TILT-WING AIRCRAFT

• US 20130099065A1
• Filed: 11/13/2012
• Published: 04/25/2013
• Est. Priority Date: 05/19/2010
• Status: Abandoned Application

• Current Assignee: EADS Deutschland GmbH (Airbus SE)
• Original Assignee: EADS Deutschland GmbH (Airbus SE)
• Inventors: Stuhlberger, Johannes
• Application Number:
  US13/675,646
• Publication Number:
  US 20130099065A1
• Time in Patent Office: Days
• US Class Current: 244/7.C
• CPC Class Codes: B64C 2027/8236 including pusher propellers
• CPC Class Codes: B64C 27/22 Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
• CPC Class Codes: B64C 29/0033 the propellers being tiltable relative to the fuselage
• CPC Class Codes: B64D 27/026 comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine Hybrid electric aircraft B64D27/33
• CPC Class Codes: B64D 27/24 using steam or spring force jet aircraft B64D27/16
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 30/297 Tilting rotors
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/30 Supply or distribution of electrical power
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10S 903/902 Prime movers comprising electrical and internal combustion motors

Abstract

A tilt-wing aircraft is provided. The tilt-wing aircraft includes a tail drive and control unit. The control unit is configured to generate a forward thrust. The control unit can also generate an upwardly or downwardly directed thrust component and/or a laterally directed thrust component in hover flight and in climb flight of the aircraft.

Claims

1. A tilt-wing aircraft comprising:

a tail drive; and

a control unit that generates a forward thrust, and generates at least one of an upwardly, downwardly and laterally directed thrust component in hover flight and in climb flight of the aircraft.

2. The tilt-wing aircraft according to claim 1, wherein the tail drive and control unit further comprises a propeller creating an air flow against an empennage of the aircraft.

3. The tilt-wing aircraft according to claim 1, wherein the tail drive and control unit further comprises a sheathed tail propeller.

4. The tilt-wing aircraft according to claim 3, wherein the sheathed tail propeller generates an upwardly or downwardly directed thrust component and a laterally directed thrust component.

5. The tilt-wing aircraft according to claim 2, wherein a number of 2 n propellers is provided for the tilt wing, where n is a positive integer.

6. The tilt-wing aircraft according to any one of claim 5, further comprising a hybrid drive which, for each propeller, includes a respective electric motor that drives the propeller.

7. The tilt-wing aircraft according to claim 6, wherein the hybrid drive further comprises at least one energy generating module that includes an internal combustion engine and a generator to generate electrical energy for at least one of the respective electric motors.

8. The tilt-wing aircraft according to claim 7, wherein at least one further energy generating module is provided.

9. The tilt-wing aircraft according to claim 7, wherein the hybrid drive further comprises a storage unit for electrical energy.

10. The tilt-wing aircraft according to claim 7, wherein the at least one energy generating module and the further energy generating module are similar.

11. The tilt-wing aircraft according to claim 8, wherein the further energy generating module is configured as a fuel cell unit.

12. A method for operating a tilt-wing aircraft, comprising:

generating electrical energy by at least one energy generating module; and

distributing the electrical energy onto a plurality of electric motors which drive a plurality of propellers to create at least one of an upwardly, downwardly and laterally directed thrust component in hover flight and in climb flight of the aircraft, depending on operating requirements.

13. The method according to claim 12, wherein the plurality of propellers includes at least one tail propeller and the method further comprises:

in cruise flight, distributing most of the electrical energy to one of the plurality of electric motors to drives the at least one tail propeller.

14. The method according to claim 12, wherein the plurality of propellers includes at least one sheathed tail propeller, and the method further comprises:

generates an upwardly or downwardly directed thrust component and a laterally directed thrust component with the at least one sheathed tail propeller.

15. The method according to claim 12, wherein generating electrical energy by the at least one energy generating module further comprises:

generating electrical energy with an internal combustion engine and a generator.

16. The method according to claim 12, wherein generating electrical energy by the at least one energy generating module further comprises:

generating electrical energy with a fuel cell.