Nonlinear electromagnetic propulsion system and method

• US 5,142,861 A
• Filed: 04/26/1991
• Issued: 09/01/1992
• Est. Priority Date: 04/26/1991
• Status: Expired due to Term

• Current Assignee: David J. Hall, Davis, Charles E., Peter M. Ranon, Rex L. Schlicher, Steven M. Rinaldi
• Original Assignee: David J. Hall, Davis, Charles E., Peter M. Ranon, Rex L. Schlicher, Steven M. Rinaldi
• Inventors: Davis, Charles E., Hall, David J., Ranon, Peter M., Schlicher, Rex L., Rinaldi, Steven M.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US07/691,889
• Time in Patent Office: 494 Days
• Field of Search: 60/200.1, 60/203.1, 60/204, 315/34, 343/867, 343/896
• US Class Current: 60/203.1
• CPC Class Codes: F03H 3/00 Use of photons to produce a reactive propulsive thrust
• CPC Class Codes: H01Q 7/00 Loop antennas with a substantially uniform current distribution around the loop and having a directional radiation pattern in a plane perpendicular to the plane of the loop
• CPC Class Codes: H02N 11/006 Motors

Abstract

An electromagnetic propulsion system based on an extremely low frequency (elf) radiating antenna structure driven by a matched high current pulsed power supply is described. The elf antenna structure resembles a modified three dimensional multiple-turn loop antenna whose geometry is optimized for the production of reaction thrust rather than the radiation of electromagnetic energy into space. The antenna structure is current driven rather than voltage drive. Rigid three dimensional geometric asymmetry, made up of flat electrical conductors that form a partially closed volume in the loop antenna structure, trap magnetic flux thereby causing a magnetic field density gradient along a single axis. This magnetic field density gradient then causes an imbalance in the magneto- mechanical forces that normally result from the interactions of the loop antenna'"'"'s internal magnetic field with the current in the conductors of the loop antenna structure, as described by the Lorentz Force Law. The pulsed power supply is designed to provide the proper waveform to the antenna structure at an impedance matching the load impedance of the antenna. The rise time and shape of the input current waveform is crucial to maximizing the production of reaction thrust. Input voltage is at a nominal value sufficient to allow the desired high input current.

Claims

1. A nonlinear electromagnetic propulsion system, comprising antenna means driven by current pulse generating means coupled to a prime power source, with transmission line means coupling the current pulse generating means to the antenna means;

wherein the current pulse generating means includes means for providing a sawtooth wave having a relatively steep leading edge compared to the trailing edge;

wherein the antenna means comprises a three dimensional laminated geometry having an extremely low frequency (elf) radiating antenna structure in the form of a three dimensional asymmetric multiple-turn loop antenna whose geometry is optimized for the production of reaction thrust rather than the radiation of electromagnetic energy into space, with rigid three dimensional geometric asymmetry, made up of flat electrical conductors that form a partially closed volume in the loop antenna structure, which trap magnetic flux thereby causing a magnetic field density gradient along a single axis, wherein the magnetic field density gradient causes an imbalance in the magneto-mechanical forces that normally result from the interactions of the loop antenna'"'"'s internal magnetic field with the current in the conductors of the loop antenna structure, as described by the Lorentz Force Law;

wherein the antenna means includes a plurality of return bundles and a center return conductor.

2. A nonlinear electromagnetic propulsion system according to claim 1, wherein the antenna structure comprises a partially closed conical volume with a ferromagnetic flux nozzle near an apex thereof.

3. A nonlinear electromagnetic propulsion system according to claim 1, wherein the antenna structure comprises a cylindrical volume.

4. A nonlinear electromagnetic propulsion system according to claim 1, wherein the antenna structure comprises a hemispherical volume.

5. A nonlinear electromagnetic propulsion system according to claim 1, wherein the antenna structure comprises hybrid structure having a conical volume followed by a cylindrical volume.

6. A nonlinear electromagnetic propulsion system according to claim 1, wherein the antenna structure comprises hybrid structure having a hemispherical volume followed by a cylindrical volume.

7. A nonlinear electromagnetic propulsion system according to claim 1, wherein the prime power source is a DC source, and th current pulse generating means comprises a DC to AC inverter having an input coupled to the prime power source, and an output coupled via a matching transformer and an SCR switch to the transmission line means, SCR trigger means coupled to a control input of the SCR switch, and frequency control means coupled the inverter and to the SCR trigger means for providing frequency control to generate the sawtooth waveform at an extremely low frequency.

8. A nonlinear electromagnetic propulsion system according to claim 1, wherein the prime power source is a AC source, and the current pulse generating means comprises a power frequency changer having an input coupled to the prime power source, and an output coupled via a matching transformer and an SCR switch to the transmission line means, SCR trigger means coupled to a control input of the SCR switch, and frequency control means coupled to the power frequency changer and to the SCR trigger means for providing frequency control to generate the sawtooth waveform at an extremely low frequency.

9. A nonlinear electromagnetic propulsion system according to claim 1, wherein the prime power source is a DC source, and the current pulse generating means comprises a current switch having an input coupled to the prime power source, and an output coupled via a pulse transformer to the transmission line means, and switch control means coupled to the current switch, wherein the switch control means includes repetition rate control means, for providing frequency control to generate the sawtooth waveform at an extremely low frequency.

10. A nonlinear electromagnetic propulsion system according to claim 9, wherein the current switch comprises a mechanical relay.

11. A nonlinear electromagnetic propulsion system according to claim 9, wherein the current switch comprises a rotating switch, and the switch control means comprises a motor.

12. A nonlinear electromagnetic propulsion system according to claim 9, wherein the current switch comprises a switching transistor.

13. A nonlinear electromagnetic propulsion system according to claim 9, wherein the current switch comprises an SCR.

14. A nonlinear electromagnetic propulsion system according to claim 1, wherein the prime power source is a high current DC source, and the current pulse generating means comprises an on-off switch having an input coupled to the prime power source, and an output coupled via a current limiting resistor to the transmission line means, and switch control means coupled to the on-off switch for providing frequency control to generate the sawtooth waveform at an extremely low frequency.