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    DEVICE FOR OPENING A PASSENGER DOOR IN CASE OF EMERGENCY
    1.
    发明申请
    DEVICE FOR OPENING A PASSENGER DOOR IN CASE OF EMERGENCY 有权
    在紧急情况下打开乘客门的装置

    公开(公告)号：US20110131986A1

    公开(公告)日：2011-06-09

    申请号：US12921520

    申请日：2009-03-02

    申请人： Stefan Andres ,  Hans Bartosch ,  Wolfgang Buchs ,  Manfred Held ,  Rainer Hertle

    发明人： Stefan Andres ,  Hans Bartosch ,  Wolfgang Buchs ,  Manfred Held ,  Rainer Hertle

    IPC分类号： B64C1/32 ,  F01B29/08 ,  E05F15/04 ,  B64C1/14 ,  B64D25/00

    CPC分类号： B64C1/1407 ,  E05F15/53 ,  E05F15/54 ,  E05F15/63 ,  E05F15/72 ,  E05Y2201/422 ,  E05Y2201/434 ,  E05Y2201/72 ,  E05Y2800/252 ,  E05Y2800/67 ,  E05Y2900/502 ,  E05Y2900/531 ,  F42B3/006 ,  F42B3/04

    摘要： The invention relates to a device for opening a passenger door (1) of an aircraft in case of emergency, which is fastened so it is manually pivotable on the fuselage (3) of the aircraft via a hinge and/or support arm configuration (2), an auxiliary-energy-operated emergency opening drive (4) being provided between the fuselage (3) and the passenger door (1), which automatically opens the passenger door (1) in accordance with an emergency control unit (5), the auxiliary energy for the emergency opening drive (4) being pyrotechnic energy, whose gas expanding inside an expansion chamber (6) after triggering by the emergency control unit (5) impinges the emergency opening drive (4) with pressure medium to open the passenger door (1), wherein said emergency opening drive (4) generates a rotational movement.

    摘要翻译： 本发明涉及一种用于在紧急情况下打开飞机的乘客门（1）的装置，其被紧固以便可以通过铰链和/或支撑臂构造（2）手动地枢转在飞行器的机身（3）上 ），在机身（3）和乘客门（1）之间设置有辅助能量操作的应急开启驱动器（4），根据应急控制单元（5）自动打开乘客门（1） 用于紧急打开驱动器（4）的辅助能量是烟火能量，其在由应急控制单元（5）触发之后在膨胀室（6）内扩张的气体用压力介质撞击紧急打开驱动器（4）以打开乘客 门（1），其中所述紧急打开驱动器（4）产生旋转运动。

    Rotating drive mechanism for swinging doors especially on vehicles
    2.
    发明授权
    Rotating drive mechanism for swinging doors especially on vehicles 失效
    特别是在车辆上摆动门的旋转驱动机构

    公开(公告)号：US4838102A

    公开(公告)日：1989-06-13

    申请号：US158182

    申请日：1988-02-19

    申请人： Jurgen Bode ,  Manfred Horn

    发明人： Jurgen Bode ,  Manfred Horn

    IPC分类号： B61D19/02 ,  E05F15/54 ,  F15B15/08

    CPC分类号： F15B15/068 ,  B61D19/02 ,  E05F15/54 ,  E05Y2900/51 ,  Y10T74/18888 ,  Y10T74/19721

    摘要： A rotating drive mechanism for swinging doors, especially on vehicles, with a helical transmission consisting of a stator that is rigidly connected to the housing of the rotating drive mechanism, a rotor that can rotate but cannot move axially and that is rigidly connected to the driveshaft, a coupling component that moves axially to rotate the rotor in relation to the stator, and a pneumatic or hydraulic drive cylinder with a piston rod that is connected to the coupling component. The drive cylinder is an annular cylinder that has an outer and an inner jacket as well as an annular piston between the inner and the outer jacket. The coupling component is a nut that extends into the inner cylinder jacket and surrounds a rotor in the form of a threaded spindle. The rotor extends coaxially through the inside of the inner jacket and is, where it emerges from the housing, in one piece with the stub of the takeoff shaft. The coupling component is non-rotationally connected to an axial positioning mechanism that has rollers that travel in a positioning slot in the stator.

    摘要翻译： 一种旋转驱动机构，用于特别是在车辆上摆动的门，具有由刚性地连接到旋转驱动机构的壳体的定子构成的螺旋传动装置，能够旋转但不能轴向移动且刚性地连接到驱动轴的转子 ，联接部件，其轴向移动以相对于定子旋转转子;以及气动或液压驱动气缸，其具有连接到联接部件的活塞杆。 驱动气缸是环形气缸，其具有外护套和内护套以及在内护套和外护套之间的环形活塞。 联接部件是延伸到内筒套中并围绕螺纹心轴形式的转子的螺母。 转子同轴地延伸通过内护套的内部，并且在其中从壳体出来的部分与起飞轴的短柱一体地延伸。 联接部件非旋转地连接到具有在定子中的定位槽中行进的辊的轴向定位机构。

    POWERED GATE
    8.
    发明申请
    POWERED GATE 审中-公开
    动力门

    公开(公告)号：US20100319262A1

    公开(公告)日：2010-12-23

    申请号：US12864712

    申请日：2009-01-30

    申请人： Edward J. Stull

    发明人： Edward J. Stull

    IPC分类号： E05F15/02 ,  E06B11/02

    CPC分类号： E05F15/614 ,  E05F15/54 ,  E05Y2201/434 ,  E05Y2201/628 ,  E05Y2800/232 ,  E05Y2800/262 ,  E05Y2800/28 ,  E05Y2900/40

    摘要： A disclosed example powered gate assembly includes an actuator disposed within a post integral to the gate assembly. The post also includes a drive mechanism for moving the gate assembly between open and closed positions. The actuator and drive mechanism are completely disposed within the gate. The integral construction of the first post and therein the actuator provides a substantially complete automated gate assembly that is ready for installation. The actuator and drive mechanism are disposed within a post of the gate assembly and therefore are protected from the elements and undesired tampering.

    摘要翻译： 公开的示例动力门组件包括设置在与门组件一体的柱内的致动器。 该柱还包括用于在打开位置和关闭位置之间移动门组件的驱动机构。 致动器和驱动机构完全设置在门内。 第一柱和其中的致动器的整体构造提供了准备安装的基本上完整的自动门组件。 致动器和驱动机构设置在门组件的柱内，因此被保护免受元件和不期望的篡改。

    Vehicle actuated gate opening/closing system
    9.
    发明授权
    Vehicle actuated gate opening/closing system 失效
    车辆开启门开/关系统

    公开(公告)号：US07114290B2

    公开(公告)日：2006-10-03

    申请号：US10794598

    申请日：2004-03-08

    申请人： Bernhard Stubbe

    发明人： Bernhard Stubbe

    IPC分类号： E05F13/02

    CPC分类号： E06B11/04 ,  E05F7/02 ,  E05F13/00 ,  E05F13/04 ,  E05F15/54 ,  E05Y2900/40

    摘要： A gate opening system which includes a barrier and a barrier mounting adapted to mount the barrier in an open or closed condition, a retention device to secure the barrier in an open or closed condition, a drive element, and an energy transmission system, whereby energy is transferred from the weight of a vehicle and is in turn transmitted through the transmission system to rotate the drive element, causing the barrier mounting to be lifted, the disengagement of the retention device, and the barrier thereby opened or closed.

    摘要翻译： 一种闸门打开系统，其包括适于将障碍物安装在打开或关闭状态的阻挡物和阻挡物安装件，用于将屏障固定在开启或关闭状态的保持装置，驱动元件和能量传输系统，由此能量 从车辆的重量被转移，并且又通过传动系统传递以使驱动元件旋转，导致挡板安装被提升，保持装置和挡板的分离由此打开或关闭。

    Aircraft door hinge mechanism with selectively triggerable actuator
    10.
    发明授权
    Aircraft door hinge mechanism with selectively triggerable actuator 失效
    具有选择性触发执行器的飞机门铰链机构

    公开(公告)号：US5180121A

    公开(公告)日：1993-01-19

    申请号：US696245

    申请日：1991-05-06

    申请人： Eddie D. Banks ,  Tomio Hamatani ,  Chung-Wah F. Wong

    发明人： Eddie D. Banks ,  Tomio Hamatani ,  Chung-Wah F. Wong

    IPC分类号： B64C1/14 ,  E05F15/04

    CPC分类号： B64C1/143 ,  B64C1/1407 ,  E05F15/54 ,  E05F15/72 ,  E05Y2900/502 ,  E05Y2900/531 ,  Y10T16/53992

    摘要： A cam actuator (12) for rapidly opening an aircraft door (14) that is attached to an aircraft fuselage (18) by a hinge assembly (26). The actuator includes a piston (40), a piston rod (42) that is secured to the piston and rotating sleeve (44) that is fitted over the piston rod that functions as the hinge pin between a hinge clevis (26) on the aircraft and a hinge arm lug (54) on the hinge assembly. The piston is contained within a housing (38) adapted to receive a pressurized pneumatic gas. An annular cam (50) through which the piston rod travels and that is formed with an outer surface (104) having a helical profile is attached to the hinge clevis. A cam follower (46) is attached for the sleeve so as to rotate in unison therewith. The hinge arm lug (54) is also secured to the sleeve (44) for rotation. When the actuator of this invention is triggered, the piston rod (42) urges the cam follower (46 ) against the cam (50) so as to cause the cam follower to rotate. The cam follower (46) in turn rotates the sleeve (44) so as to simultaneously rotate the hinge arm lug (54). As a result of this rotation, the hinge is pivoted away from the hinge clevis so as to urge the aircraft door open.