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    • 2. 发明申请
    • Force supporting module for providing a load-dependent supporting force
    • 用于提供负载相关支撑力的力支撑模块
    • US20050218264A1
    • 2005-10-06
    • US10514404
    • 2003-05-19
    • Oleg GrafRalf Poberschnigg
    • Oleg GrafRalf Poberschnigg
    • B64D11/00B64C1/20B64C1/22B64D47/00
    • B64D11/003Y02T50/46
    • The invention relates to a force assistance module (10) for providing a load-dependent assistance force, in particular for a lowerable overhead luggage compartment in an aircraft, comprising a housing (18), a spring system for generating the assistance force, of which spring system one end is coupled pivotally about an axis (Z) in the housing (18) and the other, opposite end defines a force application point (P), a force-transmitting device fastened to or in the vicinity of the force application point (P) for transmitting assistance force to a location remote from the force assistance module, a support (36), which is mounted rotatably in the housing (18) and on which a path (40) is provided, along which the force application point (P) is displaceable back and forth between a first end point (A) and a second end point (B), and an adjusting device (52), which interacts with the support (36) and a load sensor and which as a function of the load detected by the load sensor rotates the support (36) in order to vary the angle between the force application direction of the assistance force at the force application point (P) and the force-transmitting device and hence adapt the value of the assistance force acting upon the force-transmitting device to the detected load.
    • 本发明涉及一种用于提供负载相关的辅助力的力辅助模块(10),特别是用于飞行器中的可降低架空行李箱,包括壳体(18),用于产生辅助力的弹簧系统 弹簧系统一端围绕壳体(18)中的轴线(Z)枢转,另一端相对的端部限定施力点(P),紧固在施力点附近或附近的力传递装置 (P),用于将辅助力传递到远离所述力辅助模块的位置,支撑件(36),其可旋转地安装在所述壳体(18)中并且设置有路径(40),所述力施加点 (P)可在第一端点(A)和第二端点(B)之间来回移动,以及调节装置(52),其与支撑件(36)和负载传感器相互作用,并且作为功能 由负载传感器检测到的负载 旋转支撑件(36)以改变在施力点(P)处的辅助力的力施加方向与力传递装置之间的角度,并因此调整作用在力传递上的辅助力的值 设备到检测到的负载。
    • 4. 发明授权
    • Lowerable luggage compartment with a rear force supporting device
    • 具有后力支撑装置的可下放的行李箱
    • US07118068B2
    • 2006-10-10
    • US10514405
    • 2003-05-19
    • Oleg GrafRalf Poberschnigg
    • Oleg GrafRalf Poberschnigg
    • B64D11/00
    • B64D11/003Y02T50/46
    • A lowerable luggage compartment (10); in particular for a passenger aircraft, comprises a force assistance device (12) disposed behind the back of the luggage compartment (10) for providing an assistance force during opening and/or closing of the luggage compartment (10). The force provided by the force assistance device (12) is transmitted by means of a flexible force-transmitting device (cable 14) to the luggage compartment (10). The force assistance device (12) is the sole force assistance device acting upon the luggage compartment (10). In order to be able to enlarge the useful volume of the luggage compartment (10) without increasing its external dimensions and in order to combine improved maintainability with weight saving, the force assistance device takes the form of a force assistance module (12) with its own housing (24), in which a spring system generates the assistance force, and the force provided by the force assistance device is transmitted by means of a single flexible force-transmitting device to the luggage compartment (10).
    • 可行的行李箱(10); 特别是对于客机,包括设置在行李箱(10)后面的力辅助装置(12),用于在行李箱(10)的打开和/或关闭期间提供辅助力。 由力辅助装置(12)提供的力通过柔性力传递装置(电缆14)传递到行李箱(10)。 力辅助装置(12)是作用在行李箱(10)上的唯一的力辅助装置。 为了能够在不增加其外部尺寸的情况下扩大行李箱(10)的有用体积,并且为了将改进的可维护性与减轻重量相结合,力辅助装置采取其辅助模块(12)的形式,其中 其中弹簧系统产生辅助力,并且由辅助装置提供的力通过单个柔性力传递装置传递到行李箱(10)。
    • 5. 发明授权
    • Force supporting module for providing a load-dependent supporting force
    • 用于提供负载相关支撑力的力支撑模块
    • US07143977B2
    • 2006-12-05
    • US10514404
    • 2003-05-19
    • Oleg GrafRalf Poberschnigg
    • Oleg GrafRalf Poberschnigg
    • B64D11/00
    • B64D11/003Y02T50/46
    • The invention relates to a force assistance module (10) for providing a load-dependent assistance force, in particular for a lowerable overhead luggage compartment in an aircraft, comprising a housing (18), a spring system for generating the assistance force, of which spring system one end is coupled pivotally about an axis (Z) in the housing (18) and the other, opposite end defines a force application point (P), a force-transmitting device fastened to or in the vicinity of the force application point (P) for transmitting assistance force to a location remote from the force assistance module, a support (36), which is mounted rotatably in the housing (18) and on which a path (40) is provided, along which the force application point (P) is displaceable back and forth between a first end point (A) and a second end point (B), and an adjusting device (52), which interacts with the support (36) and a load sensor and which as a function of the load detected by the load sensor rotates the support (36) in order to vary the angle between the force application direction of the assistance force at the force application point (P) and the force-transmitting device and hence adapt the value of the assistance force acting upon the force-transmitting device to the detected load.
    • 本发明涉及一种用于提供负载相关的辅助力的力辅助模块(10),特别是用于飞行器中的可降低架空行李箱,包括壳体(18),用于产生辅助力的弹簧系统 弹簧系统一端围绕壳体(18)中的轴线(Z)枢转,另一端相对的端部限定施力点(P),紧固在施力点附近或附近的力传递装置 (P),用于将辅助力传递到远离所述力辅助模块的位置,支撑件(36),其可旋转地安装在所述壳体(18)中并且设置有路径(40),所述力施加点 (P)可在第一端点(A)和第二端点(B)之间来回移动,以及调节装置(52),其与支撑件(36)和负载传感器相互作用,并且作为功能 由负载传感器检测到的负载 旋转支撑件(36)以改变在施力点(P)处的辅助力的力施加方向与力传递装置之间的角度,并因此调整作用在力传递上的辅助力的值 设备到检测到的负载。
    • 6. 发明申请
    • Lowerable luggage compartment with a rear force supporting device
    • 具有后力支撑装置的可下放的行李箱
    • US20050224643A1
    • 2005-10-13
    • US10514405
    • 2003-05-19
    • Oleg GrafRalf Poberschnigg
    • Oleg GrafRalf Poberschnigg
    • B64D11/00B64C1/20B64C1/22B64D47/00
    • B64D11/003Y02T50/46
    • A lowerable luggage compartment (10), in particular for a passenger aircraft, comprises a force assistance device (12) disposed behind the back of the luggage compartment (10) for providing an assistance force during opening and/or closing of the luggage compartment (10). The force provided by the force assistance device (12) is transmitted by means of a flexible force-transmitting device (cable 14) to the luggage compartment (10). The force assistance device (12) is the sole force assistance device acting upon the luggage compartment (10). In order to be able to enlarge the useful volume of the luggage compartment (10) without increasing its external dimensions and in order to combine improved maintainability with weight saving, the force assistance device takes the form of a force assistance module (12) with its own housing (24), in which a spring system generates the assistance force, and the force provided by the force assistance device is transmitted by means of a single flexible force-transmitting device to the luggage compartment (10).
    • 特别是用于客机的可行的行李箱(10)包括设置在行李箱(10)后面的力辅助装置(12),用于在行李箱的打开和/或关闭期间提供辅助力( 10)。 由力辅助装置(12)提供的力通过柔性力传递装置(电缆14)传递到行李箱(10)。 力辅助装置(12)是作用在行李箱(10)上的唯一的力辅助装置。 为了能够在不增加其外部尺寸的情况下扩大行李箱(10)的有用体积,并且为了将改进的可维护性与减轻重量相结合,力辅助装置采取其辅助模块(12)的形式,其中 其中弹簧系统产生辅助力,并且由辅助装置提供的力通过单个柔性力传递装置传递到行李箱(10)。
    • 7. 发明授权
    • Baggage holder for an aircraft and aircraft having the baggage holder
    • 具有行李架的飞机和飞机的行李架
    • US09033279B2
    • 2015-05-19
    • US13679244
    • 2012-11-16
    • Oleg GrafMax FailenschmidUlrich EversAnnica DieterichSimon MerzMichael Zinke
    • Oleg GrafMax FailenschmidUlrich EversAnnica DieterichSimon MerzMichael Zinke
    • B64D11/00
    • B64D11/003Y02T50/46
    • Baggage compartment 1 for an aircraft, wherein the baggage compartment 1 comprises a housing 2 and a baggage holder 3, wherein the baggage holder 3 is swivel-mounted about a swivel axis A in the housing 2, wherein, the swivel axis A intersects, in its longitudinal extent, a holder side wall 32 of the baggage holder 3 and/or a housing side wall 21 of the housing 2, wherein the baggage holder 3 can be moved from a closed position G into an open position Ö with a first swivel movement S1 and the baggage compartment 1 is opened and wherein the baggage holder 3 can be moved from the open position Ö into the closed position G with a second swivel movement S2 and the baggage compartment 1 is closed, wherein the baggage compartment 1 comprises a drive device 6 having at least one drive motor 9, wherein the drive device 6 is designed to drive the baggage holder 3 during the first and/or second swivel movement S1; S2 and to open or close the baggage compartment 1, wherein the drive device 6 is connected to the holder side wall 32 on one side and to the housing side wall 21 on the other side.
    • 用于飞行器的行李舱1,其中行李舱1包括壳体2和行李托架3,其中行李托架3绕壳体2中的旋转轴线A旋转安装,其中旋转轴线A相交于 其纵向范围,行李架3的保持器侧壁32和/或壳体2的壳体侧壁21,其中行李托架3可以从关闭位置G移动到第一旋转运动的打开位置 S1和行李舱1打开,其中行李托架3可以通过第二旋转运动S2从打开位置Ö移动到关闭位置G,并且行李舱1关闭,其中行李舱1包括驱动装置 6具有至少一个驱动马达9,其中驱动装置6设计成在第一和/或第二旋转运动S1期间驱动行李托架3; S2并打开或关闭行李舱1,其中驱动装置6在一侧连接到保持器侧壁32并在另一侧连接到壳体侧壁21。
    • 8. 发明授权
    • Aircraft window darkening system
    • 飞机窗户变暗系统
    • US08157214B2
    • 2012-04-17
    • US12028072
    • 2008-02-08
    • Alexander SchwarzOleg Graf
    • Alexander SchwarzOleg Graf
    • B64C1/14
    • B64C1/1484E06B9/24
    • An aircraft window darkening system includes a movable slide that darkens an aircraft window when in a closed position and does not darken the aircraft window when in an open position. The darkening system also includes a motor which is coupled to the slide in order to move the slide. The motor may be attached to a window frame of an aircraft window. The slide may have a handle for moving the slide. The motor may be disposed behind a region covered by a frame cover and behind a holding ring, so that the motor is accessible from the aircraft cabin when the holding ring is removed.
    • 飞机窗户变暗系统包括可移动的滑动件,当处于关闭位置时使飞行器窗口变暗,并且当处于打开位置时不使飞行器窗口变暗。 变暗系统还包括电动机,其联接到滑块以移动滑块。 马达可以附接到飞机窗的窗框上。 幻灯片可能具有用于移动幻灯片的手柄。 电动机可以设置在由框架盖子覆盖的区域的后面和保持环的后面,使得当移除保持环时,电机可从飞机机舱接近。
    • 10. 发明授权
    • Force assisting system for luggage system
    • 行李系统助力系统
    • US08028957B2
    • 2011-10-04
    • US11860847
    • 2007-09-25
    • Christian WolfOleg Graf
    • Christian WolfOleg Graf
    • B64D11/00
    • B64D11/003
    • A system for reducing the manual force required to move a lowerable shell of a luggage compartment in a passenger aircraft includes a load determination device for determining a load acting on the lowerable shell of the luggage compartment, and a state detection device for detecting whether the lowerable shell is in a closed position or an open position. The system also includes a force assisting device for applying a constant assisting force which opposes the load acting on the lowerable shell. The system further includes an actuating device adapted to move the force assisting device from a first inactive operating state to a second active operating state when the lowerable shell is in the open position and the load acting on the lowerable shell exceeds a predetermined threshold value.
    • 用于减少在客机中移动行李箱的可下降壳体所需的手动力的系统包括:负载确定装置,用于确定作用在行李箱的可下降壳体上的负载;以及状态检测装置,用于检测是否可下降 壳处于关闭位置或打开位置。 该系统还包括用于施加与作用在可下降壳上的负载相对的恒定辅助力的力辅助装置。 该系统还包括一个致动装置,该致动装置适用于当可下降的壳体处于打开位置并且作用在可下降的壳体上的负载超过预定阈值时,将力辅助装置从第一非活动操作状态移动到第二主动操作状态。