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    • 41. 发明申请
    • LOCKING ELEMENT
    • 锁定元件
    • US20120119026A1
    • 2012-05-17
    • US13379947
    • 2009-06-22
    • Thomas HuberRichard Holzner
    • Thomas HuberRichard Holzner
    • B64C1/20B64D9/00B60P7/13
    • B64D9/003
    • To secure containers in a cargo bay of an aircraft, locking elements are known comprising locking lugs which can move from a locked position to a rest position. The locking lugs engage in engagement recesses of freight items. On movement of the locking lugs from the locked position to the rest position, the locking lugs can seize in the engagement recesses. A locking element is proposed to which a pair of locking lugs is allocated which in the locked position each have a stop surface which can be brought into engagement on a stop edge of the engagement recess, wherein the locking lugs are mounted mobile such that on movement from the locked position to a rest position, the two stop surfaces separate from the stop edges. As a result the space required in the holding direction for the locking lugs and the risk of seizing of the locking lugs in the engagement recess are substantially reduced.
    • 为了将集装箱固定在飞机的货舱中,已知锁定元件包括可从锁定位置移动到静止位置的锁定凸耳。 锁定凸耳接合货物的接合凹槽。 在锁定凸耳从锁定位置移动到静止位置时,锁定凸耳可以卡在接合凹槽中。 提出了一种锁定元件,其中分配有一对锁定凸耳,其在锁定位置中分别具有止动表面,该止动表面可以在接合凹部的止动边缘上接合,其中锁定凸耳被安装移动,使得在移动 从锁定位置到静止位置,两个止动表面与止动边缘分开。 结果,在锁定凸耳的保持方向上所需的空间和接合凹槽中的锁定凸耳的卡住风险显着减小。
    • 42. 发明申请
    • Floor Module of a Cargo Deck in the Hull of an Aircraft
    • 飞机船体货舱地板模块
    • US20100230537A1
    • 2010-09-16
    • US12721470
    • 2010-03-10
    • Thomas HuberRichard Holzner
    • Thomas HuberRichard Holzner
    • B64C1/20
    • B64D9/00B64C1/20B64C2211/00Y02T50/46
    • Floor modules of a cargo deck in a hull of an aircraft which comprise support devices for carrying functional elements, e.g. panels, roller conveyors or ball mats, are provided. The support devices are attachable in the hull of the aircraft directly or by way of intermediate elements. To improve stability at reduced weight, end support devices, as seen in the aircraft's longitudinal direction, have a thickness reduced in such a way compared to the other support devices of the floor module that only together with the end support devices of a floor module installed adjacently in the hull do they ensure a loading capacity that corresponds to at least the loading capacity of the other support devices.
    • 飞机外壳中的货物甲板的地板模块,其包括用于承载功能元件的支撑装置,例如, 面板,滚筒输送机或球垫。 支撑装置可直接或通过中间元件附接在飞机的船体中。 为了在减轻重量的情况下提高稳定性,如在飞行器的纵向方向上看到的端部支撑装置与底板模块的其它支撑装置相比,其厚度减小,仅与地板模块的端部支撑装置一起安装 他们相应地在船体上确保了至少对应于其他支持装置的装载能力的装载能力。
    • 46. 发明授权
    • Roller drive unit
    • 滚筒驱动单元
    • US5960934A
    • 1999-10-05
    • US53326
    • 1998-04-01
    • Thomas HuberRichard Holzner
    • Thomas HuberRichard Holzner
    • B65G13/06B65G13/02
    • B65G13/065
    • A roller drive unit to propel objects, in particular cargo containers, on a conveyor track is proposed, which comprises an electric motor (20) to rotate a drive roller (30). The drive roller (30) extends substantially across the entire width of a frame (10) of the roller drive unit and is subdivided in the middle to form two drive-roller components (31, 32). The two drive-roller components (31, 32) are rotatably mounted on the frame (10) in a bearing (33) in the middle of the drive roller. The roller drive unit comprises a lifting mechanism (41, 42) comprising paired components disposed symmetrically about the middle of the drive roller (30) and about the bearing (33). As a result of this symmetrical arrangement of the drive roller (30) and the lifting mechanism (41, 42), a good load distribution and a stable retention of the drive roller (30) in its raised position are achieved.
    • 提出了一种在传送轨道上推进物体特别是货物集装箱的辊驱动单元,其包括用于使驱动辊(30)旋转的电动机(20)。 驱动辊(30)基本上跨过辊驱动单元的框架(10)的整个宽度延伸,并且在中间被细分成两个驱动辊部件(31,32)。 两个驱动辊部件(31,32)在驱动辊的中间的轴承(33)中可旋转地安装在框架(10)上。 辊驱动单元包括提升机构(41,42),包括围绕驱动辊(30)的中间和围绕轴承(33)对称设置的成对部件。 由于驱动辊(30)和提升机构(41,42)的这种对称布置的结果,实现了良好的负载分布和驱动辊(30)在其升高位置的稳定保持。
    • 47. 发明授权
    • Cargo latch
    • 货物锁
    • US5871317A
    • 1999-02-16
    • US749537
    • 1996-11-15
    • Thomas HuberJurgen VolkelRichard Holzner
    • Thomas HuberJurgen VolkelRichard Holzner
    • B64D9/00B60P7/08
    • B64D9/003
    • So-called butterfly latches are known, by way of which containers, pallets or similar items of freight can be secured within the cargo area of an aircraft. These comprise a frame that can be attached to holding rails on the floor of the cargo area. In the present latch, in the frame is disposed a double latch hook comprising two arms that are hinged to one another at first ends and at these first ends are provided with hook elements so constructed as to engage and retain items of cargo. At second ends the arms are mounted in the frame so that they can move in a plane of rotation in such a way that when they are struck by an item of cargo travelling in a first horizontal direction parallel to the plane of rotation, the first ends of the arms are deflected downward from an upper operating position toward the frame. To prevent unintended collapse of the arms, there are provided releasable locking mechanisms that in their locked position block downward rotation of the arms in such a way that the arms can be deflected downward only when unlocked by the frontal impact of an item of cargo moving in the first horizontal direction against one of the arms.
    • 已知所谓的蝶形闩锁,通过这种方式可以在飞机的货物区域内固定集装箱,托盘或类似物品。 这些框架包括可以连接到货物区域地板上的保持轨道的框架。 在当前的闩锁中,在框架中设有一个双钩子钩子,它包括在第一端部彼此铰接的两个臂,并且在这些第一端部设置有钩构件,以构成接合和保持货物的物品。 在第二端,臂被安装在框架中,使得它们可以在旋转平面中移动,使得当它们被平行于旋转平面的第一水平方向行进的货物撞击时,第一端 的臂从上部操作位置朝向框架向下偏转。 为了防止臂的意外塌陷,提供了可释放的锁定机构,其处于其锁定位置阻止臂的向下旋转,使得仅当货物移动的前部碰撞而被解锁时,臂可以向下偏转 相对于其中一个手臂的第一个水平方向。
    • 48. 发明授权
    • Roller drive unit
    • 滚筒驱动单元
    • US06834757B2
    • 2004-12-28
    • US09832649
    • 2001-04-11
    • Richard HolznerStefan MichailovMatthias Urch
    • Richard HolznerStefan MichailovMatthias Urch
    • B65G1312
    • B65G13/073B64D9/00B64D2009/006B65G13/065B65G13/075
    • Roller drive units are used for conveying objects, in particular cargo containers, on a roller conveyor track of an aircraft. They comprise a drive motor, a planetary gear with an input connected to the drive motor and with a first as well as a second gear output. A drive roller is connected to the first gear output to propel the object and a lifting apparatus is connected to the second gear output to lift the drive roller out of a retracted resting position, in which the drive roller does not contact the object, into a raised operating position in which the drive roller can engaged with the object. A first brake is provided to slow down the drive roller and a second brake is provided to keep the lifting apparatus in position. To improve the traction characteristics and in particular to improve the force with which the drive roller can press against the object to be conveyed, the first and second brakes are constructed so as to be controllable.
    • 滚子驱动单元用于在飞机的滚筒输送轨道上输送物体,特别是货物集装箱。 它们包括驱动马达,行星齿轮,其输入端连接到驱动马达,并具有第一和第二齿轮输出。 驱动辊连接到第一齿轮输出以推动物体,并且提升装置连接到第二齿轮输出端,以将驱动辊提升出从驱动辊不接触物体的缩回静止位置到 升高的操作位置,其中驱动辊可以与物体接合。 提供第一制动器以减慢驱动辊,并且提供第二制动器以将提升装置保持在适当位置。 为了提高牵引特性,特别是为了提高驱动辊能够抵靠被输送物体的力,第一和第二制动器被构造为可控制的。