公开(公告)号：US20130327887A1

公开(公告)日：2013-12-12

申请号：US13684882

申请日：2012-11-26

申请人： Werner DYCKRUP ,  Wilfried ELLMERS

发明人： Werner DYCKRUP ,  Wilfried ELLMERS

IPC分类号： B64C13/28

CPC分类号： B64C13/28 ,  B64C9/02 ,  B64C9/16 ,  B64C13/42 ,  B64D2045/001 ,  Y02T50/44

摘要： The invention concerns a device for a adjustable flap adjustably mounted on a main wing surface of an aeroplane wing, in particular, a landing flap, with at least one adjustment unit for purposes of adjustment of the adjustable flap, which has an actuator arranged, or that can be arranged, on the main wing surface, and has a kinematic adjustment mechanism running between the actuator and the adjustable flap, wherein the adjustable flap is mechanically coupled with the actuator via the kinematic adjustment mechanism. At least one damping unit for purposes of damping a dynamic loading effected by the adjustable flap on the adjustment unit, which can occur as a result of a critical malfunction event occurring in the region of the adjustable flap, is arranged, or can be arranged, between the main wing surface and the adjustable flap.

摘要翻译： 本发明涉及一种用于可调整的翼片的装置，其可调节地安装在飞机机翼的主翼表面上，特别是着陆挡板上，具有至少一个调节单元，用于调整可调节翼片，调节翼片具有执行器，或者 其可以布置在主翼表面上，并且具有在致动器和可调节翼片之间运行的运动调节机构，其中可调节翼片通过运动调节机构与致动器机械联接。 至少一个阻尼单元用于阻尼由调节单元上的可调节挡板影响的动态载荷，其可能由于在可调节翼片的区域中发生的临界故障事件而发生，或者可以布置， 主翼面与可调翼片之间。

公开(公告)号：US5360303A

公开(公告)日：1994-11-01

申请号：US85757

申请日：1993-06-30

申请人： Guenter Behrens ,  Wilfried Ellmers

发明人： Guenter Behrens ,  Wilfried Ellmers

IPC分类号： F16B39/08 ,  F16B39/10

CPC分类号： F16B39/08 ,  Y10S411/945

摘要： A nut lock or locking cap secures a nut on a bolt so that the nut cannot loosen itself and so that the nut cannot fall off the bolt. For this purpose the nut lock has a first ring section that at least partially surrounds the bolt and a second ring section that at least partially surrounds the nut. The two ring sections are interconnected by a radially extending flange, whereby the first ring section has a smaller diameter than the diameter of the second ring section. The first ring section has at least one through-hole that can be aligned with a cross-bore in the bolt for the insertion of a locking pin. The second ring section has radially inwardly facing profiled surfaces that enter into a form-locking, force-transmitting connection with the outer profile of the nut.

摘要翻译： 螺母锁或锁盖将螺母固定在螺栓上，使得螺母不能松动，从而螺母不能从螺栓上脱落。 为此，螺母锁具有至少部分地围绕螺栓的第一环部分和至少部分地围绕螺母的第二环部分。 两个环形部分通过径向延伸的凸缘相互连接，由此第一环​​形部分的直径小于第二环形部分的直径。 第一环段具有至少一个通孔，该通孔可以与螺栓中的横向孔对齐以插入锁定销。 第二环形部分具有径向向内的成型表面，其进入与螺母的外部轮廓的形式锁定的力传递连接。

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。