| 摘要 |
The purpose of this proposed solution is the increase of the carrying capacity of epicyclical gears under the reduction of operating expenses. The introduced purpose is achieved by a more harmonious distribution of a force from the sun gear on satellites being individually spring-loaded in the satellite-gear carrier. The power of each satellite is carried over to the carrier through elastic bushings embedded in the satellite pin hollow supports placed in openings of the satellite pin wall.<IMAGE>
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