UNIVERSAL FLYING TERRAIN VEHICLE

Abstract

A universal aerial platform (11, 41) supports lift elements (13, 14), thrusters (15), landing gear (21, 22) and a fuel supply (16) and has a coupling mechanism (17) external to the aerial platform for coupling to a terrain vehicle (20) so as to convert any suitably adapted terrain vehicle to a flying vehicle (10, 40). The terrain vehicle forms the cockpit of the flying vehicle. The terrain vehicle (20) includes flight controls that are automatically coupled to the airplane structure either wirelessly or by wires when the terrain vehicle is coupled thereto.

Claims

1-18. (canceled)

19. An aerial platform comprising a structure that supports lift elements, thrusters, landing gear and a fuel supply and has a coupling mechanism external to said structure adapted for coupling to a suitably adapted terrain vehicle so as to convert the terrain vehicle to a flying vehicle; the aerial platform has a wingspan whose height from the ground provides sufficient clearance for accommodating terrain vehicles of different heights, the coupling mechanism is adapted to engage one or more connectors supported directly or indirectly by a chassis of the terrain vehicle, the coupling mechanism is capable of engaging the connectors regardless of the height of the terrain vehicle and of supporting the terrain vehicle off the ground after engagement.

20. The aerial platform according to claim 19, wherein the coupling mechanism is capable of being lowered and raised in order to facilitate engagement with the connectors regardless of the height of the terrain vehicle and to lift the terrain vehicle off the ground after engagement.

21. The aerial platform according to claim 19, further including adjustable legs that serve as landing gear and each of which comprises at least two telescopic elements that can be extended between a collapsed position and an extended position.

22. The aerial platform according to claim 21, wherein height adjustment of the adjustable legs serves to lower and raise the coupling mechanism in order to facilitate engagement with the connectors regardless of the height of the terrain vehicle and to lift the terrain vehicle off the ground after engagement.

23. A flying vehicle comprising the aerial platform according to claim 19 coupled to a terrain vehicle, wherein the terrain vehicle forms the cockpit of the flying vehicle.

24. The flying vehicle according to claim 19, wherein the terrain vehicle includes flight controls that are automatically coupled to the airplane structure when the terrain vehicle is coupled to the airplane structure.

25. The flying vehicle according to claim 24, wherein the flight controls includes levers that are coupled via the coupling mechanism to control elements of the airplane structure.

26. The flying vehicle according to claim 24, wherein the flight controls generate control signals that are conveyed wirelessly to control elements of the airplane structure.

27. The flying vehicle according to claim 24, wherein the flight controls generate control signals that are conveyed by wires to control elements of the airplane structure, each of said wires having respective segments in the terrain vehicle and the airplane structure and said respective segments being adapted for mutual coupling via respective connectors in the terrain vehicle and the airplane structure.

28. The flying vehicle according to claim 19, wherein the terrain vehicle serves only as a payload and the airplane structure is adapted for remote control.

29. The flying vehicle according to claim 19, wherein the coupling mechanism includes at least one latch mechanism adapted to latch on to said one or more connectors.

30. The flying vehicle according to claim 29, wherein the one or more connectors are fixed to elements mounted on a roof of the terrain vehicle.

31. The flying vehicle according to claim 29, wherein each latch mechanism includes on opposite sides thereof clasps capable of being retracted hydraulically or pneumatically via pistons so as to close the clasps from an open position to a closed position wherein they engage recesses on opposite sides of the respective connector.

32. The aerial platform according to claim 29, wherein each latch mechanism includes on opposite sides thereof clasps capable of being retracted hydraulically or pneumatically via pistons so as to close the clasps from an initially open position.

33. The aerial platform according to claim 19, being a fixed-wing airplane wherein the lift elements are wings mounted on opposite sides of a fuselage of the aerial platform and the thrusters are engines mounted under the wings.

34. The aerial platform according to claim 19, being a rotate-wing aircraft wherein the lift elements are rotor blades.

35. The aerial platform according to claim 34, further including adjustable legs that serve as landing gear and each of which comprises at least two telescopic elements that can be extended between a collapsed position and an extended position.

36. The aerial platform according to claim 19, being a parafoil wing aircraft wherein the lift elements are parafoils.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0021] In order to understand the invention and to see how it may be carried out in practice, embodiments will now be described, by way of non-limiting example only, with reference to the accompanying drawings, in which:

[0022] FIG. 1 is a partial front elevation showing a flying car according to a first embodiment of the invention comprising a terrain vehicle coupled to an aerial platform having a fixed wing;

[0023] FIG. 2 is a partial section showing the terrain vehicle disengaged from the aerial platform;

[0024] FIG. 3 is a pictorial view of the terrain vehicle after disengagement from the aerial platform;

[0025] FIG. 4 is a pictorial view showing a detail of chassis of the terrain vehicle;

[0026] FIG. 5 is a pictorial view showing a detail of a coupling mechanism used in the aerial platform;

[0027] FIG. 6 is a pictorial view showing a partial detail of the terrain vehicle including connectors for manual latching by the coupling mechanism of the aerial platform;

[0028] FIG. 7 is a pictorial perspective view showing a flying car according to a second embodiment wherein the terrain vehicle is coupled to a rotate wing aerial platform;

[0029] FIG. 8 is a pictorial plan view showing a detail of the rotate wing aerial platform;

[0030] FIG. 9 is a pictorial side elevation showing the terrain vehicle prior to disengagement from the aerial platform; and

[0031] FIG. 10 is a partially exploded front elevation showing the terrain vehicle after disengagement from the aerial platform.

DETAILED DESCRIPTION OF EMBODIMENTS

[0032] In the following description of some embodiments, identical components that appear in more than one figure or that share similar functionality will be referenced by identical reference symbols.

[0033] FIG. 1 shows a flying vehicle 10 according to a first embodiment including an aerial platform 11 supporting wings 13, propellers 14 driven by a suitable thruster 15 coupled to a fuel supply shown schematically as 16. The aerial platform 11 also has a coupling mechanism 17 for coupling to a terrain vehicle 20. FIG. 2 shows a partial sectional view of the terrain vehicle 20 disengaged from the aerial platform 11.

[0034] The aerial platform 11 supports engines to create thrust, wings to create lift, control surfaces such as ailerons, rudder and height controls, an array of three undercarriages (primary and secondary landing gear having nose or tail wheels 21 and secondary wheels 22, respectively) to transport the weight during aircraft takeoff and landing, a servo control for the aircraft control surfaces and for the primary landing gear. The aerial platform 11 also has a chassis that is sufficiently massive to carry the combined weight of the aerial platform and the terrain vehicle and means for anchoring the terrain vehicle, which may serve as a cockpit or cabin. Additionally, a computer 23 in the aerial platform 11 shown schematically in FIG. 3 receives control signals from flight controllers installed in the cockpit (the ground assembly) and transfers these control signals to the control surfaces, throttles, steering main landing gear.

[0035] The terrain vehicle 20 hangs or is otherwise suspended from the aerial platform, for example by means of a pair of cable-operated latch mechanisms 25 that extend downward from a lower surface of the aerial platform shown in FIG. 5 each capable of being lowered until a pair of registration pins 27 engage complementary sockets in a mating connector 30 mounted on the roof of the terrain vehicle 20. Clasps 31 on opposite sides of the latch mechanism 25 are then retracted hydraulically or pneumatically via pistons 26 so as to close the clasps 31 from the open position shown in FIG. 5 whereby they engage recesses on the opposite sides of the connector 30. The latch mechanisms 25 are then retracted so as to lift the terrain vehicle 20 toward the fuselage of the aerial platform 11 as shown in FIG. 1. The height of the wingspan from the ground provides sufficient clearance for accommodating vehicles of varying heights, while the ability to raise and lower the latch mechanism 25 facilitates engagement with the roof connectors 30 regardless of the vehicle height. After landing, the latch mechanisms 25 are lowered via the pistons 26 so as to lower the vehicle to the ground, whereupon the clasps 31 are released in preparation for a ground phase. As shown in FIGS. 4 and 6, the vehicle has a chassis 35 comprising a matrix of welded struts 36 that extend to a reinforced roof 37 to which the connectors 30 are welded. This allows the vehicle to be coupled externally to the aerial platform and lifted or lowered by the connectors. When coupled to the aerial platform, the vehicle is transported thereby and thus flies with the aerial platform, the pilot and/or passengers being located in the terrain vehicle.

[0036] In some embodiments, the latch mechanism 25 includes controls that are automatically coupled to respective controls in the terrain vehicle 20, which then serves as a cockpit for allowing the motorist to pilot the airplane. Alternatively, the aerial platform 11 may be autonomous and be remotely controlled, thus obviating the need for the motorist to have a pilot license.

[0037] FIGS. 7 to 10 show a flying car 40 according to a second embodiment wherein the terrain vehicle 20 is coupled to a rotate wing aerial platform 41. The aerial platform 41 supports propellers 14 driven by a thruster 15 powered by a battery (constituting a fuel supply). The aerial platform 11 has latching mechanisms 25 as shown in FIG. 5 for coupling to a terrain vehicle 20. Also attached to the aerial platform 11 are adjustable legs 42 that serve as landing gear and each of which comprises at least two telescopic elements 43 that can be extended from an initial collapsed position shown in FIG. 7 during flight to an extended position shown in FIG. 9 on landing. Upon landing, the telescopic elements 43 are extended until the terrain vehicle 20 is lifted off the ground. The latch mechanisms 25 are then lowered via the pistons 26 so as to lower the vehicle to the ground and the clasps 31 are released in preparation for a ground phase.

[0038] The construction according to the invention also facilitates a business model whereby any motorist with a suitably modified terrain vehicle can hire an aerial platform to fly them out from an initial takeoff location to a landing site, where they can return the aerial platform and continue on their way by road. In those cases where the aerial platform is piloted, hiring the aerial platform effectively requires that the pilot also be hired unless the motorist has a pilot license. If the aerial platform is autonomous, no on-board pilot is required but obviously it must still be controlled although the manner in which this is done is known per se.

[0039] For those embodiments where the terrain vehicle 20 serves as the cockpit, it may be provided with a kit for assembly in the terrain vehicle customized for the assemblies installed on the aerial platform. Such a kit will include a wireless control for controlling the control surfaces, engines and thrusters. In addition, telemetry is provided in the vehicle to receive data from the various flight control systems of the aerial platform for monitoring air speed, engine control, state of the control surfaces, etc. like in any normal aircraft. Alternatively, the flight controls may generate control signals that are conveyed by wires to control elements of the airplane structure, each of the wires having respective segments in the terrain vehicle and the airplane structure, the respective segments being adapted for mutual coupling via respective connectors in the terrain vehicle and the airplane structure. The coupling is preferably achieved automatically when coupling the terrain vehicle to the aerial platform, but can also be manual via a cable having connectors at opposite ends that are coupled to appropriate connectors in the aerial platform.

[0040] The aerial platform 11 may be produced in different dimensions according to the engine thrust, vehicle size and lift capacity resulting from wing size and shape. In such manner, a manufacturer will be able to adapt virtually any existing model of vehicle for coupling to an appropriate aerial platform and convert it into a flying vehicle. Heavier terrain vehicles are simply adapted for a more massive aerial platform. In effect, this renders the aerial platform universal since theoretically it can be fitted to all vehicles of every conceivable size and weight.

[0041] Independent aircraft engines provide thrust for takeoff, flight and landing. These engines also provide the electrical power needed to operate the air control surfaces and the instruments and other items that are installed in the cockpit during the flight. To this end, voltage is fed to the vehicle controls from the aerial platform to operate the aeronautical and electrical systems during flight. This avoids the need to use the vehicle battery during flight, since the vehicle alternator does not function in flight mode unless the vehicle engine is operating. This is generally not necessary other than to provide power for heating and air conditioning of the vehicle if required. Fuel is fed to the aircraft engines from fuel tanks mounted on the aerial platform, like any normal aircraft. Alternatively, the engines may be electric motors powered by a battery.

[0042] The consumer is able to buy the terrain vehicle from any manufacturer that produces models adapted for connection to the aerial platform. The consumer can change cars without restriction, as long as they are adapted for connection to an aerial platform of a type and size that he possesses or is able to hire.

[0043] During flight the aerial platform functions as an unmanned aerial vehicle, except that the operator sits in the car and not on the ground. When the motorist pilots the aircraft, flight control is performed wirelessly, using Fly-By-Wire. The aircraft is controlled using controllers such as pedals, stick and throttles installed in the terrain vehicle. A basic physical connection point can also be installed by means of which the aerial platform can be flown from the terrain vehicle, even in an emergency situation where wireless communication between the vehicle and the aerial platform is lost.

[0044] The following table shows how control of the different functions of the aerial platform and the ground vehicle may be shared between the two vehicles:

TABLE-US-00001 TABLE I Component Used during: Location During flight During driving Air throttle Flight One for each engine: Connected by control Disconnected installed on right/left of cables to the aircraft cabin/cockpit computer system Stick Flight Cabin/cockpit 3-axis rigid structure Disconnected controls ailerons and altitude sticks Brake control using parachute or soft wing Glider control using rigid structure with glider wing Right pedal Flight/ground Beneath right foot in Rudder Vehicle engine pedal array facing the throttle two front seats in the cockpit/cabin Center pedal Ground Center of pedal array Disconnected Vehicle brake Left pedal Flight Left of pedal array Rudder Disconnected Gearbox Ground Center of cockpit/cabin Not used Gear control Flight Flight Double opposite right Indicates air system data Not used instrument and left seats in cockpit/ array cabin Vehicle Ground On dashboard at center Not used Indicates ground instrument of cockpit/ cabin system data array Steering wheel Ground Opposite left or right seat Disconnected Controls steering according to local requirements Ground Taxi, takeoff To left of left front seat Controls the wheel of steering wheel and landing of cockpit/ cabin primary landing gear of aerial runs platform

[0045] It will be appreciated that changes may be made to the construction of the aerial platform without departing from the scope of the claims. For example, although the invention has been described with particular reference to a fixed-wing plane, the aerial platform may be a suitably modified rotate-wing adapted for coupling to the terrain vehicle. The manner of coupling is not limited to what is described, it being only important that the coupling be releasable and secure and operate to couple the terrain vehicle external to the lower surface of the aerial platform. In the embodiment as described, the terrain vehicle is supported from its roof since this provides easy access without the need for providing brackets that allow connection to the chassis from below. But no limitation is thereby implied. Likewise, the terrain vehicle can be a motorcycle that is provided with a bracket for suspending from the aerial platform and which has a connector that couples to the computer on board the aerial platform so as to allow the motor cycle to double as the aircraft cockpit. In this case, the handlebar may serve to control the steering of the aircraft landing gear through the coupling. Other changes will likewise be apparent to those skilled in the art.

[0046] It should also be noted that features that are described with reference to one or more embodiments are described by way of example rather than by way of limitation to those embodiments. Thus, unless stated otherwise or unless particular combinations are clearly inadmissible, optional features that are described with reference to only some embodiments are assumed to be likewise applicable to all other embodiments also.

[0047] The description of the above embodiments is not intended to be limiting, the scope of protection being provided only by the appended claims.