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    • 72. 发明授权
    • PIVOT JOINT FOR LOADER LINKAGES AND THE LIKE
    • GLIED MIT ZAPFENFÜRLADERVERBINDUNGEN UNDÄHNLICHE。
    • EP0448648B1
    • 1995-04-05
    • EP90902026.5
    • 1990-01-16
    • CATERPILLAR INC.
    • REINSMA, Harold, L.BORN, W., Stanley
    • F16C11/02
    • E02F9/006F16C11/02F16C11/045F16C2350/26Y10T403/16Y10T403/32926Y10T403/52
    • A maintenance-free pivot joint (10) is disclosed for mounting a first member (16) of a loader linkage (12) to a second member (18) thereof. The first member (16) is provided with a clevis (62) having a pair of brackets (64, 66). The pivot joint (10) includes a pivot pin (60) which is pivotally mounted within the second loader linkage member (16). A first end collar (64) is fixedly secured to one end of the pivot pin (60) of the joint (10) and is slidably mounted to a first one of the pair of brackets (64). Conversely, a second end collar (74) is slidably mounted on the other end of the pin (60) and fixedly secured to a second of the brackets (66), but at a preselectable axial position relative to the second member (16). The positioning of the second end collar (74) at the preselected position allows the joint (10) to accommodate lateral misalignment between the first and second members (16, 18) of the linkage (12), while maintaining a closely spaced lateral relationship therebetween to eliminate end play and facilitate good sealability.
    • 公开了一种免维护的枢转接头,用于将装载机连杆的第一构件安装到其第二构件。 第一个成员具有一个具有一对支架的U形夹。 枢转接头包括可枢转地安装在第二加载器连杆构件内的枢轴销。 第一端环固定地固定在接头的枢转销的一端,并可滑动地安装在一对支架中的第一个。 相反地​​,第二端环可滑动地安装在销的另一端上并且固定地固定到第二托架,但是相对于第二构件处于可选择的轴向位置。 第二端部轴环在预定位置的定位允许接头适应连杆的第一和第二构件之间的横向偏移,同时保持其间的紧密间隔的横向关系,以消除端部冲击并促进良好的密封性。
    • 74. 发明公开
    • Main lever for a rotary dobby operating at high speed
    • Haupthebelfürschnell laufende Drehschaftmaschinen。
    • EP0393750A2
    • 1990-10-24
    • EP90200872.1
    • 1990-04-10
    • NUOVOPIGNONE INDUSTRIE MECCANICHE E FONDERIA S.p.A.
    • Vinciguerra, Costantino
    • D03C1/14F16C11/02
    • F16C11/04D03C1/144F16C2340/00Y10T74/18184Y10T74/20582
    • A main lever for a high-speed rotary dobby, consisting of two opposing sidepieces in which, by pressing or milling, there are formed two corresponding opposing frusto-conically flared holes for the removable main pin for coupling the lever to the dobby crank arm, and two inner annular recesses concentric with said holes for housing a bearing of increased axial length, said sidepieces being joined together without welding by a special annular spacer hub acting as the fulcrum for the lever and, at the free end of the curved guide for the slider which adjusts the travel of the heddle frames, by a spacing and vibration-damping block, said slider passing between the two sidepieces in the curved guide zone and being locked in position by a special locking device. Lever modifications and special reinforcements are also provided.
    • 用于高速旋转多臂机的主杆,由两个相对的侧面组成,其中通过压制或铣削形成两个对应的相对的截头圆锥形孔,用于可移动主销,用于将杠杆连接到多臂曲柄臂, 以及与所述孔同心的两个内环形凹槽,用于容纳轴向长度增加的轴承,所述侧面连接在一起,而不用用作杠杆支点的特殊环形隔离轮毂进行焊接,并且在弯曲导向件的自由端 滑块,其通过间隔和减振块调整综框的行程,所述滑块在弯曲导向区域中通过两个侧面之间,并通过特殊的锁定装置锁定在适当位置。 还提供杠杆修改和特殊增援。
    • 77. 发明公开
    • PINTLE PIN ASSEMBLY MECHANISM
    • EP4122820A1
    • 2023-01-25
    • EP21187379.9
    • 2021-07-23
    • Safran Landing Systems UK Ltd
    • BENNETT, Ian Robert
    • B64C25/08F16C11/02F16C11/04
    • The invention provides an attachment assembly for an aircraft joint, and in particular for a strut mounting joint. The attachment assembly comprises a tubular structure having a central axis (PA) and at least one open end. The attachment assembly further comprises at least one mounting pin (560a, 560b) arranged at least partially within the at least one open end of the tubular structure and moveable along the central axis between a retracted position and an extended position. In the extended position, a portion of the at least one mounting pin protrudes from the at least one open end of the tubular structure for engagement with a lug and in the retracted position the at least one mounting pin is withdrawn into the tubular structure for disengagement with the lug. The attachment assembly further comprises a retraction mechanism disposed within the tubular structure and coupled to the at least one mounting pin, the retraction mechanism arranged to convert a rotary input motion into linear motion of the at least one mounting pin along the central axis to drive the at least one mounting pin between the extended position and the retracted position.