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    • 1. 发明申请
    • FLUGZEUGSITZVORRICHTUNG
    • 飞机座椅装置
    • WO2016166027A1
    • 2016-10-20
    • PCT/EP2016/057758
    • 2016-04-08
    • RECARO AIRCRAFT SEATING GMBH & CO KG
    • JUSSLI, ZoltanERB, Andreas
    • B60N3/00B64D11/06
    • B64D11/0638B60N3/004B64D11/00152B64D11/00153Y02T50/46
    • Die Erfindung geht aus von einer Flugzeugsitzvorrichtung mit einem Tischmodul (10a; 0b; 10c; 10d) und mit einem PED-Halter (36a; 36b; 36c; 36d), der dazu vorgesehen ist, 5 ein PED (38a; 38b; 38c; 38d) in einer Bedienposition auf dem Tischmodul (10a; 10b; 10c; 0d) zu lagern, wobei der PED-Halter (36a; 36b; 36c; 36d) wenigstens ein Halteelement (40a; 40b; 40c; 40d) aufweist, das schwenkbar mit dem Tischmodul (10a; 10b; 10c; 10d) verbunden ist. Es wird vorgeschlagen, dass der PED-Halter (36a; 36b; 36c; 36d) eine Schwenklagereinheit (42a; 42d) umfasst, die dazu vorgesehen ist, das Halteelement (40a; 40b; 40c; 40d) um mehr als 180 Grad zu verschwenken.
    • 本发明涉及一种具有表模块的飞机座椅设备(10A; 0B; 10C; 10D)和具有PED保持器(36A; 36B; 36C; 36D),其被提供给图5中,PED(38A; 38B; 38C; 在表模块上的操作位置存储0D)时,PED保持器(36A ;; 38D)(10A; 10B; 10C具有40D)可枢转地; 36B; 36C; 36D)至少一个保持元件(40A; 40B; 40C 被连接到该表模块(10D 10A; 10B ;; 10C)。 它提出,PED保持器(36A; 36D 36B; 36C);其被设置用于保持元件的枢转轴承部(42D 42A)的(40A; 40B; 40C; 40D),以大于180度的枢转 ,
    • 5. 发明申请
    • SEAT ATTACHMENT DEVICE
    • 座椅安装装置
    • WO2011116888A2
    • 2011-09-29
    • PCT/EP2011001216
    • 2011-03-11
    • RECARO AIRCRAFT SEATING GMBHHAEUSER MARKUS OTTMAR
    • HAEUSER MARKUS OTTMAR
    • B64D11/00B64D11/06
    • B64D11/00153B60R11/0235B64D11/06B64D11/0646
    • The invention relates to a seat attachment device, in particular an airline passenger seat attachment device, for the movable fastening of an object (12) to a seat (14), comprising a supporting arm part (16), a device receiving part (18) for fastening the object (12), an intermediate part (20) for coupling the device receiving part (18) to the supporting arm part (16), and at least one first joint (22) which is disposed between the supporting arm part (16) and the intermediate part (20) and has a first joint axis (24), and a second joint (26) which is disposed between the intermediate part (20) and the device receiving part (18) and has a second joint axis (28). According to the invention, the intermediate part (20) provides an offset (30) which offsets the first joint axis (24) of the first joint (22) and the second joint axis (28) of the second joint (26) with respect to one another in at least one projection direction.
    • 本发明涉及一种座椅安装装置,尤其是乘客座位安装装置,用于在座位(14)可移动地安装在被测物体(12),具有Tragarmstück(16),具有用于所述制品(12)的紧固设备接收件(18),具有 中间片(20),用于所述设备接收件(18)与所述Tragarmstück(16)联接,并具有至少一个第一,Tragarmstück之间(16)和中间件(20),其设置铰链(22),其具有第一铰链轴(24) (20)与设备接收件(18)之间的第二铰链(26)布置,所述铰链(26)具有第二铰链轴线(28)。 它建议,所述中间部件(20)提供的偏移(30)彼此错开,所述第一关节运动(22)和在投影中的至少一个方向上的第二关节运动(26)的第二铰链轴(28)的第一铰链轴(24)。
    • 8. 发明申请
    • INFORMATION DISPLAY SYSTEM FOR AIRCRAFT
    • 航空器信息显示系统
    • WO2006002852A2
    • 2006-01-12
    • PCT/EP2005/006903
    • 2005-06-27
    • AIRBUS DEUTSCHLAND GMBHHEYM, Detlef
    • HEYM, Detlef
    • B64D11/00153B64D11/0015B64D2011/0038G09F19/18Y02T50/46
    • In current passenger aircraft, signs are used to represent specific information, which reproduce the information as writing or a pictogram. According to one exemplary embodiment of the present invention, an information display system for aircraft is specified, comprising a light source, a projection means, and a housing. For this purpose, according to one exemplary embodiment of the present invention, the projection means is implemented in the form of a liquid crystal display, so that, in combination with a high-performance light-emitting diode and a suitable lens, static and dynamic information may be presented on arbitrarily shaped projection surfaces. The flexibility of the onboard information display is thus advantageously increased.
    • 在当前的客机中,标志用于表示特定的信息,这些信息以书面或象形图的形式重现信息。 根据本发明的一个示例性实施例,提供了一种用于飞行器的信息显示系统,包括光源,投影装置和壳体。 为此,根据本发明的一个示例性实施例,投影装置以液晶显示器的形式实现,使得与高性能发光二极管和合适的透镜相结合,静态和动态的 信息可以呈现在任意形状的投影表面上。 因此有利地增加了机载信息显示器的灵活性。