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    • 97. 发明申请
    • MECHANISM FOR GENERATING AN ORBITAL MOTION OR A ROTATION MOTION BY INVERSING A DRIVE DIRECTION OF A DRIVE UNIT
    • 用于通过反转驱动单元的驱动方向产生运动或旋转运动的机构
    • WO2013113849A1
    • 2013-08-08
    • PCT/EP2013/051959
    • 2013-01-31
    • QUANTIFOIL INSTRUMENTS GMBH
    • VESTER, Andreas
    • B01F11/00B04B1/02B06B1/16
    • F16H1/32B01F9/0001B01F9/10B01F11/0014B01F2015/00642F16H1/321F16H3/003F16H2001/323F16H2001/324F16H2001/327F16H2200/00F16H2200/2079
    • A mechanism for switching a sample holder (14, 40) accommodating a fluidic sample (38) between an orbital motion mode for sample mixing, particularly for shaking, and a rotary motion mode for sample separation, particularly for centrifuging, wherein the mechanism comprises a gear element (11) being drivable by a drive unit (42) to move selectively in a first direction (A) or in a second direction (B) being inverse to the first direction (A), an orbital motion generator (2 to 5) configured for generating an orbital motion of the sample holder (14, 40) when being operated in the orbital motion mode, a rotary motion generator (2, 4, 5) configured for generating a rotary motion of the sample holder (14, 40) when being operated in the rotary motion mode, and a one-way clutch arrangement (12, 13) configured for selectively coupling the gear element (11) with the orbital motion generator (2 to 5) to transfer a driving force from the gear element (11) to the orbital motion generator (2 to 5) for generating the orbital motion when the gear element (11) is driven in the first direction (A) and to freewheel when the gear element (11) is driven in the second direction (B) or coupling the gear element (11) with the rotary motion generator (2, 4, 5) to transfer a driving force from the gear element (11) to the rotary motion generator (2, 4, 5) for generating the rotary motion when the gear element (11) is driven in the second direction (B) and to freewheel when the gear element (11) is driven in the first direction (A).
    • 一种用于在用于样品混合的轨道运动模式,特别是用于摇动的轨道运动模式和用于样品分离的旋转运动模式,特别是用于离心分离的旋转运动模式之间切换容纳流体样品(38)的样品架(14,40)的机构,其中所述机构包括 齿轮元件(11)可由驱动单元(42)驱动,以沿与第一方向(A)相反的第一方向(A)或第二方向(B)有选择地移动;轨道运动发生器(2至5) ),被配置为当以轨道运动模式操作时产生样品保持器(14,40)的轨道运动;旋转运动发生器(2,4,5),其被配置为产生样品保持器(14,40)的旋转运动 ),以及单向离合器装置(12,13),其构造成用于选择性地将所述齿轮元件(11)与所述轨道运动发生器(2至5)联接以从所述齿轮传动驱动力 元件(11)到轨道运动发生器(2到5)f 或当沿第一方向(A)驱动齿轮元件(11)时产生轨道运动,并且当齿轮元件(11)沿第二方向(B)被驱动或者将齿轮元件(11)与 旋转运动发生器(2,4,5),用于当齿轮元件(11)被驱动时将驱动力从齿轮元件(11)传递到旋转运动发生器(2,4,5),用于产生旋转运动 第二方向(B),并且当齿轮元件(11)沿第一方向(A)被驱动时飞轮。
    • 98. 发明申请
    • COG-BASED MECHANISM FOR GENERATING AN ORBITAL SHAKING MOTION
    • 基于COG的机制,用于产生一个经典的摇摆运动
    • WO2013113847A1
    • 2013-08-08
    • PCT/EP2013/051957
    • 2013-01-31
    • QUANTIFOIL INSTRUMENTS GMBH
    • VESTER, Andreas
    • B01F11/00B04B1/02B06B1/16
    • B01F11/0097B01F11/0014B01F2015/00642B01F2215/0037
    • A mechanism for generating an orbital motion for mixing, particularly for shaking, a fluidic sample (38) accommodated by a sample holder (14, 40), wherein the mechanism comprises a stationary mounted or lockable first cogwheel (2) having a first through hole (30) and a plurality of first cogs (80) arranged along an outer circumference of the first cogwheel (2), a movably mounted second cogwheel (4) having a second through hole (32) and a plurality of second cogs (82) arranged along an outer circumference of the second cogwheel (4), a drive shaft (3) having a concentric first section (34) and an eccentric second section (36), wherein the first section (34) is guided through the first through hole (30) and the second section (36) is guided through the second through hole (32), and a coupling body (5) having a plurality of third cogs (84) arranged along an inner circumference of the coupling body (5), wherein the coupling body (5) is mounted with the first cogwheel (2) and with the second cogwheel (4) to engage part of the first cogs (80) and part of the second cogs (82) by part of the third cogs (84) to thereby generate the orbital motion of the second cogwheel (4) and a sample holder (14, 40) to be mounted so as to follow a motion of the second cogwheel (4) upon rotating the first section (34) of the drive shaft (3).
    • 一种用于产生用于混合,特别是用于摇动的轨道运动的机构,其由样本保持器(14,40)容纳的流体样本(38),其中所述机构包括固定的安装或可锁定的第一齿轮(2),其具有第一通孔 (30)和沿着所述第一齿轮(2)的外周布置的多个第一齿轮(80),具有第二通孔(32)和多个第二齿轮(82)的可移动安装的第二齿轮(4) 沿着第二齿轮(4)的外周布置有具有同心第一部分(34)和偏心第二部分(36)的驱动轴(3),其中第一部分(34)被引导穿过第一通孔 (30)和第二部分(36)被引导通过第二通孔(32),并且具有沿着联接体(5)的内周布置的多个第三齿轮(84)的联接体(5) 其中所述联接体(5)安装有所述第一齿轮(2)和所述第二齿轮 齿轮(4)通过第三齿轮(84)的一部分接合第一齿轮(80)的一部分和第二齿轮(82)的一部分,从而产生第二齿轮(4)和样品保持器( 14,40),以便在驱动轴(3)的第一部分(34)旋转时遵循第二齿轮(4)的运动。
    • 100. 发明申请
    • A COMBINATION COMPRISING AN AIRCRAFT WING TRAILING EDGE SECTION AND AN ADJUSTMENT BODY
    • 包括航空货运边缘部分和调整机构的组合
    • WO2013102656A1
    • 2013-07-11
    • PCT/EP2013/050096
    • 2013-01-04
    • AIRBUS OPERATIONS GMBHAIRBUS SASEBERLE, AdrianNÜSSLE, Tobias
    • EBERLE, AdrianNÜSSLE, Tobias
    • B64C3/14
    • B64C3/28B64C3/14B64C3/50B64C2003/147B64C2003/148Y02T50/12
    • A combination comprises an aircraft wing trailing edge section (2) and an adjustment body (8). The adjustment body (8) comprises a tapered cross section in a local chord axis direction of the wing trailing edge section (2), a lower adjustment body surface (16) connected to a top surface of the aircraft wing trailing edge section (2) and a back-end surface (12) having a height (h). The adjustment body (8) is positioned such that the back-end surface (12) is flush with the trailing edge (14) of the aircraft wing trailing edge section (2). Attaching the adjustment body (8) onto a top surface of the wing trailing edge section (2) leads to compensation of an offset rolling moment due to unavoidable structural shape deviations of the aircraft and eliminates additional structural reinforcement requirements on the trailing edge compared to edge wedges mounted on the bottom surface of trailing edges. The trailing edge section (2) may comprise a flap.
    • 组合包括飞机机翼后缘部分(2)和调节体(8)。 调节体(8)包括翼缘后缘部(2)的局部弦线方向的锥形横截面,与飞机机翼后缘部(2)的顶面连接的下调整体表面(16) 和具有高度(h)的后端表面(12)。 调整体(8)被定位成使得后端表面(12)与飞机机翼后缘部分(2)的后缘(14)齐平。 将调整体(8)安装在机翼后缘部分(2)的顶表面上,导致由于飞机的不可避免的结构形状偏差而导致的偏移滚动力矩的补偿,并消除了与边缘相比的后缘附加的结构加固要求 安装在后缘底面的楔子。 后缘部分(2)可以包括翼片。