发明名称 ABSTÜTZVORRICHTUNG FÜR SATTELAUFLIEGER
摘要 A landing gear for semitrailers includes a two-speed single reduction gear assembly for conversion of crank-handle input turns into vertical travel of the landing gear leg (13). Shifting from a low speed ratio to a high speed ratio is achieved by axial displacement of the input shaft (75). With the input shaft (75) in its low speed position, rotary motion of the shaft (75) is transmitted via a pinion gear (83) formed on the input shaft (75) to a first gear (72) attached to a second shaft (60). Rotation of the second shaft (60) is converted into vertical movement of the leg (13) via a bevel gear assembly (74,34) and a nut-and-screw assembly (25,26). With the input shaft in its high-speed position, the pinion (83) engages interior teeth (84) formed on a high-speed drive gear (90). The exterior teeth (85) of said high-speed drive gear (90) engage a second gear (73), of smaller diameter than the first gear (72), attached to the second shaft (60), resulting in higher speed ratio transmitted to the landing gear leg (13). A simple, compact reduction gear assembly is hereby achieved. <IMAGE> <IMAGE>
申请公布号 AT211086(T) 申请公布日期 2002.01.15
申请号 AT19980102980T 申请日期 1995.03.29
申请人 JOST INTERNATIONAL 发明人 VANDENBERG, ERVIN
分类号 B60S9/06;B60S9/08;B62D53/06;B62D63/08;F16H3/08;F16H63/30;(IPC1-7):B60S9/08 主分类号 B60S9/06
代理机构 代理人
主权项
地址