A drive shaft for an aircraft according to an example of the present disclosure includes, among other things, an elongated core extending between a pair of opposed couplings, an energy absorption layer made of a composite comprising metal, the energy absorption layer disposed on the core, and a first composite ballistic layer disposed along a length of the core.
BALLISTIC RESISTANT DRIVE SHAFT
2020-02-27
Patent
Elektronische Ressource
Englisch