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    STEUERFLÄCHENELEMENT
    6.
    发明公开
    STEUERFLÄCHENELEMENT 审中-公开

    公开(公告)号：EP3286078A1

    公开(公告)日：2018-02-28

    申请号：EP16720996

    申请日：2016-04-22

    申请人： FACC AG

    发明人： FILSEGGER HERMANN ,  STEPHAN WALTER

    IPC分类号： B64C9/00 ,  B64C9/32

    CPC分类号： B64C9/00 ,  B29C70/443 ,  B64C9/32 ,  Y02T50/433

    摘要： A control surface element (1) for an aircraft, more particularly a spoiler, comprising an upper outer skin element (2) that has an outer air flow face (4); comprising a lower outer skin element (3); comprising at least one reinforcement rib (8); and comprising a core element (9) made of a foam material; wherein the reinforcement rib (8) is positioned between two core segments (10) of the core element (9).

    ÜBERKOPF-GEPÄCKFACH FÜR FLUGZEUGE UND FLUGZEUG
    7.
    发明公开
    ÜBERKOPF-GEPÄCKFACH FÜR FLUGZEUGE UND FLUGZEUG 有权
    ÜBERKOPF-GEPÄCKFACHFÜRFLUGZEUGE UND FLUGZEUG

    公开(公告)号：EP3148879A1

    公开(公告)日：2017-04-05

    申请号：EP15731239.8

    申请日：2015-05-26

    申请人： FACC AG

    发明人： KAMMERER, Bernhard ,  SCHÖRKHUBER, Jakob

    IPC分类号： B64D11/00

    CPC分类号： B64D11/003

    摘要： The invention relates to an overhead luggage compartment (1) for airplanes, comprising a stationary luggage compartment element (2) which can be secured to a structural element and comprising a movable luggage compartment element (3) which can be loaded with a piece of luggage, said compartments being connected together by a joint (4) such that the movable luggage compartment element (3) can be pivoted between an open position and a closed position. The overhead luggage compartment also comprises a device (10) for holding the movable luggage compartment element (3) in the open position, said device having a force transmission element (11) which is connected to the joint (4) between the stationary luggage compartment element (2) and the movable luggage compartment element (3). In the open position of the movable luggage compartment element (3), the joint (4) can be moved depending on the load state of the movable luggage compartment element (3), wherein when the movable luggage compartment element (3) is in the open position, the force transmission element (11) is arranged in an active position in the unloaded state and in an inactive position in the loaded state by means of a movement of the joint (4). In the active position of the force transmission element (11), a holding torque is exerted which counteracts the pivot of the movable luggage compartment element (3) from the open position in the direction of the closed position.

    摘要翻译： 一种用于飞机的高架行李舱，包括固定的行李箱元件，其可固定到结构元件并且包括可装载行李箱的可移动行李箱元件，所述隔间通过接头连接在一起，使得可移动 行李箱元件可以在打开位置和关闭位置之间枢转。 架空行李箱可以包括用于将可移动行李舱元件保持在打开位置的装置，所述装置具有连接到固定行李箱元件和可移动行李箱元件之间的接头的力传递元件。

    VORRICHTUNG ZUM ÖFFNEN EINER FLUGZEUGTÜR
    8.
    发明公开
    VORRICHTUNG ZUM ÖFFNEN EINER FLUGZEUGTÜR 有权
    用于开启一个平面DOOR

    公开(公告)号：EP3097012A1

    公开(公告)日：2016-11-30

    申请号：EP15708695.0

    申请日：2015-01-20

    申请人： FACC AG

    发明人： KAMMERER, Bernhard ,  SCHÖRKHUBER, Jakob ,  BURGHOZER, Thomas

    IPC分类号： B64C1/14

    CPC分类号： B64C1/143 ,  B64C1/066 ,  B64C1/1407 ,  B64C1/1461

    摘要： The invention relates to a device (1) for opening an aircraft door (2) provided in an aircraft fuselage (4), said device comprising: a support arm (3) that can be arranged in an articulated manner between the aircraft fuselage (4) and the aircraft door (2); an opening system (5) for opening the aircraft door (2) by lifting the aircraft door (2) from a closed position into an intermediate position and swivelling the aircraft door (2) from the intermediate position into an open position; a support arm cover (10) substantially entirely covering the support arm (3) in the closed position of the aircraft door (2), wherein the support arm cover (10) has a cover element (11) immovably arranged on the support arm (3), and a flap element (12) which, when the aircraft door (2) is opened, can swivel between a state in which said flap element is substantially flush with the cover element (11), and a state in which said flap element overlaps the cover element (11); and a guide system (13) for guiding the flap element (12) when the aircraft door (2) is opened, wherein the guide system (13) has at least one guide arm (14), one end of which is joined in an articulated manner to the support arm (3), and the other end of which is joined to at least one guide element (17), which guide element can be guided along a guide track (18) on the inner side of the flap element (12), when the aircraft door (2) is opened.

    DEKOMPRESSIONSEINHEIT
    9.
    发明公开
    DEKOMPRESSIONSEINHEIT 有权
    减压

    公开(公告)号：EP2630031A1

    公开(公告)日：2013-08-28

    申请号：EP11773654.6

    申请日：2011-10-13

    申请人： FACC AG

    发明人： PAMMINGER, Erich ,  KAMMERER, Bernhard

    IPC分类号： B64C1/10 ,  B64C1/20

    CPC分类号： B64C1/00 ,  B64C1/10 ,  B64C2001/009

    摘要： The invention relates to a decompression unit (1) for use in a decompression opening (2) of a wall element (3) of an aircraft, having a panel (5) which can be mounted via a frame (4) in or over the decompression opening (2) which panel (5) can be moved out of the frame (4) at a predetermined differential pressure Δρ in order to open the decompression opening (2). In order to form a decompression unit (1) of as simple a design as possible and with an optimum response behaviour, provision is made for the panel (5) to be formed by at least one hardened prepreg layer (6) with at least one separating joint (7) which is filled with cured resin as a weak point, which separating joint (7) breaks when the predetermined differential pressure (Δρ) is exceeded.