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    • 31. 发明申请
    • SYSTÈME HEXAPODE
    • HEXAPOD系统
    • WO2014076079A1
    • 2014-05-22
    • PCT/EP2013/073618
    • 2013-11-12
    • COMMISSARIAT A L'ENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVES
    • REY, FrédéricALOUANI, Slim
    • B25J17/02B25J18/06B25J9/00
    • B25J9/144B25J9/0057B25J9/0075B25J9/06B25J9/08B25J17/0216B25J19/0091Y10S901/22Y10S901/28
    • La présente invention porte sur un système hexapode (1) comprenant un premier (2) et un deuxième (3) support et six actionneurs linéaires (10a, 10b, 10c, 10d, 10e, 10f), chaque actionneur linéaire présentant deux extrémités articulées respectivement au premier (2) et au deuxième (3) support par une liaison rotule (41, 42, 43, 44), caractérisé en ce qu'il comprend : une structure de reprise d'effort (50) d'une part encastrée sur le premier support (2) et d'autre part couplée au deuxième support (3) par une liaison rotule (51, 52) dont le centre de rotation (60) est situé dans l'épaisseur du deuxième support (3). L'invention porte également sur un robot d'inspection et/ou de réparation caractérisé en ce qu'il comprend un bras poly-articulé équipé d'une pluralité de systèmes hexapodes (1) selon l'invention et dans lequel les systèmes hexapodes (1) sont disposés en série.
    • 本发明涉及包括第一(2)和第二(3)支撑件和六个线性致动器(10a,10b,10c,10d,10e,10f)的六足系统(1),每个线性致动器具有分别在第一 (2)和第二支撑件(3)通过球窝接头(41,42,43,44)支撑,其特征在于,其包括:力传递结构(50),其嵌入在所述第一支撑件(2)上并联接到 第二支撑件(3)通过其中心旋转(60)位于第二支撑件(3)的厚度中的球窝接头(51,52)。 本发明还涉及一种检查和/或修理机器人,其特征在于,其包括具有根据本发明的多个六足体系(1)的多关节臂,并且其中六足体系(1)串联设置。
    • 37. 发明申请
    • ASSEMBLY ROBOT FOR WING
    • 组装机器人WING
    • WO99047415A1
    • 1999-09-23
    • PCT/SE1999/000237
    • 1999-02-22
    • B23P21/00B23P19/00B23P19/04B23Q1/00B23Q1/25B23Q1/44B25J17/02B64C3/00B64F5/00
    • B25J17/0216B23P19/04B23P2700/01B64F5/10Y10S483/901Y10T29/4978Y10T29/5118Y10T29/519Y10T29/5191Y10T483/10Y10T483/15Y10T483/1795
    • A method and a device for assembling an aircraft wing incorporating at least two of the operations drilling, riveting and fitting of anchor nuts (20), where a robot (7) is mobile relative to the wing in a plane parallel to the wing and where the robot (7) is equipped with an arm (9) designed to accommodate a tool holder (15), where the tool holder (15) is primarily equipped with tools for performing a single work operation, whereby the robot is moved so that the robot arm (9) is positioned at the first work position on the aircraft wing unit, where the robot (7) carries out the first work operation at the said first work position, where the robot arm (9) is manoeuvred in the correct order to new work positions on the wing unit within a work area (10) reachable by the robot arm (9), and carries out the first work operation at these new work positions, where a tool holder with tools for performing a second work operation is mounted on the robot arm (9), after which the second work operation is executed by the robot at the work positions and where the robot (7) is moved in relation to the wing to the new work areas (10) and carries out the said steps for each work area (10) or carries out the said first work operation at all work positions in several work areas of the wing unit before the second work operation is performed in the work areas (10) of the wing unit.
    • 一种用于组装飞行器机翼的方法和装置,其结合了锚定螺母(20)的钻孔,铆接和装配中的至少两个操作,其中机器人(7)在平行于机翼的平面中相对于机翼移动,并且其中 机器人(7)配备有设计成容纳工具架(15)的臂(9),其中工具架(15)主要装备有用于执行单个作业操作的工具,由此机器人被移动,使得机器人 机器人臂(9)位于飞机机翼单元上的第一工作位置,机器人(7)在所述第一工作位置执行机器人手臂(9)以正确的顺序操纵的第一工作操作 在机器人臂(9)可到达的工作区域(10)内的机翼单元上的新的工作位置,并且在这些新的工作位置执行第一工作操作,其中具有用于执行第二工作操作的工具的工具架是 安装在机器人手臂(9)上,之后是第二工作操作 离子由机器人在工作位置执行,并且机器人(7)相对于翼移动到新的工作区域(10)并且对于每个工作区域(10)执行所述步骤,或者执行所述 在机翼单元的工作区域(10)中执行在第二工作操作之前在机翼单元的几个工作区域中的所有工作位置的第一工作操作。
    • 40. 发明申请
    • HOISTING DEVICE FOR LOADS
    • 起重载荷
    • WO1993025464A1
    • 1993-12-23
    • PCT/EP1993001367
    • 1993-06-01
    • KRUPP FÖRDERTECHNIK GMBHLÜCKING, ManfredMENDE, Burkhard
    • KRUPP FÖRDERTECHNIK GMBH
    • B66C13/06
    • B66C13/08B25J17/0216B66C13/06
    • In the hoisting device with a horizontally movable structural component (e.g. a crab 1; 1'; 1''), in order to prevent swinging and increase the transfer capacity, the means for grasping the load (e.g. a spreader 4) is suspended via six or more hydraulic adjusting cylinders (11 to 16; 41, ...; 51, ...), the length of which is individually adjustable, which are supported via a movable coupling (21 to 26 and 31 to 36; 59, 60) on the crab (1; 1'; 1'') and on the spreader (4). Here, at least four adjusting cylinders (11 to 16; 41 to 44; 55 to 58) are fitted obliquely. The couplings (21 to 26 and 31 to 36) of the adjusting cylinders are arranged on both the crab (1) and the spreader (4) preferably on a mathematical circle (20 or 30). With a purely vertically acting load it can be of advantage to have eight adjusting cylinders (51 to 54; 55 to 58) of which four (51 to 54) are vertical and lie at the angles of a mathematical rectangle or square in plan view. In the four mathematical planes between each two adjusting cylinders (51/52, 52/53, ...) is arranged an oblique cylinder (55, 56, ...), the inclination of the oblique adjusting cylinders being oppositely directed in each two of the parallel mathematical planes.