Vehicles particularly useful as VTOL vehicles

• US 20080142643A1
• Filed: 07/12/2007
• Published: 06/19/2008
• Est. Priority Date: 06/04/2001
• Status: Active Grant

• Current Assignee: Urban Aeronautics Ltd.
• Original Assignee: Urban Aeronautics Ltd.
• Inventors: Yoeli, Rafi
• Granted Patent: US 7,789,342 B2
• Time in Patent Office: Days
• US Class Current: 244/23R
• CPC Class Codes: B60V 1/06 wherein the cushion is formed within plenum chamber
• CPC Class Codes: B60V 3/02 Land vehicles, e.g. road vehicles
• CPC Class Codes: B64C 27/20 Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
• CPC Class Codes: B64C 29/0025 the propellers being fixed relative to the fuselage

Abstract

A vehicle including a fuselage, at least one lift-producing propeller carried by the fuselage on each side of its transverse axis a pilot'"'"'s compartment formed in the fuselage between the lift-producing propellers and substantially aligned with the longitudinal axis, and a pair of payload bays formed in the fuselage between the lift-producing propellers and on opposite sides of the pilot'"'"'s compartment. Many variations are described enabling the vehicle to be used not only as a VTOL vehicle, but also as a multi-function utility vehicle for performing many diverse functions including hovercraft and ATV functions.

Claims

1-24. -24. (canceled)

25. A vehicle comprising:

a fuselage having a longitudinal axis and a transverse axis wherein said fuselage includes a pair of thrust-producing propellers at the rear end of said fuselage on opposite sides of said longitudinal axis, said pair of thrust-producing propellers supported above said fuselage on a pair of pylons extending upwardly from said fuselage;

at least two lift-producing propellers carried within said fuselage respectively on each side of said transverse axis;

a compartment formed in said fuselage between said lift-producing propellers; and

at least two engines, each capable of driving said pair of thrust-producing propellers and said lift-producing propellers.

26. The vehicle of claim 25 wherein said thrust producing propellers are located at opposite ends of a horizontal stabilizer, said horizontal stabilizer adjustable about a horizontal axis.

27. The vehicle according to claim 25 wherein said two engines are located in engine compartments within said pylons.

28. The vehicle according to claim 25 wherein said two engines are located in a common engine compartment aligned with said longitudinal axis and underlying said compartment.

29. The vehicle according to claim 25 wherein the vehicle includes a flexible skirt extending below the fuselage enabling the vehicle to be used as a hovercraft for movement over ground or water.

30. The vehicle according to claim 25 wherein the vehicle includes a plurality of wheels attachable to the rear end of said fuselage for converting the vehicle to an all-terrain vehicle.

31. The vehicle according to claim 25 wherein a plurality of vanes extend across an inlet side of each lift producing propeller.

32. The vehicle according to claim 31 wherein said plurality of vanes extend substantially parallel to said longitudinal axis.

33. The vehicle according to claim 25 wherein said fuselage carries landing gear moveable between extended and retracted positions.

34. A vehicle, comprising:

a fuselage having a longitudinal axis and a transverse axis;

at least one lift-producing propeller carried by said fuselage on each side of said transverse axis;

a compartment formed in said fuselage between said lift-producing propellers;

at least one payload bay formed in said fuselage between said lift-producing propellers, wherein the vehicle is a vertical take-off and landing (VTOL) vehicle; and

wherein said VTOL vehicle includes a pair of stub wings each moveable between a retracted, stored position and an extended, deployed position.

35. The vehicle according to claim 34, wherein said fuselage carries landing gear moveable between extended and retracted positions.

36. The vehicle according to claim 34 wherein said payload bay includes a support for supporting at least a portion of the payload externally of the fuselage.

37. The vehicle according to claim 34 wherein said payload bay includes a cover extendable between open and closed positions, and wherein, in said open position, said cover provides support for at least a portion of the payload externally of said fuselage.

38. The vehicle according to claim 34 further comprising a pair of thrust-producing propellers supported on pylons extending upwardly from a rear end of said fuselage, on opposite sides of said longitudinal axis.

39. The vehicle according to claim 38 wherein said thrust producing propellers are located at opposite ends of an adjustable horizontal stabilizer extending between said pylons.

40. The vehicle according to claim 38 further comprising at least two engines, each capable of driving said pair of thrust producing propellers and said at least one lift producing propeller.

41. The vehicle according to claim 34 wherein the vehicle includes a flexible skirt extending below the fuselage enabling the vehicle to be used as a hovercraft for movement over ground or water.

42. A ducted fan vehicle comprising:

a fuselage having a longitudinal axis and a transverse axis wherein said fuselage includes at least two ducted fans incorporating lift-producing propellers carried within said fuselage respectively on each side of said transverse axis;

a compartment formed in said fuselage between said lift-producing propellers;

wherein said fuselage includes two engines, each of said engines capable of driving all of said lift-producing propellers, said two engines being mechanically coupled together in a common transmission system; and

wherein each of the engines connects to one of the lift-producing propellers via plural gear boxes, and the other of the lift-producing propellers is connected to said two engines via another gear box longitudinally aligned with one of said plural gear boxes.

43. The ducted fan vehicle according to claim 42 further comprising a pair of thrust-producing propellers connected to respective ones of said two engines via two of said plural gear boxes connected directly to said engines.

44. The ducted fan vehicle of claim 42 wherein a plurality of vanes extend across an inlet side of each ducted fan.

45. The ducted fan vehicle of claim 44 wherein said plurality of vanes extend substantially parallel to said longitudinal axis.

46. The ducted fan vehicle of claim 43 wherein the vehicle includes a flexible skirt extending below the fuselage enabling the vehicle to be used as a hovercraft for movement over ground or water.

47. The ducted fan vehicle of claim 43 wherein said fuselage carries landing gear moveable between extended and retracted positions.

48. A vehicle comprising:

a fuselage having a longitudinal axis and a transverse axis;

at least two lift-producing propellers carried within said fuselage respectively on each side of said transverse axis;

a compartment formed in said fuselage between said lift-producing propellers;

at least two engines, each capable of driving said lift-producing propellers; and

wherein the vehicle includes a flexible skirt extending below the fuselage enabling the vehicle to be used as a hovercraft for movement over ground or water.

49. A vehicle comprising:

a fuselage having a longitudinal axis and a transverse axis;

at least two lift-producing propellers carried within said fuselage respectively on each side of said transverse axis;

a compartment formed in said fuselage between said lift-producing propellers;

at least two engines, each capable of driving said lift-producing propellers; and

wherein said fuselage carries landing gear.