Airfoil canopy aircraft

• US 5,160,100 A
• Filed: 07/01/1991
• Issued: 11/03/1992
• Est. Priority Date: 07/01/1991
• Status: Expired due to Term

• Current Assignee: Ist Aerospace Inc.
• Original Assignee: Stephen L. Snyder
• Inventors: Snyder, Stephen L.
• Primary Examiner(s): BAREFOOT, GALEN L
• Application Number:
  US07/724,191
• Time in Patent Office: 491 Days
• Field of Search: 244/2, 244/13, 244/16, 244/46, 244/47, 244/48, 244/49, 244/145, 244/902, 244/903, 244/904
• US Class Current: 244/13
• CPC Class Codes: B64C 31/036 having parachute-type wing

Abstract

An aircraft comprises a vehicle (1) suspended in flight by a steering control rod (68) pivotally mounted to the body of the vehicle and having outer ends (12, 14) connected to the lower ends of load suspension lines (3, 5, 6) connected at their upper ends to a flexible wing portion (2) of a ram air inflatable type of airfoil canopy. Steering of the aircraft is by pivotal movement of control rod (68) to manipulate the load suspension lines and thereby the canopy surfaces. The aircraft may be radio controlled by a radio receiver (112) in the vehicle body for operating the speed of a drive motor (36) for driving a propeller (38) and a steering drive motor (98) coupled to the control rod (68) by a suitable linkage system. Battery pack (104) is removably mounted in the vehicle body for providing power to the receiver and motors therein. The radio controlled aircraft is controlled by a remote transmitter which controls the steering and speed of the aircraft.

Claims

1. An aircraft comprising:

an airfoil canopy for producing lift by aerodynamic forces exerted thereon;

a plurality of flexible load lines connected to said canopy;

a vehicle suspended from said canopy by said load lines in a flight supporting position, said vehicle having a center of gravity and a directional axis extending substantially in the direction of flight of said vehicle in said flight supporting position;

steering control bar means movabley mounted on said vehicle and extending in a direction substantially transverse to said directional axis;

at least two suspension points on said control bar means connected to said load liens so that said center of gravity of said vehicle is below said suspension points in said flight supporting position; and

control means for moving said steering control bar means relative to said vehicle for manipulating said load lines to control the attitude of said canopy in said flight supporting position and steer the aircraft.

2. An aircraft as claimed in claim 1 wherein said steering control bar means comprises:

an elongated control bar having end portions; and

pivot means for pivotally mounting said control bar on said vehicle between said end portions.

3. An aircraft as claimed in claim 2 wherein:

said control bar is mounted by said pivot means for pivotal movement about an axis which is substantially horizontal in level flight.

4. An aircraft as claimed in claim 2 wherein:

said control bar is mounted by said pivot means for pivotal movement about an axis which is substantially vertical in level flight.

5. An aircraft as claimed in claim 1 wherein

an elongated control bar having a longitudinal axis and end portions;

and

means for mounting said control bar for movement in the longitudinal direction thereof substantially transversely relative to said directional axis of said vehicle.

6. An aircraft as claimed in claim 1 and further comprising:

power means mounted on said vehicle for providing forward thrust to said aircraft.

7. An aircraft as claimed in claim 3 wherein:

said directional axis of said vehicle comprises a directional front to rear axis;

a mounting hole extending transversely through said control rod; and

said pivot means comprises a pivot shaft extending through said mounting hole and having a pivot axis and mounted on said vehicle with said pivot axis substantially parallel with said directional axis.

8. An aircraft as claimed in claim 3 wherein:

said directional axis of said vehicle comprises a directional front to rear axis;

a mounting hole extends transversely through said control rod; and

said pivot means comprises a pivot shaft extending through said mounting hole and having a pivot axis and mounted on said vehicle with said pivot axis extending substantially perpendicular to said directional axis.

9. An aircraft as claimed in claim 7 and further comprising:

a plurality of ground support wheels rotatably mounted on said vehicle for supporting said vehicle for movement on the ground.

10. An aircraft as claimed in claim 1 wherein:

said airfoil canopy comprises a substantially flexible canopy.

11. An aircraft as claimed in claim 10 wherein:

said canopy comprises a ram air inflatable canopy.

12. An aircraft as claimed in claim 1 wherein said control means comprises:

linkage means mounted on said vehicle and operatively connected to said steering control bar means;

servo motor means mounted on said vehicle and connected to said linkage means for moving said steering control bar; and

means for operating said servo motor means.

13. An aircraft as claimed in claim 1 wherein said control means comprises:

cable and pulley means mounted on said vehicle and operatively connected to said steering control bar for moving said steering control bar; and

means for operating said cable and pulley means.

14. An aircraft as claimed in claim 12 wherein said means for operating said servo motor means comprises:

electric storage battery means supported on said vehicle and electrically connected to said servo motor;

radio signal receiver means mounted on said vehicle and electrically connected to said battery means and said servo motor for controlling the operation of said servo motor; and

remote control radio transmitter means for transmitting control signals to said receiver means for controlling said servo motor.

15. An aircraft as claimed in claim 14 wherein:

electric motor power means is mounted on said vehicle;

propeller means is mounted on said electric motor power means to be driven thereby to provide thrust for the aircraft;

said battery means is electrically connected to said motor power means; and

said receiver means and radio transmitter means further comprise means for controlling the speed of said motor power means.

16. An aircraft as claimed in claim 2 and further comprising:

power means mounted on said vehicle for providing forward thrust to said aircraft.

17. An aircraft as claimed in claim 3 and further comprising:

power means mounted on said vehicle for providing forward thrust to said aircraft.

18. An aircraft as claimed in claim 4 and further comprising:

power means mounted on said vehicle for providing forward thrust to said aircraft.

19. An aircraft as claimed in claim 5 and further comprising:

power means mounted on said vehicle for providing forward thrust to said aircraft.

20. An aircraft as claimed in claim 1 wherein:

said control means comprises a pilot operated control mechanism.

21. An aircraft comprising:

an airfoil canopy for producing lift by aerodynamic forces exerted thereon;

a plurality of flexible load lines connected to said canopy;

a vehicle suspended from said canopy by said load lines in a flight supporting position said vehicle having a center of gravity and a directional axis extending in the direction substantially of flight of said vehicle in said flight supporting position;

steering control bar means movably mounted on said vehicle and extending in a direction substantially transverse to said directional axis;

at least two suspension points on said control bar means connected to said load lines so that said center of gravity of said vehicle is below said suspension points in said flight supporting position;

control means for moving said steering control bar means relative to said vehicle for manipulating said load lines to control the attitude of said canopy in said flight supporting position and steer the aircraft;

electric motor means mounted on said vehicle;

propeller means mounted on said vehicle and connected to said motor means for being driven thereby to provide thrust for the aircraft; and

battery means supported on the vehicle below said control bar means and operatively connected to said motor means for operating said motor means.