Helicopter with control by displacement of its center gravity
OwnerFranz Weinhartinventor
Life of this patent
Estimating the term…
Abstract
In the case of a helicopter comprising a rotor system (3) with rotor blades (6 and 6′) held on a fuselage (2) and at least one rotor shaft (5 and 5′) and furthermore comprising a drive system (4) for causing rotation of the rotor system (3), the rotor system (3) together with the drive system (4) is able to be slid in the longitudinal direction of the fuselage (2) and to be pivoted around a pivot axis extending along the fuselage (2).
Claims6
A helicopter comprising a rotor system with rotor blades held on a fuselage and at least one rotor shaft and furthermore comprising a drive system for causing rotation of the rotor system wherein the rotor system together with the drive system is able to be slid in the longitudinal direction of the fuselage and to be pivoted around a pivot axis extending along the fuselage.
Dependencies are inferred from the claim text.