marcush,
"BUT: the same is even more true for carbon fibre,isn´t it?And this does not stop F1 making CF wishbones.."
No, the reversing load cycle fatigue limitations of aluminum are not the same for carbon epoxy composites. While it is true that composite structures don't do as well in compression as they do in tension (can't push on a string, right?), they also do not have a defined fatigue life like conventional metal structures. Metal structures fail in fatigue due to fractures that propagate through the section, and these fractures usually originate from the outer surfaces of the metal structure where the stresses are highest. Surface fractures in a composite structure do not propagate through the section in the same manner because the composite structure is a series of discrete fiber layers within a resin matrix. So a fracture in one layer will only propagate as far as the next resin bond line, and will be halted.
The trick to making a composite structure good in compression is to make sure that your fiber alignment is kept as straight as possible under compressive loads. The limit to compressive strength of composites is usually related to how well it can handle buckling within the individual fibers.
Good luck.
Terry