会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 39. 发明公开
    • Landing gear door damping mechanism for aircraft
    • Flugrug的Fahrwerkstürdämpfungsmechanismus
    • EP2644500A1
    • 2013-10-02
    • EP13163772.0
    • 2012-03-27
    • AIRBUS OPERATIONS (S.A.S)
    • Veerabadran, Karounen
    • B64C25/16F16F15/00
    • B64C1/1407B64C25/16E05B77/00
    • The invention provides a damping mechanism which comprises a damper (27); and a coupling mechanism. The coupling mechanism comprises a coupling member (25) which is pivotally attached to the damper and has a pivot bearing (26) for pivotally connecting the coupling member to a structure when in use; anda fitting (22,40) which can be engaged with the coupling member to couple the fitting with the damper and disengaged with the coupling member to decouple the fitting from the damper. More, the coupling member (25) has a pair of parallel planar faces which taper outwardly from the pivot bearing(26) to a convex curved edge (34), an upper edge (35) and a lower edge (36); and a first (37) and a second recess (38) formed in the convex curved edge (34), a rib (39) between the first and the second recesses and, a third recess (36a) formed in the lower edge (36)
    • 本发明提供一种阻尼机构,其包括阻尼器(27); 和耦合机构。 联接机构包括枢转地附接到阻尼器并具有枢转轴承(26)的联接构件(25),用于在使用时将联接构件枢转地连接到结构; 和安装件(22,40),其可以与联接构件接合以将配件与阻尼器联接,并与联接构件脱离接合以使配件与阻尼器分离。 更重要的是,联接构件(25)具有一对平行的平面,其从枢转轴承(26)向外渐缩成凸曲线边缘(34),上边缘(35)和下边缘(36)。 以及形成在所述凸曲线边缘(34)中的第一凹部(37)和第二凹部(38),所述第一凹部和所述第二凹部之间形成有肋(39),所述第三凹部(36a)形成在所述下边缘 )