We are looking for assistance with Solidworks modeling and structural design of UAV components. The first part we are looking into is an undercarriage leg which can deform and absorb load without structural failure. The first kind of structure that we are imagining is similar to a leaf spring. Typical loads are in the order of 11kg static load, but with peak loads in the order of 100kg without failure. A light weight, simple to manufacture structure is important.
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hello , i'm a mechanical engineer have a good experience with mechanical design. i designed a geer box once before . i have a good experience with solidworks so i hope i can help you.