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    • 1. 发明授权
    • Connecting device
    • 连接装置
    • US08435040B2
    • 2013-05-07
    • US13144013
    • 2010-02-23
    • Sascha CostabelMarkus Schmidt
    • Sascha CostabelMarkus Schmidt
    • H01R33/00
    • F16B5/00B60R13/0206B64C1/066F16B2200/10Y10T403/24
    • A connecting device (10) is provided for releasably connecting a fitting piece, such as an interior lining, to a supporting structure, such as a fuselage. The connecting device (10) includes a plug-in holding mechanism (50) including a bushing piece (52) and a connecting pin (75) that can be releasably locked therein. A bent connecting arm (60), to which the connecting pin is fastened, is releasably fastened to a structural holder (40) mounted on the supporting structure. In one position, the connecting arm (60) is plugged into the structural holder (40) and is releasably locked therein. In a second position (125), in which the connecting arm (60) is rotated 180° about the longitudinal axis thereof, an electrical contact device (90) is additionally inserted between the connecting arm (60) and the bushing piece (52). Hence, the same structural holder (40) and the same connecting arm (60) allow the fitting piece and the supporting structure to be connected to one another with or without connecting a contact device (90) therebetween.
    • 连接装置(10)被设置用于将诸如内衬之类的配件可释放地连接到诸如机身的支撑结构。 连接装置(10)包括插入式保持机构(50),该插入保持机构包括可拆卸地锁定在其中的衬套件(52)和连接销(75)。 连接销紧固在其上的弯曲的连接臂(60)可释放地紧固到安装在支撑结构上的结构保持架(40)上。 在一个位置,连接臂(60)被插入结构保持器(40)中并且可释放地锁定在其中。 在其中连接臂(60)围绕其纵向轴线旋转180°的第二位置(125)中,电连接装置(90)另外插入在连接臂(60)和套管件(52)之间, 。 因此,相同的结构保持器(40)和相同的连接臂(60)允许配件和支撑结构在其间具有或不连接接触装置(90)而彼此连接。
    • 2. 发明申请
    • CONNECTING DEVICE
    • 连接设备
    • US20110318091A1
    • 2011-12-29
    • US13144013
    • 2010-02-23
    • Sascha CostabelMarkus Schmidt
    • Sascha CostabelMarkus Schmidt
    • H01R13/04F16B17/00
    • F16B5/00B60R13/0206B64C1/066F16B2200/10Y10T403/24
    • A connecting device (10) is provided for releasably connecting a fitting piece, such as an interior lining, to a supporting structure, such as a fuselage. The connecting device (10) includes a plug-in holding mechanism (50) including a bushing piece (52) and a connecting pin (75) that can be releasably locked therein. A bent connecting arm (60), to which the connecting pin is fastened, is releasably fastened to a structural holder (40) mounted on the supporting structure. In one position, the connecting arm (60) is plugged into the structural holder (40) and is releasably locked therein. In a second position (125), in which the connecting arm (60) is rotated 180° about the longitudinal axis thereof, an electrical contact device (90) is additionally inserted between the connecting arm (60) and the bushing piece (52). Hence, the same structural holder (40) and the same connecting arm (60) allow the fitting piece and the supporting structure to be connected to one another with or without connecting a contact device (90) therebetween.
    • 连接装置(10)被设置用于将诸如内衬之类的配件可释放地连接到诸如机身的支撑结构。 连接装置(10)包括插入式保持机构(50),该插入保持机构包括可拆卸地锁定在其中的衬套件(52)和连接销(75)。 连接销紧固在其上的弯曲的连接臂(60)可释放地紧固到安装在支撑结构上的结构保持架(40)上。 在一个位置,连接臂(60)被插入结构保持器(40)中并且可释放地锁定在其中。 在其中连接臂(60)围绕其纵向轴线旋转180°的第二位置(125)中,电连接装置(90)另外插入在连接臂(60)和套管件(52)之间, 。 因此,相同的结构保持器(40)和相同的连接臂(60)允许配件和支撑结构在其间具有或不连接接触装置(90)而彼此连接。
    • 3. 发明授权
    • Plug-type mount
    • 插头式安装
    • US07955111B2
    • 2011-06-07
    • US12745273
    • 2008-12-17
    • Sascha CostabelMarkus Schmidt
    • Sascha CostabelMarkus Schmidt
    • H01R13/28
    • H01R13/73F16B5/0628H01R2201/26
    • A plug-type mount is provided for releasably holding an equipment part such as a panel or an interior trim part on a sub-frame such as a fuselage. The plug-type mount (5) includes a first holder (30) and a second holder (35) which can be fastened to one another with the aid of a holding pin (11) and a housing (20), in which the holding pin (11) can be releasably locked. The holders (30, 35) carry in each case at least one electrical contact (33, 34) and are configured in such a way that, in the case of the holding pin (11) being locked in the housing (20), the holders (30, 35) are fastened to one another and the electrical contacts (33, 34) are connected electrically. Excessive cable lengths can be avoided by the preferable use of the plug-type mount (5) in an airplane because the electrical connection is also produced and disconnected as the mechanical connection is produced and disconnected.
    • 提供插头型安装件,用于将诸如面板或内饰件的设备部件可释放地保持在诸如机身的子框架上。 插头式安装座(5)包括第一保持器(30)和第二保持器(35),第二保持器可借助于保持销(11)和壳体(20)彼此紧固在一起,其中保持 销(11)可以可释放地锁定。 保持器(30,35)在每种情况下承载至少一个电触头(33,34),并且被构造成使得在保持销(11)被锁定在壳体(20)的情况下, 保持器(30,35)彼此紧固并且电触头(33,34)电连接。 通过在飞机上优选使用插头式安装座(5)可以避免电缆长度过长,因为在制造和断开机械连接时电连接也被产生和断开。
    • 4. 发明申请
    • PLUG-TYPE MOUNT
    • US20100304588A1
    • 2010-12-02
    • US12745273
    • 2008-12-17
    • Sascha CostabelMarkus Schmidt
    • Sascha CostabelMarkus Schmidt
    • H01R13/62H01R24/00
    • H01R13/73F16B5/0628H01R2201/26
    • A plug-type mount is provided for releasably holding an equipment part such as a panel or an interior trim part on a sub-frame such as a fuselage. The plug-type mount (5) includes a first holder (30) and a second holder (35) which can be fastened to one another with the aid of a holding pin (11) and a housing (20), in which the holding pin (11) can be releasably locked. The holders (30, 35) carry in each case at least one electrical contact (33, 34) and are configured in such a way that, in the case of the holding pin (11) being locked in the housing (20), the holders (30, 35) are fastened to one another and the electrical contacts (33, 34) are connected electrically. Excessive cable lengths can be avoided by the preferable use of the plug-type mount (5) in an airplane because the electrical connection is also produced and disconnected as the mechanical connection is produced and disconnected.
    • 提供插头型安装件,用于将诸如面板或内饰件的设备部件可释放地保持在诸如机身的子框架上。 插头式安装座(5)包括第一保持器(30)和第二保持器(35),第二保持器可借助于保持销(11)和壳体(20)彼此紧固在一起,其中保持 销(11)可以可释放地锁定。 保持器(30,35)在每种情况下承载至少一个电触头(33,34),并且被构造成使得在保持销(11)被锁定在壳体(20)的情况下, 保持器(30,35)彼此紧固并且电触头(33,34)电连接。 通过在飞机上优选使用插头式安装座(5)可以避免电缆长度过长,因为在制造和断开机械连接时电连接也被产生和断开。