Ducted fan vehicles particularly useful as VTOL aircraft

• US 6,464,166 B1
• Filed: 05/29/2001
• Issued: 10/15/2002
• Est. Priority Date: 05/29/2001
• Status: Expired due to Term

• Current Assignee: Romeo Yankee Limited
• Original Assignee: Romeo Yankee Limited
• Inventors: Yoeli, Rafi
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US09/865,678
• Time in Patent Office: 504 Days
• Field of Search: 244/21, 244/23, 244/53.B
• US Class Current: 244/12.1
• 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, particularly a VTOL air vehicle, includes 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, e.g. air, 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 are selectively pivotal to produce a desired horizontal force component to the lift force applied to the vehicle. Various vane arrangements are disclosed for producing side, roll, pitch and yaw movements of the vehicle.

Claims

1. A vehicle, comprising

a vehicle frame;

a duct carried by said vehicle frame with the longitudinal axis of the duct perpendicular to the longitudinal axis of the vehicle frame;

a propeller rotatably mounted within said 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 said longitudinal axis of the duct and substantially parallel to said longitudinal axis of the vehicle frame, said vanes being selectively pivotal about their 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 and are spaced from each other a distance approximately equal to the chord length of the vanes.

3. The vehicle according to claim 1, wherein each of said vanes is pivotally mounted as a unit for its complete length to produce a desired side force component.

4. The vehicle according to claim 1, wherein each of said vanes is split into two halves, each half of all the vanes being separately pivotal 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.

5. The vehicle according to claim 1, wherein each of said vanes is pivotally mounted about an axis passing through the vane.

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

7. The vehicle according to claim 1, wherein said duct includes a second plurality of parallel, spaced vanes pivotally mounted to and across said inlet end of the duct about pivotal axes perpendicular to said pivotal axes of the first-mentioned plurality of vanes and perpendicular to said longitudinal axis of the duct.

8. The vehicle according to claim 7, wherein the pivotal axes of said second plurality of vanes are in a plane vertically spaced from the pivotal axes of said first-mentioned plurality of vanes.

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

10. The vehicle according to claim 1, wherein said duct includes a second plurality of parallel, spaced vanes pivotally mounted to and across said exit end of the duct about pivotal 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.

11. The vehicle according to claim 10, wherein said vanes in both of said plurality have a symmetrical airfoil shape and are spaced from each other a distance approximately equal to the chord length of the vanes in the second plurality of vanes.

12. The vehicle according to claim 1, wherein said duct, propeller and plurality of vanes are carried by said vehicle at one end of the vehicle, and said vehicle includes a second duct, propeller and plurality of vanes at the opposite end of the vehicle.

13. The vehicle according to claim 1, wherein the vehicle carries the duct, propeller and plurality of vanes at the center of the vehicle.

14. The vehicle according to claim 1, wherein the vehicle is a VTOL air vehicle.

15. A VTOL air vehicle, comprising:

a vehicle frame;

a duct carried by said vehicle frame with the longitudinal axis of the duct perpendicular to the longitudinal axis of the vehicle frame;

a propeller rotatably mounted within said duct about the longitudinal axis of the duct to force air 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 said longitudinal axis of the duct and substantially parallel to said longitudinal axis of the vehicle frame, said vanes being selectively pivotal along their axes to produce a desired horizontal force component to the lift force applied to the vehicle.

16. The VTOL air vehicle according to claim 15, wherein said vanes have a symmetrical airfoil shape and are spaced from each other a distance approximately equal to the chord length of the vanes.

17. The VTOL air vehicle according to claim 15, wherein each of said vanes is pivotally mounted as a unit for its complete length to produce a desired side force component.

18. The VTOL air vehicle according to claim 15, wherein said duct includes a second plurality of parallel, spaced vanes pivotally mounted to and across said exit end of the duct about pivotal axes perpendicular to said longitudinal axes of the duct and 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.

19. The VTOL air vehicle according to claim 18, wherein said duct, propeller and plurality of vanes are carried by said vehicle at one end of the vehicle, and said vehicle includes a second duct, propeller and plurality of vanes at the opposite end of the vehicle.

20. The VTOL air vehicle according to claim 18, wherein the vehicle carries the duct, propeller and plurality of vanes at the center of the vehicle.