| 摘要 |
The invention relates to a gyropter having coaxial contrarotating rotating aerofoils, in particular, one having two crown rotors (2,1) that rotate in opposite directions about a pod (6) either provided in the form of a drone or of a manned pod with a machine piloting process involving the control of the angle of attack of the blades by control rings. The safety is advantageously increased by adapted structures, by a multifunctional protective envelop (27), and by a lift system between the crowns (2,1) and the pod (6) with regard to both the radial forces as well as the axial forces, assisting in the optimized control of stresses. The gyropter also comprises electronic controls that are adapted to both model making and drones as well as to manned and/or piloted aircraft. |
