公开(公告)号：US1804105A

公开(公告)日：1931-05-05

申请号：US26702028

申请日：1928-04-03

申请人： WILHELM MARTENS

发明人： WILHELM MARTENS

IPC分类号： G02B25/02

CPC分类号： G02B25/02

公开(公告)号：US06200223B1

公开(公告)日：2001-03-13

申请号：US09095444

申请日：1998-06-10

申请人： Wilhelm Martens

发明人： Wilhelm Martens

IPC分类号： F16D352

CPC分类号： F16D3/78 ,  F16B2200/506 ,  F16D3/79 ,  Y10T403/45

摘要： A flexible coupling for flexibly connecting two rotary drive shafts includes a first coupling flange connected to the first shaft, a second coupling flange connected to the second shaft, a flexible disk arranged between the two coupling flanges, and four connector bolts that respectively connect the two flanges to the flexible disk. A first pair of the bolts is securely connected to the first flange and to the flexible disk, while passing with free play through a clearance hole in the second flange. A second pair of the bolts is securely connected to the second flange and to the flexible disk, while passing with free play through a clearance hole in the first flange. In ordinary operation, the connection and force transmission between the coupling flanges is carried out through the flexible disk. If the flexible disk or one or more of the connector bolts fails, then the connection and force transmission between the two coupling flanges will be carried out directly through the connector bolts in a fail-safe operating mode. The flexible coupling is especially adapted for use in a transmission system for transmitting drive power from a central drive unit to the high lift flaps and slats of an aircraft.

摘要翻译： 用于柔性连接两个旋转驱动轴的柔性联接器包括连接到第一轴的第一联接凸缘，连接到第二轴的第二联接凸缘，布置在两个联接凸缘之间的柔性圆盘，以及分别连接两个连接凸缘的四个连接器螺栓 法兰到柔性盘。 第一对螺栓牢固地连接到第一凸缘和柔性盘，同时通过第二凸缘中的间隙自由地穿过。 第二对螺栓与第二凸缘和柔性盘牢固连接，同时自由地穿过第一凸缘中的间隙。 在通常的操作中，连接法兰之间的连接和力传递通过软盘进行。 如果软盘或一个或多个连接器螺栓故障，则两个联轴器法兰之间的连接和力传递将通过连接器螺栓在故障安全操作模式下直接执行。 柔性联轴器特别适用于用于将驱动力从中央驱动单元传送到飞行器的高提升襟翼和板条的传动系统中。

公开(公告)号：US4915327A

公开(公告)日：1990-04-10

申请号：US213335

申请日：1988-06-30

申请人： Wilfried Ellmers ,  Wilhelm Martens

发明人： Wilfried Ellmers ,  Wilhelm Martens

IPC分类号： B64C9/24 ,  B64C13/30

CPC分类号： B64C13/30 ,  B64C9/24

摘要： An actuation device for a slat, a rail for guiding and moving the slat into and out of an aircraft wing has the slat pivoted on the rail in a particular point (8); a thrust rod has one end hinged to the slat and a drive crank is connected to a second end of the thrust rod; a lever assembly connects the rail additionally to the slat at points on the rail and the slat different from the particular point and for pivoting and steering the slat relative to the particular point, for holding the rear end of the slat against the wing in a first protraction range and opening a gap upon further protraction.

摘要翻译： 用于板条的致动装置，用于引导和移动板条进入和离开飞机机翼的轨道具有在特定点（8）上在轨道上枢转的板条; 推力杆的一端铰接到板条上，驱动曲柄连接到推杆的第二端; 杠杆组件将轨道附加到轨道上的板条和不同于特定点的板条上，并且用于相对于特定点枢转和转向板条，用于将板条的后端以第一 延伸范围，并在进一步延伸时打开空白。

公开(公告)号：US4720066A

公开(公告)日：1988-01-19

申请号：US900507

申请日：1986-08-26

申请人： Juergen Renken ,  Wilhelm Martens

发明人： Juergen Renken ,  Wilhelm Martens

IPC分类号： B64C9/12 ,  B64C13/26 ,  B64C13/50

CPC分类号： B64C9/12 ,  B64C13/26 ,  B64C13/50

摘要： A flap arrangement for an aircraft wing having along its trailing edge independently actuated high lift flap and spoiler. During cruising the flap is used for camber line curvature control while the spoiler is controlled in a follow up configuration such that a gap between the spoiler and the high lift flap does not form.

摘要翻译： 一种用于飞机机翼的翼片装置，其沿着其后缘独立地致动高升降挡板和扰流板。 在巡航期间，翼片用于弯曲线曲率控制，而扰流板被控制在跟随构造中，使得扰流板和高升降挡板之间的间隙不会形成。

公开(公告)号：US5339924A

公开(公告)日：1994-08-23

申请号：US44220

申请日：1993-04-07

申请人： Wilhelm Martens

发明人： Wilhelm Martens

IPC分类号： F16N21/00 ,  F16N27/00 ,  F16N11/10

CPC分类号： F16N27/00 ,  F16N21/00

摘要： A dosing device for a lubricating mechanism is constructed for discharging a measured volume of lubricant into a component to be lubricated, such as a rotary gear box in an aircraft. For this purpose the dosing device has a housing with a defined volume in which a piston is movable in an axial direction to define two chambers. The end walls of the housing are connected through quick coupling connectors to a lubricant supply and to the component to be lubricated. The device operates in such a way that the filling of one chamber with lubricant under pressure pushes the piston, and thus the lubricant in the other chamber, out into the component to be lubricated. Thus, always a precisely measured volume of lubricant is discharged from one chamber while the same volume is being filled into the other chamber and vice versa. A coupling adapter may be used for a quick reversal.

摘要翻译： 用于润滑机构的计量装置被构造用于将测量体积的润滑剂排放到待润滑的部件中，例如飞行器中的旋转齿轮箱。 为此，配量装置具有具有限定体积的壳体，其中活塞可沿轴向移动以限定两个腔室。 壳体的端壁通过快速联接连接器连接到润滑剂供应和要润滑的部件上。 该装置以这样的方式工作，即在一个室内用润滑剂在一定压力下填充一个活塞，从而将另一个室中的润滑剂推出到待润滑的部件中。 因此，始终将精确测量的润滑剂体积从一个室排出，同时将相同的体积填充到另一个室中，反之亦然。 耦合适配器可用于快速反转。

公开(公告)号：US5566910A

公开(公告)日：1996-10-22

申请号：US322055

申请日：1994-10-12

申请人： Thomas Diekmann ,  Norbert Geyer ,  Wilhelm Martens

发明人： Thomas Diekmann ,  Norbert Geyer ,  Wilhelm Martens

IPC分类号： B64C9/16 ,  B64C13/28

CPC分类号： B64C9/16 ,  B64C13/28

摘要： A wing gap closure flap is positioned in an aircraft wing so that a gap between the wing structure and the leading edge of a landing flap can be closed during normal cruising positions of the landing flap and opened when the landing flap is in a starting position or in a landing position. The gap is formed on the underside of the aircraft wing and the gap closure flap is operated by a positioning shaft which itself is driven through a drive lever linkage by the drive shaft for the landing flap. The wing gap closure flap is connected through a lever mechanism to the positioning shaft which is preferably divided into shaft sections where a plurality of wing gap closure flaps are used. Each shaft section is driven by the landing flap drive shaft. A defined motion of the wing gap closure flap or flaps is achieved in that the positioning of the wing gap closure flaps is synchronized in a limited angular range with the positioning of the landing flap by the cooperation of the respective drive mechanisms.

摘要翻译： 机翼间隙关闭翼片定位在飞机机翼中，使得在着陆翼的正常巡航位置期间，机翼结构和着陆翼的前缘之间的间隙可以关闭，并且当着陆翼处于起始位置时打开， 在着陆位置。 间隙形成在飞行器机翼的下侧，并且间隙闭合翼片由定位轴操作，定位轴本身通过用于着陆挡板的驱动轴通过驱动杆连杆驱动。 机翼间隙闭合翼片通过杠杆机构连接到定位轴，定位轴优选地分成轴部分，其中使用多个机翼间隙闭合翼片。 每个轴段由着陆挡板驱动轴驱动。 实现翼间隙闭合翼片或翼片的限定运动的目的在于，通过各个驱动机构的配合，机翼间隙闭合翼片的定位在有限角度范围内与着陆翼片的定位同步。

公开(公告)号：US4437631A

公开(公告)日：1984-03-20

申请号：US141008

申请日：1980-04-17

申请人： Wilhelm Martens ,  Homayoun Dilmaghani

发明人： Wilhelm Martens ,  Homayoun Dilmaghani

IPC分类号： B64C9/24 ,  B64C3/50

CPC分类号： B64C9/24

摘要： A leading edge slat of an aircraft wing is connected to the ends of two rods each of them being linked to a crank arm which, in turn, is swung over a particular angular range by means of a planetary gear being driven by a common shaft. Arcuate guide rails on the slat run in rolls which are journalled on the wing case.

摘要翻译： 飞机机翼的前缘板条连接到两个杆的端部，每个杆的端部连接到曲柄臂，曲柄臂通过由公共轴驱动的行星齿轮在特定的角度范围内摆动。 板条上的弧形导轨在卷轴上运行，这些导轨位于翼壳上。