Aircraft and method for operating an aircraft

• US 6,254,032 B1
• Filed: 12/30/1999
• Issued: 07/03/2001
• Est. Priority Date: 10/26/1999
• Status: Expired due to Term

• Current Assignee: Franz Bucher
• Original Assignee: Franz Bucher
• Inventors: Bucher, Franz
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US09/475,325
• Time in Patent Office: 551 Days
• Field of Search: 244/12.2, 244/23.C, 244/56, 244/66, 244/12.4, 244/23.A
• US Class Current: 244/12.2
• CPC Class Codes: B64C 29/0033 the propellers being tiltable relative to the fuselage
• CPC Class Codes: B64D 27/24 using steam or spring force jet aircraft B64D27/16
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

The aircraft comprises a central cabin, which is located in the center of a circular wing. Several pivotal electric drive units are arranged in a gap between the central cabin and the circular ring. In hover flight, the drive units are pivoted to generate a lift. When the aircraft goes into cruise flight, the drive units are pivoted to generate a forward thrust. Attitude and movements of the aircraft can be controlled by individual or common adjustment of the thrust and pivot angle of the drive units. Due to its simple design, the aircraft is economic and safe in operation. Still it has a high payload for its size.

Claims

1. An aircraft comprising

a centrally located cabin,

a wing extending around said cabin, said wing having an outer edge and defining at least one opening between said outer edge and said cabin,

at least one generator for generating electrical power,

at least one engine for driving said generator,

a plurality of electrically driven, individually pivotal drive units mounted in said at least one opening for generating lift and forward thrust, wherein said drive units can be pivoted from a vertical position to a horizontal position, and

means for adjusting a power of at least part of said drive units individually,

wherein in said vertical position said drive units generate a lift sufficient for lifting the weight of said aircraft, and wherein in said horizontal position said pivotal drive units generate a forward thrust while said lift is generated aerodynamically by said cabin and said wing.

2. The aircraft of claim 1 wherein each of said pivotal drive units is pivotal about a pivoting axis, wherein said pivotal axes are parallel to each other and perpendicular to a forward direction of said aircraft.

3. The aircraft of claim 1 wherein said drive units comprise ducted fans.

4. The aircraft of claim 1 wherein said drive units are arranged in a circle.

5. The aircraft of claim 1 comprising at least five drive units.

6. The aircraft of claim 1 comprising at least six drive units.

7. The aircraft of claim 1 wherein each drive unit comprises a fan.

8. The aircraft of claim 1 wherein all said drive units are substantially identical.

9. The aircraft of claim 1 wherein each of said drive units comprises an electric motor.

10. A method for operating an aircraft, said aircraft comprising a centrally located cabin, a wing extending around said cabin, said wing having an outer edge and defining at least one opening between said outer edge and said cabin, at least one generator for generating electrical energy, at least one engine for driving said generator, and a plurality of electrically driven, pivotal drive units for generating lift and forward thrust, wherein each drive unit has a thrust axis, said method comprising the steps of

adjusting said thrust axes of said drive units downwards through said at least one opening for generating a lift for lifting the weight of said aircraft for hover flight and

adjusting said thrust axes of said drive units horizontally for generating a forward thrust for cruise flight, wherein in said cruise flight said lift is generated by an aerodynamic profile of said aircraft,

wherein an attitude of said aircraft is controlled by tilting said drive units and adjusting a thrust of said drive units.

11. An aircraft comprising

a centrally located cabin,

a wing extending around said cabin, said wing having an outer edge and having an inner edge spaced apart from said cabin to define a gap between said inner edge and said cabin,

at least one generator for generating electrical power,

at least one engine for driving said generator, and

a plurality of electrically driven pivotal drive units arranged in said gap between said cabin and said inner edge that can be oriented vertically for generating lift or horizontally for generating forward thrust.

12. The aircraft of claim 11 wherein at least one of said drive units can be pivoted individually.

13. The aircraft of claim 11 wherein said wing is circular.

14. The aircraft of claim 11 comprising a substantially circular gap between said cabin and said wing, wherein said drive units are arranged in said gap.

15. The aircraft of claim 11 wherein at least one of said drive units can be pivoted, wherein a thrust axis of said pivotal drive unit can be pivoted to a horizontal position where said drive unit generates a forward thrust, wherein in said horizontal position said thrust axes are located above a central plane of said wing.

16. The aircraft of claim 11 comprising means for adjusting a power of at least one of said drive units individually.