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    Convertible aircraft toilet
    3.
    发明授权
    Convertible aircraft toilet 有权

    公开(公告)号：US11319696B2

    公开(公告)日：2022-05-03

    申请号：US16725324

    申请日：2019-12-23

    申请人： Airbus Operations SAS

    发明人： Bernard Guering ,  Romain Delahaye

    IPC分类号： E03C1/01 ,  B64D11/02

    摘要： To reduce the bulk of an aircraft toilet which includes a toilet bowl and a washbasin, the washbasin is movably mounted in the toilet to be able to adopt at least two distinct positions relative to the toilet bowl, including a retracted position adopted to bring the toilet into a configuration of use of the bowl, and a deployed position adopted to bring the toilet into a washbasin configuration, a position in which the washbasin is arranged above the bowl.

    Self-stiffened skin for aircraft fuselage including stringers with a closed section and associated manufacturing method
    4.
    发明授权
    Self-stiffened skin for aircraft fuselage including stringers with a closed section and associated manufacturing method 有权
    用于飞机机身的自加强皮肤，包括具有封闭截面的桁条和相关的制造方法

    公开(公告)号：US09446834B2

    公开(公告)日：2016-09-20

    申请号：US14140513

    申请日：2013-12-25

    申请人： Airbus Operations (SAS)

    发明人： Patrick Lieven ,  Romain Delahaye

    IPC分类号： B64C1/06 ,  B64C1/12 ,  B29D99/00 ,  B64C1/00

    CPC分类号： B64C1/068 ,  B29D99/0014 ,  B64C1/064 ,  B64C1/12 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10T156/1052 ,  Y10T428/13

    摘要： Simplification of the manufacture of composite material fuselages for aircraft, as well as mass reduction of fuselage sections and space optimization inside such fuselage sections. To accomplish this, it is proposed to use stringers of a new type which have a closed transverse section, and which are thus able to be self-positioned relative to one another by being positioned edge-to-edge on a stringer supporting structure, such as the outer surface of a mandrel. The installation of the stringers in grooves of conjugate shape is by this means made unnecessary. The stringers have cut-outs located between circumferential frames, and are able to house utility systems.

    摘要翻译： 简化飞机复合材料机身的制造，以及机身部分的大量减少和机身部分内的空间优化。 为了实现这一点，提出了使用具有闭合横截面的新型的桁条，并且因此能够通过在纵梁支撑结构上边缘到边缘定位而相对于彼此自定位，例如 作为心轴的外表面。 通过这种方式将桁条安装在共轭形状的槽中是不必要的。 桁条具有位于圆周框架之间的切口，并且能够容纳公用事业系统。

    STIFFENER FOR AN AIRCRAFT FUSELAGE, METHOD FOR MANUFACTURING SAME, AND AIRCRAFT FUSELAGE EQUIPPED WITH SUCH A STIFFENER
    5.
    发明申请
    STIFFENER FOR AN AIRCRAFT FUSELAGE, METHOD FOR MANUFACTURING SAME, AND AIRCRAFT FUSELAGE EQUIPPED WITH SUCH A STIFFENER 有权
    用于制造飞机的冲击器，其制造方法和装备有这种加速器的飞机配件

    公开(公告)号：US20150321742A1

    公开(公告)日：2015-11-12

    申请号：US14652118

    申请日：2013-12-20

    申请人： AIRBUS OPERATIONS (SAS)

    发明人： Christophe Mialhe ,  Romain Delahaye ,  Philipe Rodrigo

    IPC分类号： B64C1/06 ,  B21D53/92 ,  B21D5/16

    CPC分类号： B64C1/06 ,  B21D5/16 ,  B21D53/92 ,  B64C1/061 ,  B64C1/12

    摘要： This stiffener is intended for a fuselage. It comprises a hollow section that can be trapezoidal, with a base attached to the fuselage or to the floor, high enough rising sides and a top side contributing to the rigidity and cohesion of the stiffener. A direct assembly with the fuselage is possible. The base is made of two edges provided one on the other or in front of the other. This rigid stiffener, in spite of its discontinuous section, can be manufactured by simple foldings of a planar metal sheet at the beginning.

    摘要翻译： 这种加强筋适用于机身。 它包括可以是梯形的中空部分，其底部附接到机身或地板，足够高的上升侧和顶侧有助于加强件的刚性和内聚力。 与机身直接组装是可能的。 基座由另一个或另一个前面提供的两个边缘组成。 该刚性加强件尽管具有不连续的截面，但可以通过平面金属板在开始时的简单折叠来制造。

    RUDDER BAR FOR AN AIRCRAFT
    9.
    发明申请
    RUDDER BAR FOR AN AIRCRAFT 有权

    公开(公告)号：US20160159457A1

    公开(公告)日：2016-06-09

    申请号：US14961349

    申请日：2015-12-07

    申请人： Airbus Operations (SAS)

    发明人： Laurent Saint-Marc ,  Christophe Mialhe ,  Patrick Lieven ,  Romain Delahaye ,  Marc Audibert ,  Nicolas Chatrenet

    IPC分类号： B64C9/02

    CPC分类号： B64C13/04 ,  B64C13/06 ,  G05G1/30

    摘要： A rudder bar for an aircraft comprising a floor, a steering connecting rod and a braking connecting rod. The rudder bar comprises a base fixed above the floor, a pedal arm mounted rotatably on the base about a first axis of rotation and having a lower end and an upper end, a pedal mounted rotatably on the lower end about a second axis of rotation, a first transmission assembly configured to transmit a movement to the steering connecting rod when the pedal arm pivots about the first axis of rotation, and a second transmission assembly configured to transmit a movement to the braking connecting rod when the pedal pivots about the second axis of rotation.

    摘要翻译： 用于飞机的舵杆，包括地板，转向连杆和制动连杆。 方向舵杆包括固定在地板上方的底座，踏板臂，其围绕第一旋转轴线可旋转地安装在基座上，并具有下端和上端，踏板围绕第二旋转轴线可旋转地安装在下端上， 第一传动组件，其构造成当踏板臂围绕第一旋转轴线枢转时将运动传递到转向连杆;以及第二传动组件，其构造成当踏板围绕第二轴线枢转时将运动传递到制动连杆 回转。

    AIRPLANE WITH A FUSELAGE HAVING SIDE OUTGROWTH DELIMITING STORAGE SPACES
    10.
    发明申请
    AIRPLANE WITH A FUSELAGE HAVING SIDE OUTGROWTH DELIMITING STORAGE SPACES 有权
    具有一个具有一个成熟的分离存储空间的空中飞机

    公开(公告)号：US20140175218A1

    公开(公告)日：2014-06-26

    申请号：US14139153

    申请日：2013-12-23

    申请人： Airbus Operations (SAS)

    发明人： Guillaume Gallant ,  Romain Delahaye

    IPC分类号： B64D9/00 ,  B64C1/26 ,  B64C1/14 ,  B64D37/04

    CPC分类号： B64D9/00 ,  B64C1/00 ,  B64C1/1484 ,  B64C1/26 ,  B64C2001/0045 ,  B64D37/04

    摘要： An aircraft of which the transversal section of the fuselage is reduced optimally at the price of a reduced carrying capacity of luggage or merchandise but adapted to short- and medium-haul type routes. The fuselage has for this purpose lateral protuberances defining storage areas arranged on either side of a passenger cabin and able to house luggage and/or merchandise, and/or onboard service equipment, and/or removable fuel tanks.

    摘要翻译： 飞机的机身横截面以最小的行李箱或商品的承载能力降低，但适用于短途和中程航线的方式最优化。 机身为此目的设置横向突起，其定义了存放在客舱两侧的储存区域，并且能够容纳行李和/或商品，和/或船上服务设备和/或可拆卸的燃料箱。