Cost Minimization for the planet carrier by topology optimization
Torsten Bunge, Flender
The objective of the work was to minimize by means of topology
optimization the costs for the planet carrier in the main
gear stage for a planetary gear unit being presently developed.
In this case, the starting point was a reduction in weight.
To this end, the already existing draft was analyzed first.
The boundary conditions to be taken into consideration were
determined. Then, a calculation method for the optimization
of the topology was made up and the optimum determined by
means of different parameters. On the basis of the results,
three planet carrier variants were developed and compared
with the existing draft. An evaluation scheme was worked out
to assess the evaluation criteria according to their relevance.
Because of the technical demands on a planet carrier and
the small space available, it is not possible to reduce the
costs by material savings. If a functional and manufacturing-oriented
planet carrier is designed, it becomes heavier than the reference
model. But it was possible to derive constructional rules
from the optimization which can be easily realized without
great design expenditure and amount of time required.
Although in this concrete case topology optimization did
not lead us to our goal it is nevertheless correct and purposeful
to use this tool for the task of cost reduction. As the calculation
results show, the design engineer gets clear indications of
what the design of the component should look like in the ideal
case to satisfy the determined boundary conditions. It may,
however, not excite the impression that this technology would
make designing unnecessary. Although manufacturing restrictions
such as the direction of extraction in the foundry or the
necessity of a repetitive pattern have been implemented to
a small extent, a design proposal achieved by optimization
cannot be taken on without expensive and time consuming rework.
It can serve for orientation only.
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