Ducted fan vehicles particularly useful as VTOL aircraft

• US 7,918,416 B2
• Filed: 08/22/2007
• Issued: 04/05/2011
• Est. Priority Date: 05/29/2001
• Status: Expired due to Fees

• Current Assignee: Urban Aeronautics Ltd.
• Original Assignee: Urban Aeronautics Ltd.
• Inventors: Yoeli, Rafi
• Primary Examiner(s): SWIATEK, ROBERT P
• Application Number:
  US11/892,414
• Publication Number:
  US 20090140102A1
• Time in Patent Office: 1,322 Days
• Field of Search: 244/12.1, 244/12.2, 244/12.3, 244/12.4, 244/12.5, 244/12.6, 244/23.R, 244/23.A, 244/23.B, 244/23.C, 244/23.D, 244/53.B, 180/116, 180/117
• US Class Current: 244/23.00A
• 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 vehicle frame, a duct carried by the vehicle frame with the longitudinal axis of the duct perpendicular to the longitudinal axis of the vehicle frame, a propeller rotatably mounted within the duct about the longitudinal axis of the duct to force an ambient fluid therethrough from its inlet at the upper end of the duct through its exit at the lower end of the duct, and thereby to produce an upward lift force applied to the vehicle, and a plurality of parallel, spaced vanes pivotally mounted to and across the inlet end of the duct about pivotal axes perpendicular to the longitudinal axis of the duct and substantially parallel to the longitudinal axis of the vehicle frame, the vanes being selectively pivotal about their axes to produce a desired horizontal force component to the lift force applied to the vehicle.

Claims

1. A vehicle, comprising:

a vehicle frame;

a first duct carried by said vehicle frame at a forward end of said vehicle frame and a second duct carried by said vehicle frame at an aft end of said vehicle frame, with longitudinal axes of said first and second ducts arranged substantially perpendicular to a longitudinal axis of the vehicle frame;

a propeller rotatably mounted within each of said first and second ducts, each propeller arranged to force an ambient fluid through its respective duct from an inlet at an upper end of the duct through an exit at a lower end of the duct, to thereby produce an upward lift force applied to the vehicle; and

a plurality of parallel, pivotably mounted vanes extending across the inlet of each duct for rotation about respective axes substantially perpendicular to said longitudinal axes of the ducts and substantially parallel to said longitudinal axis of the vehicle frame, said vanes being selectively pivotable about said respective axes to produce a desired horizontal force component to the lift force applied to the vehicle.

2. The vehicle according to claim 1 wherein said vanes have a symmetrical airfoil shape.

3. The vehicle according to claim 1 wherein each of said vanes is split into two halves, each half of all the vanes being separately pivotable from the other half of all the vanes, whereby the force component to the lift force applied to the vehicle is a rotary moment force about the duct longitudinal axis.

4. The vehicle according to claim 1, wherein each of said vanes includes a fixed section and a pivotable section mounted at the trailing side of the fixed section.

5. The vehicle according to claim 1, wherein each of said first and second ducts includes a second plurality of parallel pivotably mounted vanes extending across said inlet of the duct and pivotable about second axes perpendicular to said respective axes of the first-mentioned plurality of vanes and perpendicular to said longitudinal axis of the duct.

6. The vehicle according to claim 5 wherein the second axes of said second plurality of vanes are in a plane vertically spaced from the axes of said first-mentioned plurality of vanes.

7. The vehicle according to claim 5 wherein the second axes of said second vanes are in a common plane with that of the pivotal axes of said first-mentioned plurality of vanes.

8. The vehicle according to claim 1 wherein each said duct includes a second plurality of parallel pivotably mounted vanes extending across said exit of the duct about axes perpendicular to said longitudinal axis of the duct and substantially parallel to said longitudinal axis of the vehicle frame to thereby produce a desired side force component, or a rotary moment force component about the duct transverse axis, to the lift force applied to the vehicle.

9. The vehicle according to claim 8 wherein said first and second plurality of vanes are respectively pivotable in opposite directions to thereby produce a rotary moment about a transverse axis of said duct.

10. The vehicle according to claim 8 wherein said first and second plurality of vanes are respectively pivotable in the same direction to thereby produce a side force on the vehicle.