发明名称 GEAR UNIT, PARTICULARLY FOR USE IN A HELICOPTER
摘要 <p>In a high-loaded, light-weight, compact, multi-stage gear transmission unit with at least one stage with non-parallel shafts, and a transmission ratio between approximately 70 and 150, like a helicopter transmission, said angle transmission generally forms the weakest link. By adoption of a face gear/cylindrical pinion-stage instead of the commonly used bevelled-stage, not only a more reliable drive is possible, but its efficiency is higher, due to less friction, its size is smaller, its adjustment is simpler such that straight forward replacement becomes possible, and-not in the least-the transmission ratio of said angle drive tends to high ratios in contrast to known bevelled-drives which tend to low ratios. In many cases one or even more stages less become possible, providing a further important reduction in weight and size.</p>
申请公布号 EP0234058(B1) 申请公布日期 1989.05.17
申请号 EP19860202218 申请日期 1986.12.09
申请人 DAF SPECIAL PRODUCTS 发明人 LUIJTEN, WALTHERUS J. T. H.
分类号 B64C27/12;F16H1/12;F16H37/04 主分类号 B64C27/12
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