Compound helicopter

• US 20050151001A1
• Filed: 06/21/2004
• Published: 07/14/2005
• Est. Priority Date: 07/02/2003
• Status: Abandoned Application

• Current Assignee: Arthur W. Loper
• Original Assignee: Arthur W. Loper
• Inventors: Loper, Arthur W.
• Application Number:
  US10/871,028
• Publication Number:
  US 20050151001A1
• Time in Patent Office: Days
• US Class Current: 244/6
• CPC Class Codes: B64C 2027/8236 including pusher propellers
• CPC Class Codes: B64C 2027/8281 comprising horizontal tail planes
• CPC Class Codes: B64C 27/14 Direct drive between power plant and rotor hub
• CPC Class Codes: B64C 27/26 characterised by provision of fixed wings

Abstract

The compound helicopter is a hybrid combination of a helicopter and a fixed wing aircraft. A conventional helicopter is modified with a nose-mounted tractor propeller to provide thrust for forward flight. Wings are added to provide lift during forward flight. With the propeller providing thrust and the wings lift during forward flight, the helicopter rotor blades are unloaded during cruising flight to allow increased forward speed by avoiding limitations of conventional helicopters, including retreating rotor blade stall and maximum rotor blade tip speeds. A single powerplant drives both the main rotor and the nose-mounted propeller. The compound helicopter employs high aspect ratio wings with large flaps that may be extended to reduce vertical drag during vertical flight and hovering operations.

Claims

1. A compound helicopter, comprising:

a fuselage having a nose and a tail;

a wing structure mounted on said fuselage;

a main helicopter rotor operably disposed on top of said fuselage, the main helicopter rotor having a plurality of rotor blades, the rotor blades defining a rotor disk;

a propeller operably disposed on the nose of said fuselage ahead of said rotor disk;

a powerplant disposed in said fuselage;

a propeller drive train connected between said powerplant and said propeller in order to drive said propeller; and

a main rotor drive train connected between said powerplant and said main rotor to drive said main rotor.

3. The compound helicopter according to claim 1, wherein said wing structure has a high aspect ratio.

4. The compound helicopter according to claim 1, wherein said wing structure comprises a pair of wings extending from either side of said fuselage, each of said pair of wings having a leading edge and a trailing edge.

5. The compound helicopter according to claim 4, wherein each of said pair of wings comprises at least one wing flap pivotally disposed on the trailing edge.

6. The compound helicopter according to claim 5, wherein said at least one wing flap comprises a slotted flap.

7. The compound helicopter according to claim 5, wherein said at least one wing flap comprises an umbrella flap having a flap member, an upper trailing edge slat, and a lower trailing edge slat.

8. The compound helicopter according to claim 4, wherein each of said pair of wings comprises a plurality of leading edge slats pivotally disposed on said leading edge.

9. The compound helicopter according to claim 1, wherein said propeller drive train comprises a clutch selectively engaging said propeller to, and disengaging said propeller from, said powerplant.

10. The compound helicopter according to claim 1, wherein said main rotor drive train comprises a clutch selectively engaging said main rotor to, and disengaging said main rotor from, said powerplant.

11. The compound helicopter according to claim 1, wherein said powerplant comprises:

at least one engine; and

a transmission coupled to said at least one engine, the transmission having a plurality of output shafts.

12. The compound helicopter according to claim 11, wherein said propeller drive train is connected to one of said output shafts.

13. The compound helicopter according to claim 12, wherein said transmission comprises means for selectively engaging and disengaging said propeller drive train to and from said one of said output shafts.

14. The compound helicopter according to claim 11, wherein said main rotor drive train is connected to one of said output shafts.

15. The compound helicopter according to claim 14, wherein said transmission comprises means for selectively engaging and disengaging said main rotor drive train to and from said one of said output shafts.

16. The compound helicopter according to claim 11, further comprising an engine control system operably connected to said at least one engine.

17. The compound helicopter according to claim 16, further comprising a main rotor control unit operably connected to said main rotor and in communication with said engine control system.

18. The compound helicopter according to claim 16, further comprising a propeller control unit operably connected to said propeller and in communication with said engine control system.

19. The compound helicopter according to claim 11, further comprising:

an engine control system operably connected to said at least one engine;

a propeller control unit operably connected to said propeller and in communication with said engine control system; and

a main rotor control unit operably connected to said main rotor and in communication with said engine control system.

20. The compound helicopter according to claim 16, wherein said engine control system is a full authority digital engine controller.

2. (canceled)