。

    ACOUSTICALLY OPTIMIZED AIR CONDITIONING COMPONENTS
    5.
    发明申请
    ACOUSTICALLY OPTIMIZED AIR CONDITIONING COMPONENTS 审中-公开
    声学优化的空调组件

    公开(公告)号:WO2011082983A3

    公开(公告)日:2011-10-20

    申请号:PCT/EP2010069570

    申请日:2010-12-14

    Inventor: THOMAS CHRISTIAN

    CPC classification number: B64D13/00 B64D2013/0625 F16L9/21 Y02T50/44 Y02T50/56

    Abstract: The present invention relates to sound damping of air conditioning systems in an aircraft. The invention in particular relates to an air conditioning air duct for an aircraft, and to an aircraft having air conditioning air ducts. In order to provide an air conditioner air duct optimized for installed space and weight for use in an aircraft, by means of which the best possible sound damping properties are achieved at the same time, an air conditioner air duct (50) having a sound damping effect is provided, comprising a sound damping wall (52) at least partially enclosing a continuous hollow space (54) for carrying the air, wherein the continuous hollow space has an air inlet opening (56) and an air outlet opening (58), wherein the hollow space for carrying air is immediately adjacent to the wall. The wall (52) comprises a multilayer construction having a core layer (60) and at least one first cover layer (62). The core layer (60) is made of a sound absorbing, open pore core material, so that the wall comprises an acoustic effect. The first cover layer (62) is designed to be airtight, and is disposed on the outer face of the core layer (60), and is areally bonded to the core layer (60). The areal bond between the core layer (60) and the first cover layer (62) brings about a composite effect, such that the wall (52) is self-supporting and comprises a structural function, in order to be able to transmit mechanical loads to load bearing parts of the aircraft, so that the wall also has a load bearing effect.

    Abstract translation: 本发明涉及飞机中空调系统的静音。 具体地,本发明涉及用于飞机的空调风道以及具有空调风道的飞行器。 A相对于放在安装空间和重量优化的空调风道用在飞机得,实现最佳的声音吸收性质,空调空气管道(50)上设置有吸音效果,其具有吸音壁(52)的同时, 通过空腔中的一个(54)至少部分地围绕用于引导空气,所述提供了一种具有空气入口开口(56)和空气出口开口(58)连续空腔,其特征在于,用于引导空气紧邻壁的空腔中。 壁(52)具有多层结构,其具有芯层(60)和至少一个第一覆盖层(62)。 核心层(60)由吸音开孔核心材料组成,因此墙具有声学效果。 第一覆盖层(62)气密地布置在芯层(60)的外侧并且与芯层(60)平坦地连接。 芯层(60)和所述第一覆盖层之间的扁平连接(62)导致的复合作用,使得所述壁(52)是自支撑的并且具有这样的结构的功能载荷机械上发生转移飞行器的承载部分,从而使 沃尔也有一个携带行动。

    AIRCRAFT CABIN AIRFLOW NOZZLES AND ASSOCIATED SYSTEMS AND METHODS
    6.
    发明申请
    AIRCRAFT CABIN AIRFLOW NOZZLES AND ASSOCIATED SYSTEMS AND METHODS 审中-公开
    飞机舱气流喷头及相关系统及方法

    公开(公告)号:WO2009032497A1

    公开(公告)日:2009-03-12

    申请号:PCT/US2008/073043

    申请日:2008-08-13

    CPC classification number: B64D13/00 B64D2013/0625

    Abstract: Aircraft cabin airflow nozzles and associated systems and methods are disclosed. A system in accordance with a particular embodiment includes a cabin air nozzle (220) that in turn has a first passageway (223a) bounded at least in part by a first wall portion (222a) and a second wall portion (222b) spaced apart from the first wall portion. The second wall portion (222b) can have a first surface exposed to air within the first passageway (223a), and a second surface facing away from the first surface. The first passageway (223a) can have an exit (232) between the first and second wall portions, and the second passageway (223b) can be positioned to direct air along the second surface of the wall portion.

    Abstract translation: 公开了飞机机舱气流喷嘴及相关系统和方法。 根据特定实施例的系统包括机舱空气喷嘴(220),其还具有至少部分地由第一壁部分(222a)限定的第一通道(223a)和与第一壁部分(222a)间隔开的第二壁部分 第一壁部分。 第二壁部分(222b)可以具有暴露于第一通道(223a)内的空气的第一表面和背离第一表面的第二表面。 第一通道(223a)可以在第一和第二壁部分之间具有出口(232),并且第二通道(223b)可以被定位成沿着壁部分的第二表面引导空气。

    NOISE OPTIMIZED AIR DISTRIBUTOR
    7.
    发明申请
    NOISE OPTIMIZED AIR DISTRIBUTOR 审中-公开
    噪声优化空气分配器

    公开(公告)号:WO2007121855A1

    公开(公告)日:2007-11-01

    申请号:PCT/EP2007/003191

    申请日:2007-04-10

    Abstract: An air distributor according to the invention has a perforated body, insertable at a joint between a first air duct, which extends in one direction, and a second air duct, that extends in a second different direction, to redirect air flowing in the first air duct into the second air duct and to reduce low frequency high volume noise.

    Abstract translation: 根据本发明的空气分配器具有穿孔体,其可插入在沿一个方向延伸的第一空气管道和沿第二不同方向延伸的第二空气管道之间的接头处,以重新定向在第一空气中流动的空气 管道进入第二个风道,并减少低频大容量噪音。

    PIVOT BIN ASSEMBLY WITH MINIMAL FORCE REQUIRED FOR CLOSING
    8.
    发明申请
    PIVOT BIN ASSEMBLY WITH MINIMAL FORCE REQUIRED FOR CLOSING 审中-公开
    PIVOT BIN大会需要最小的力量才能关闭

    公开(公告)号:WO2016122737A1

    公开(公告)日:2016-08-04

    申请号:PCT/US2015/057655

    申请日:2015-10-27

    Inventor: SAVIAN, Scott

    CPC classification number: B64D11/003 B64D2011/0053 B64D2013/0625 Y02T50/46

    Abstract: An aircraft storage bin that includes an upper housing, and a bucket pivotally connected to the upper housing that cooperates with the upper housing to define a bin interior. The bucket includes a bottom, a front edge, first and second opposing side walls extending upwardly from the bottom and a center of gravity. The bucket pivots about a pivot axis with respect to the upper housing between an open position and a closed position. The center of gravity of the bucket is positioned below the pivot axis when the bucket is in the closed position.

    Abstract translation: 一种包括上部壳体的飞行器存储箱,以及与上壳体枢转连接的铲斗,该铲斗与上壳体配合以限定箱体内部。 铲斗包括底部,前缘,从底部向上延伸的第一和第二相对的侧壁和重心。 斗在相对于上壳体的枢转轴线在打开位置和关闭位置之间枢转。 当铲斗处于关闭位置时,铲斗的重心位于枢转轴线的下方。

    AIRCRAFT CIRCULATION SYSTEM FOR PASSENGER CABINS
    9.
    发明申请
    AIRCRAFT CIRCULATION SYSTEM FOR PASSENGER CABINS 审中-公开
    飞机客舱飞机循环系统

    公开(公告)号:WO2014137515A1

    公开(公告)日:2014-09-12

    申请号:PCT/US2014/014386

    申请日:2014-02-03

    Abstract: A method and apparatus for an air circulation system. The apparatus comprises a suite and a circulation unit. The suite has walls extending upward from a floor of the passenger cabin without reaching a ceiling of the passenger cabin. The circulation unit comprises an inlet system configured to receive air in the passenger cabin in a location outside of the suite; an outlet system configured to output the air received by the inlet system into an interior of the suite; and a fan system configured to cause a movement of the air into the inlet system from outside of the suite and out of the outlet system into the interior of the suite. The air moves upwards in the suite and over the walls. The air moving over the walls causes a desired circulation of the air within the passenger cabin.

    Abstract translation: 一种用于空气循环系统的方法和装置。 该装置包括套件和循环单元。 该套房具有从客舱的地板向上延伸的墙壁,而不到达客舱的天花板。 循环单元包括入口系统,该入口系统构造成在套房外的位置处接收乘客舱内的空气; 出口系统,被配置为将由入口系统接收的空气输出到套件的内部; 以及风扇系统,其构造成使得空气从套件的外部进入入口系统并且从出口系统进入套件的内部。 空气在套间和墙壁上向上移动。 在墙壁上移动的空气导致客舱内空气的期望循环。

    ZULUFTVERSORGUNG FÜR PASSAGIERE IN FLUGZEUGEN
    10.
    发明申请
    ZULUFTVERSORGUNG FÜR PASSAGIERE IN FLUGZEUGEN 审中-公开
    气源用于飞机PASSENGERS

    公开(公告)号:WO2011101211A1

    公开(公告)日:2011-08-25

    申请号:PCT/EP2011/051057

    申请日:2011-01-26

    CPC classification number: B64D13/00 B64D2013/0625

    Abstract: Zuluftsystem für Passagiere in einem Passagierraum, wobei der Zuluftkanal bei einer Änderung der Sitzkonfiguration nicht umgebaut werden muss. Dies wird durch ein in Flugzeuglängsrichtung durchgängiges Luft-Verteilungselement (100) gewährleistet, das an definierten Positionen, welche auf mögliche Sitz-Layouts abgestimmt sind, Öffnungen (110) aufweist. Nicht benötigte Öffnungen werden verschlossen, beispielsweise durch ein Auswahlelement (200), das das Luft-Verteilungselement umschließt, und an einer Seite geschlitzt ist.

    Abstract translation: 用于在乘客空间的乘客空气供给系统中,供给空气不得改变座椅配置时修改。 这是通过一个连续的平面中具有其适于安置布局可能的开口(110)限定的位置的空气分配元件(100)的纵向方向上确保。 未使用的开口是闭合的,例如通过一个选择元件(200),其包围所述空气分配部件,并且开槽在一侧。

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