Computerized electric cable powered/guided aircraft transportation/power/communication system

• US 5,653,174 A
• Filed: 07/20/1995
• Issued: 08/05/1997
• Est. Priority Date: 07/20/1995
• Status: Expired due to Fees

• Current Assignee: William J. Halus
• Original Assignee: William J. Halus
• Inventors: Halus, William J.
• Primary Examiner(s): Le, Mark T.
• Application Number:
  US08/504,286
• Time in Patent Office: 747 Days
• Field of Search: 104/123, 104/124, 104/112, 104/125, 104/126, 104/281, 104/282, 104/289, 104/292, 104/53, 104/88.02, 104/88.03, 104/89, 104/286, 244/901, 244/173, 105/148, 105/149.1
• US Class Current: 104/124
• CPC Class Codes: B61B 13/08 Sliding or levitation systems vehicles with air cushions between rails and vehicles B60V3/04
• CPC Class Codes: B61C 11/06 tractive effort applied or supplied by aerodynamic force or fluid reaction, e.g. air-screws and jet or rocket propulsion
• CPC Class Codes: E01B 25/22 Tracks for railways with the vehicle suspended from rigid supporting rails
• CPC Class Codes: H02K 41/02 Linear motors; Sectional motors

Abstract

Aircraft with full flight capability are connected to structural cables by an electrically powered drive element traveling inside the structural cables. Electricity distribution cables, part of a power distribution grid, connect to the structural cable along its length and provide power to the drive element. A linear series of annular electromagnets in the structural cable encircle a linear array of circular electromagnets in the drive element. A centralized computer controls a constantly changing phase shift in the electromagnets along the structural cable causing the drive element electromagnets to move through the structural cable without contacting the structural cable. The aircraft is connected by cables or rods to the drive elements. Retractable delta wings, an airfoil body, and a controlled angle of attack create lift maintaining the aircraft in flight as the drive element moves through the structural cable. An onboard computer in communication with the central computer controls the drive element electromagnets, the lift creating elements, trim tabs on vertical and horizontal stabilizers, and a number of spoilers to maintain a precise flight path. Fiber optic cables, part of a communication network grid, are attached along the length of the structural cable in communication with an onboard long distance communication system. The structural cables, fiber optic cables, and electricity distribution cables all connect to buildings providing a door-to-door transportation, communication, and nationwide power distribution system. This smart transportation system of the twenty-first century is known as the Aerial SmarTrans (TM). This is the high tech vehicle that will construct and travel the information super highway, thus invigorating and renewing American civilization. It will give the American people great pleasure and pride to pay and ride smart transportation for the next century.

Claims

1. A transportation system comprising:

an elongated member, having means for conducting electricity, extending along a travel route;

means for supporting the elongated member above ground level;

at least one drive element which travels along the elongated member;

an electrically activated means for causing the at least one drive element to travel along the elongated member, which electrically activated means draws electric power from the means for conducting electricity;

an aircraft connected to the at least one drive element, the aircraft having means for flying, the aircraft held in flight by movement of the at least one drive element along the elongated member;

a computerized means for controlling the flying means;

wherein the means for flying comprises means for creating lift, at least one horizontal stabilizer, at least one vertical stabilizer, a plurality of trim, and a plurality of spoilers extending from the aircraft and the computerized controlling means is programmed to operate as a fly-by-wire autopilot, controlling the drive element and the means for flying maintaining the aircraft in a precise flight pattern out of contact with the elongated member;

wherein the elongated member comprises a structural cable having a central opening and an interconnected bottom slot through the elongated member along its length, the at least one drive element comprises at least one linear array of first electromagnets fitting within the central opening, and the means for moving the at least one drive element comprises a series of second electromagnets encircling the central opening along its length and means for creating a constantly changing phase shift along the second electromagnets electrically connected therewith, so that creating a constantly changing phase shift along the second electromagnets attracts the first electromagnets drawing the first electromagnets along the length of the structural cable, the first electromagnets remaining spaced apart from the second electromagnets so that a linear electromagnetic motor/generator is created by the interaction of the first and second electromagnets.

2. The transportation system of claim 1 wherein the means for creating lift comprises retractable delta wings reversibly extensible from two opposing sides of the aircraft.

3. The transportation system of claim 2 wherein the means for creating lift further comprises an airfoil contour of the aircraft so that the aircraft creates lift.

4. The transportation system of claim 3 wherein the means for creating lift further comprises means for changing the angle of attack of the aircraft to create lift.

5. The transportation system of claim 1 wherein the at least one drive element further comprises an elongated support extending from each of the at least one linear arrays of first electromagnets through the slot interconnecting the at least one drive element with the aircraft and the elongated support further comprises at least one wire for conducting electricity from the drive element to the aircraft.

6. The transportation system of claim 5 wherein the elongated support comprises a support cable adjustable in length, so that the aircraft can be raised and lowered from the horizontal structural cable.

7. The transportation system of claim 1 wherein the means for conducting electricity comprises an electricity distribution cable attached to the structural cable along its length, the electric distribution cable connected into an electricity distribution grid so that acceleration of the aircraft draws electric power from the electricity distribution grid and deceleration of the aircraft adds electric power to the electricity distribution grid, creating highly efficient use of energy.

8. The transportation system of claim 7 further comprising a fiber optic cable attached to the structural cable along its length and means for long distance digital audiovisual communicating having a radio wave transmitter and receiver within the aircraft, so that the means for long distance communicating interacts with the fiber optic cable by radio waves, the fiber optic cable connected via satellites to a global digital audiovisual communication grid.

9. The transportation system of claim 8 wherein the fiber optic cable and the electric distribution cable both connect to a building, the aircraft is configured to fit within a room in the building, the computerized means for controlling the flying means is programmed to be usable within the room in the building for other uses, and the means for long distance digital audiovisual communicating is configured to be usable within the room in the building.

10. The transportation system of claim 1 further comprising a central mainframe super computer electrically interconnected with the means for creating a constantly changing phase shift along the second electromagnets and electrically interconnected with the computerized means for controlling the flying means, so that movement of a number of aircraft along the structural cable is controlled by the central mainframe super computer and the computerized means for controlling the flying means can communicate routing information between the aircraft and the central computer.

11. The transportation system of claim 10 wherein the aircraft is controlled by the central computer and carries only cargo.

12. The transportation system of claim 11 wherein a plurality of aircraft are constantly moving on a plurality of structural cables, the plurality of aircraft carrying missiles, thereby creating an instant response ground-based mobile missile transportation system.

13. The transportation system of claim 1 further comprising an auxiliary electric motor connected to the at least one drive element having mechanical means for moving the at least one drive element along the structural cable, a battery in the aircraft for powering the electric motor, and a means for recharging the battery.

14. The transportation system of claim 13 further comprising access and egress branch cables connected with the structural cable, the branch cables being stronger than the structural cable for supporting the aircraft hanging from the branch cables, the branch cables sloping to position the aircraft at ground level for loading and unloading the aircraft so that the mechanical means for moving the at least one drive element engages the branch cables to move the aircraft along the branch cables slowing to a stop on the egress branch cables and accelerating from stop to flying speed on the access branch cable.

15. The transportation system of claim 13 further comprising solar panels on the aircraft for charging the battery.

16. The transportation system of claim 1 further comprising at least one additional structural cable separated from and parallel to the structural cable so that a wide-bodied aircraft is connected to both structural cables by the at least one drive element to each structural cable so that the wide-bodied aircraft is capable of carrying heavy cargo, and the wide-bodied aircraft has a means for docking so that the aircraft traveling along a single structural cable may dock with the wide-bodied aircraft, while at full speed for loading and unloading individual passengers for selected destinations.

17. The transportation system of claim 1 wherein the means for supporting the structural cable comprises a series of vertical posts in the ground having means for supporting the structural cable along the top of the structural cable.

18. The transportation system of claim 1 wherein the at least one drive element further comprises a plurality of rolling means spaced around the at least one drive element so that the rolling means will contact the structural cable should the electromagnets fail to space the at least one drive element from the structural cable.