发明名称 Satellite Antenna Adjustment Mechanism
摘要 A satellite antenna mounting apparatus with two spaced parts 20, 22 for adjustment connected through apertures by a shaft 24 which is at least partially threaded, with rotation of the shaft causing the second part 22 to move along a slot and cause relative pivoting of two portions 4, 6 about an axis offset to the adjustment parts. The second part 22 is located with both portions 4, 6 and may protrude through the slot which may be linear and located in the portion 4 in which the first part 20 is located. The parts 20, 22 may comprise a body and a housing with ribs, grooves and recesses to locate the parts and a helical coil in part 22 to allow for rotation. The shaft may have an exterior biasing spring (26, figure 3a) with stops and allow for azimuthal adjustment between portions 4, 6. The position of the satellite dish may be adjustable using the bracket in both horizontal and elevated directions. The satellite aerial bracket reduces movement or backlash when fine tuning alignment.
申请公布号 GB201513800(D0) 申请公布日期 2015.09.16
申请号 GB20150013800 申请日期 2015.08.04
申请人 GLOBAL INVACOM LIMITED 发明人
分类号 主分类号
代理机构 代理人
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