Ducted fan vehicles particularly useful as VTOL aircraft

• US 20050178881A1
• Filed: 11/15/2004
• Published: 08/18/2005
• Est. Priority Date: 05/28/2002
• Status: Active Grant

• Current Assignee: Urban Aeronautics Ltd.
• Original Assignee: Urban Aeronautics Ltd.
• Inventors: Yoeli, Rafi
• Granted Patent: US 7,275,712 B2
• Time in Patent Office: Days
• US Class Current: 244/12.100
• 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

1-22. -22. (canceled)

23. 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, wherein said vanes include;

a first group of parallel vanes extending across one half of the inlet of said duct and pivotal about axes at a predetermined acute angle with respect to the longitudinal axis of the vehicle frame; and

a second group of parallel vanes extending across the remaining half of the inlet end of said duct and pivotal about axes at said predetermined angle, but in the opposite direction, with respect to the longitudinal axis of the vehicle frame, wherein said first and second groups of vanes being selectively pivotal to produce a desired net control force in addition to the lift force applied to the vehicle.

24. The vehicle according to claim 23, wherein said predetermined angle is 45 degrees.