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An aircraft includes two rotors for rotation about a non-rotating rotor mast. The rotors are driven by permanent and/or electromagnets positioned on each of the rotors. A rotor mast joint connecting the rotor mast to a fuselage or wing of the aircraft permits the rotor mast to tilt relative to the f

An aircraft includes two rotors for rotation about a non-rotating rotor mast. The rotors are driven by permanent and/or electromagnets positioned on each of the rotors. A rotor mast joint connecting the rotor mast to a fuselage or wing of the aircraft permits the rotor mast to tilt relative to the fuselage or wing in at least one plane.

대표청구항 ▼

1. An aircraft including: a fuselage or wing;a rotor mast;first and second rotors spaced axially along; and rotatably connected to the rotor mast;at least one of: (i) an electro magnet, (ii) a permanent magnet; or (iii) an electrically conductive ring, on the second rotor; anda rotor mast joint conn

1. An aircraft including: a fuselage or wing;a rotor mast;first and second rotors spaced axially along; and rotatably connected to the rotor mast;at least one of: (i) an electro magnet, (ii) a permanent magnet; or (iii) an electrically conductive ring, on the second rotor; anda rotor mast joint connecting the rotor mast to the fuselage or wing, wherein the rotor mast joint, in use, permits the rotor mast to tilt relative to the fuselage or wing in at least one plane. 2. An aircraft according to claim 1, further including an electro magnet on the first rotor. 3. An aircraft according to claim 2, wherein the second rotor includes the electrically conductive ring arranged in relation to the electro magnet on the first rotor to provide a linear electric motor. 4. An aircraft according to claim 2, wherein each rotor includes at least one rotor blade with an aerofoil cross section. 5. An aircraft according to claim 4, wherein at least one of the permanent magnet, electro magnet, and electrically conductive ring is located within the inner half-radius of the second rotor. 6. An aircraft according to claim 5, wherein the rotor mast joint permits the rotor mast to tilt in a vertical plane that runs along a major axis of the aircraft. 7. An aircraft according to claim 5, wherein the rotor mast joint permits the rotor mast to tilt: (i) in a vertical plane that runs along a major axis of the aircraft; and (ii) a vertical plane that runs along a minor axis of the aircraft. 8. An aircraft according to claim 7, wherein the rotor mast joint permits relative angular movement between the rotor mast and fuselage or wing greater than 0 degrees and less than 25 degrees. 9. An aircraft according to claim 7, wherein the rotor mast joint permits relative angular movement between the rotor mast and fuselage or wing greater than 2 degrees and less than 25 degrees. 10. An aircraft according to claim 9, wherein a parachute is located on the rotor mast above the rotors. 11. An aircraft according to claim 7, wherein the rotor mast joint permits relative angular movement between the rotor mast and fuselage or wing greater than 4 degrees and less than 25 degrees. 12. An aircraft according to claim 11, wherein the aircraft is a helicopter or a toy helicopter. 13. An aircraft according to claim 12 including a mechanical generator for generating electricity to power rotation of the rotors. 14. An aircraft including: a fuselage or wing;a rotor mast;a rotor rotatably connected to the rotor mast;at least one of permanent magnets, electro magnets, and an electrically conductive ring on the rotor;a stator fixed against rotation on the rotor mast;at least one of permanent magnets, electro magnets, and an electrically conductive ring on the stator; anda rotor mast joint connecting the rotor mast to the fuselage or wing, wherein the rotor mast joint, in use, permits the rotor mast to tilt relative to the fuselage or wing in at least one plane. 15. An aircraft according to claim 14, wherein one of the rotor or stator includes electro magnets and the other of the rotor or stator includes the electrically conductive ring arranged in relation to the electro magnets to provide a linear electric motor. 16. An aircraft according to claim 15, wherein the rotor mast joint permits the rotor mast to tilt in a vertical plane that runs along a major axis of the aircraft. 17. An aircraft according to claim 16, wherein the rotor mast joint permits the rotor mast to tilt: (i) in a vertical plane that runs along the major axis of the aircraft; and (ii) a vertical plane that runs along a minor axis of the aircraft. 18. An aircraft according to claim 17, wherein the rotor mast joint permits relative angular movement between the rotor mast and fuselage or wing greater than 0 degrees and less than 25 degrees. 19. An aircraft according to claim 17, wherein the rotor mast joint permits relative angular movement between the rotor mast and fuselage or wing greater than 2 degrees and less than 25 degrees. 20. An aircraft according to claim 19, wherein a parachute is located on the rotor mast above the rotor. 21. An aircraft according to claim 17, wherein the rotor mast joint permits relative angular movement between the rotor mast and fuselage or wing greater than 4 degrees and less than 25 degrees. 22. An aircraft according to claim 20, wherein the aircraft is a helicopter or a toy helicopter.