Aircraft

• US 4,196,877 A
• Filed: 06/15/1977
• Issued: 04/08/1980
• Est. Priority Date: 06/15/1977
• Status: Expired due to Term

• Current Assignee: Jean L. Mutrux
• Original Assignee: Jean L. Mutrux
• Inventors: Mutrux, Jean L.
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US05/806,580
• Time in Patent Office: 1,028 Days
• Field of Search: 244/12.1, 244/12.2, 244/12.3, 244/23 R, 244/23 C, 244/23 B, 244/17.19, 244/6, 244/91, 244/34 A, 244/45 R, 416/114
• US Class Current: 244/12.2
• CPC Class Codes: B64C 39/06 having disc- or ring-shaped wings

Abstract

An aircraft comprising a generally annular wing structure surrounding a circular central structure to form an annular air duct, a pair of fuselages extending longitudinally at opposite sides of the aircraft, and rotor blades extending radially across the air duct from the central structure and rotatable relative to the central structure around the duct for inducing airflow through the duct to effect a lift on the aircraft. The annular wing structure consists of forward and rear wings forming air foils, the forward wing having a generally semicircular trailing edge and the rear wing having a generally semicircular leading edge.

Claims

1. An aircraft comprising a generally annular wing structure surrounding a circular central structure forming an annular air duct, said central structure having a vertical central axis,

a first fuselage extending longitudinally of the aircraft at one side of the wing structure,

a second fuselage extending longitudinally of the aircraft at the opposite side of the wing structure,

rotor means carried by said central structure comprising a plurality of rotor blades extending radially across said duct, said blades being rotatable relative to said central structure around the duct generally on the vertical central axis of said central structure for inducing airflow through the duct to effect a lift on the aircraft,

said annular wing structure comprising forward and rear wings forming air foils, the forward wing having a trailing edge and the rear wing having a leading edge which are generally on a circle generally concentric with the vertical central axis of the central structure, the trailing edge of the forward wing and the leading edge of the rear wing being semicircles of said circle, the annular air duct being constituted by the space between said central structure and said circle, the forward wing having a generally forward angle of air attack such that the rotation of said rotor blades around said duct causes a high-velocity airflow over the upper surface of the forward wing for increasing said lift,

parallel counterrotation vanes extending across said air duct below the rotor blades and between said forward and rear wings generally parallel to the fuselages for preventing rotation of the aircraft in reaction to rotation of the blades, said vanes being mounted at their outer ends on said wing structure for swinging about their longitudinal axes, and

a rotor drive shaft carried by the central structure and extending along the axis of rotation of said blades for rotating the blades around the duct, said vanes being arranged in forward and rearward sets extending from a central vane support at the lower end of the shaft to said forward and rearward wings, respectively.

2. An aircraft as set forth in claim 1 wherein navigation fins extend from said vane support to the fuselages generally perpendicular to said counterrotation vanes, said fins being swingable about axes extending longitudinally of the fins for controlling the axial flow of air through the duct thereby to allow navigation of the aircraft generally forwardly and rearwardly.

3. An aircraft comprising a generally annular wing structure surrounding a circular central structure forming an annular air duct, said central structure having a vertical central axis,

a first fuselage extending longitudinally of the aircraft at one side of the wing structure,

a second fuselage extending longitudinally of the aircraft at the opposite side of the wing structure, and

rotor means carried by said central structure comprising a plurality of rotor blades extending radially across said duct, said blades being rotatable relative to said central structure around the duct generally on the vertical central axis of said central structure for inducing airflow through the duct to effect a lift on the aircraft,

said annular wing structure comprising forward and rear wings forming air foils, the forward wing having a trailing edge and the rear wing having a leading edge which are generally on a circle generally concentric with the vertical central axis of the central structure, the trailing edge of the forward wing and the leading edge of the rear wing being semicircles of said circle, the annular air duct being constituted by the space between said central structure and said circle, the forward wing having a generally forward angle of air attack such that the rotation of said rotor blades around said duct causes a high-velocity airflow over the upper surface of the forward wing for increasing said lift,

parallel counterrotation vanes extending across said air duct below the rotor blades for preventing rotation of the aircraft in reaction to rotation of the blades, said vanes being mounted at their outer ends on said wing structure for swinging about their longitudinal axes, and

navigation fins extending across the air duct between said central structure and said fuselages at substantially the same elevation as said counterrotation vanes, said fins being swingable about axes extending longitudinally of the fins for controlling the axial flow of air through the duct thereby to allow navigation of the aircraft generally forwardly and rearwardly.

4. An aircraft comprising a generally annular wing structure surrounding a circular central structure forming an annular air duct, a first fuselage extending longitudinally of the aircraft at one side of the wing structure, a second fuselage extending longitudinally of the aircraft at the opposite side of the wing structure, rotor means carried by said central structure comprising a rotor member rotatable relative to the central structure and a plurality of rotor blades pivoted to the rotor member and extending radially outwardly therefrom toward the annular wing structure across said duct, said blades being rotatable relative to said central structure around the duct for inducing airflow through the duct to effect a lift on the aircraft, said annular wing structure comprising forward and rear wings forming air foils, the forward wing having a generally semicircular trailing edge, and the rear wing having a generally semicircular leading edge, said edges defining a circle generally concentric with and spaced from said circular central structure, circular cam means carried by the central structure and disposed around the axis of rotation of said blades, means rigidly carried by the central structure for tilting the cam means in any of various directions relative to the central structure and for changing the elevation of the cam means relative to the blades at any or no tilt while preventing rotation of the cam means relative to the central structure, follower means engageable with opposite sides of the cam means at any tilt and elevation thereof, and linkages connecting the rotor blades with the follower means for pivoting the blades whereby the angle of air attack of the blades is simultaneously and equally changed when the elevation of the cam means is changed and the angle of attack of each blade is varied from a maximum to a minimum during one revolution of the blade around said duct when the cam means is tilted, each of said linkages comprising a guide block on said rotatable ring, a control bar slidable in the guide block in a direction parallel to the axis of rotation of the rotatable ring and having said follower means secured thereto, and a crank means connecting the control bar and a respective rotor blade pivot whereby the bar is adapted to slide in the guide when the elevation of said cam means is changed thereby to rotate the crank means and the rotor blade pivot for pivoting the blade.

5. An aircraft as set forth in claim 4 wherein said follower means comprises a pair of rollers mounted on the control bar for rolling engagement with the top and bottom of the cam means.

6. An aircraft comprising a generally annular wing structure surrounding a circular central structure forming an annular air duct, said central structure having a vertical central axis,

a first fuselage extending longitudinally of the aircraft at one side of the wing structure,

a second fuselage extending longitudinally of the aircraft at the opposite side of the wing structure,

rotor means carried by said central structure comprising a plurality of rotor blades extending radially across said duct, said blades being rotatable relative to said central structure around the duct generally on the vertical central axis of said central structure for inducing airflow through the duct to effect a lift on the aircraft,

said annular wing structure comprising forward and rear wings forming air foils, the forward wing having a trailing edge and the rear wing having a leading edge which are generally on a circle generally concentric with the vertical central axis of the central structure, the trailing edge of the forward wing and the leading edge of the rear wing being semicircles of said circle, the annular air duct being constituted by the space between said central structure and said circle, the forward wing having a generally forward angle of air attack such that the rotation of said rotor blades around said duct causes a high-velocity airflow over the upper surface of the forward wing for increasing said lift,

a tail extending rearwardly from each of said fuselages, and

a rudder mounted at the center of said rear wing between said tails.

7. An aircraft as set forth in claim 6 wherein each of said tails has a flap mounted at its rear for rotation about an axis extending generally transversely of the aircraft.

8. An aircraft comprising a generally annular wing structure surrounding a circular central structure forming an annular air duct, said central structure having a vertical central axis,

a first fuselage extending longitudinally of the aircraft at one side of the wing structure,

a second fuselage extending longitudinally of the aircraft at the opposite side of the wing structure,

rotor means carried by said central structure comprising a plurality of rotor blades extending radially across said duct, said blades being rotatable relative to said central structure around the duct generally on the vertical central axis of said central structure for inducing airflow through the duct to effect a lift on the aircraft,

said annular wing structure comprising forward and rear wings forming air foils, the forward wing having a trailing edge and the rear wing having a leading edge which are generally on a circle generally concentric with the vertical central axis of the central structure, the trailing edge of the forward wing and the leading edge of the rear wing being semicircles of said circle, the annular air duct being constituted by the space between said central structure and said circle, the forward wing having a generally forward angle of air attack such that the rotation of said rotor blades around said duct causes a high-velocity airflow over the upper surface of the forward wing for increasing said lift, and

deflector fins extending longitudinally along the bottom of said fuselages for deflecting downwardly the axial flow of air through said duct.