Patent ID: 9567067
Date: 2017-02-14
CPC Classifications: B64C,B64D

Claim:
1. An aircraft comprising: a fuselage, a wing, at least one jet engine on one side of the fuselage, the jet engine is housed in a nacelle attached to the wing, and a main landing gear; wherein the wing comprises a load-bearing structure extending in a span wise direction and the main landing gear comprises at least a landing gear at one side of the wing having one or more wheels coupled to a driving device arranged for moving the landing gear from a stowed position to a deployed position and vice versa, wherein the nacelle includes a well aligned with the jet engine such that the well and jet engine both intersect a line extending in a span wise direction of the wing and the well is configured as a housing space for the one or more wheels of the landing gear in its stowed position, and said driving device comprises a strut attached by one end to the load-bearing structure of the wing in a rotatory manner and by the other end to the one or more wheels.