Electron beam directed energy device and methods of using same

• US 7,282,727 B2
• Filed: 07/22/2005
• Issued: 10/16/2007
• Est. Priority Date: 07/26/2004
• Status: Expired due to Fees

• Current Assignee: Michael W. Retsky
• Original Assignee: Michael W. Retsky
• Inventors: Retsky, Michael W.
• Primary Examiner(s): Wells, Nikita
• Assistant Examiner(s): Hashmi, Zia R.
• Application Number:
  US11/187,519
• Publication Number:
  US 20070029497A1
• Time in Patent Office: 816 Days
• Field of Search: None
• US Class Current: 250/492.3
• CPC Class Codes: F41H 11/02 Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems cartridges or missiles for producing smoke or for dispensing radar chaff or infrared material F42B5/15, F42B12/48, F42B12/70; informative reference: details of radar or sonar systems G01S7/00; jamming or electronic countermeasures G01S7/38, G01S7/495, H04K3/00
• CPC Class Codes: F41H 11/12 Means for clearing land minefields; Systems specially adapted for detection of landmines
• CPC Class Codes: F41H 11/136 Magnetic, electromagnetic, acoustic or radiation systems, e.g. ground penetrating radars or metal-detectors
• CPC Class Codes: F41H 13/00 Means of attack or defence not otherwise provided for details of radar or sonar systems G01S7/00
• CPC Class Codes: F41H 13/0043 Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target
• CPC Class Codes: F42B 33/065 by laser means
• CPC Class Codes: H01J 3/02 Electron guns
• CPC Class Codes: H01J 3/026 Eliminating deleterious effects due to thermal effects, electric or magnetic field H01J3/021 - H01J3/025 take precedence
• CPC Class Codes: H01J 3/14 Arrangements for focusing or reflecting ray or beam H01J3/02, H01J3/04 take precedence

Abstract

A method and apparatus is disclosed for an electron beam directed energy device. The device consists of an electron gun with one or more electron beams. The device includes one or more accelerating plates with holes aligned for beam passage. The plates may be flat or preferably shaped to direct each electron beam to exit the electron gun at a predetermined orientation. In one preferred application, the device is located in outer space with individual beams that are directed to focus at a distant target to be used to impact and destroy missiles. The aimings of the separate beams are designed to overcome Coulomb repulsion. A method is also presented for directing the beams to a target considering the variable terrestrial magnetic field. In another preferred application, the electron beam is directed into the ground to produce a subsurface x-ray source to locate and/or destroy buried or otherwise hidden objects including explosive devices.

Claims

1. A directed energy device comprising:

an electron gun generating a plurality of electron beams, said plurality of electron beams disposed such that their beam axes are oriented in a pre-configured direction and separation to substantially overcome Coulomb repulsion at a point greater than 100 kilometers distant;

an electron accelerator positioned after the electron gun consisting of a plurality of sequential conductive shaped plates, each plate having at least one aperture per electron beam where the apertures are positioned at the respective beam'"'"'s axis, and the shape of the plates is essentially normal to the electron beams, the approximate spacing of the plates from adjacent plates is larger than the electrical breakdown limit; and

means for applying voltages to each conductive plate relative to other conductive plates.

2. The directed energy device of claim 1 having a beam envelope that exceeds 1 m in any diameter.

3. The directed energy device of claim 1 wherein the device is used to direct energy to a target.

4. The directed energy device of claim 1 wherein the device is used as a weapon.

5. The directed energy device of claim 1 wherein the device is directed to targets above the atmosphere.

6. The directed energy device of claim 1 wherein the device is directed to targets within the atmosphere.

7. The directed energy device of claim 1 in which the pre-configured direction and separation of the beams is designed by considering the other charged particles to be a continuum of charges.

8. The directed energy device of claim 1 in which the pre-configured direction and separation of the beams is designed by considering the other charged particles to be discrete charges.

9. The directed energy device of claim 1 wherein the means for applying the separate plate voltages comprises an energy storage device.

10. The directed energy device of claim 9 wherein the energy storage device comprises at least one flywheel.

11. The directed energy device of claim 1 disposed in an environment defining a pressure of less than 10⁻

5 torr.

12. The directed energy device of claim 1 wherein the plurality of particle beams are disposed such that the beams are convergent to a point at a specified distance greater than 100 km from the exit of the device.

13. The directed energy device of claim 1 wherein the electron gun produces an energy of over 0.1 GV beam voltage and over 100 amps total beam current with a beam landing of less than 50 cm diameter at a distance greater than 100 km.

14. The directed energy device of claim 1 wherein the placement of the apertures in the conductive plates corresponds to trajectories that will mostly direct the electrons to land at a target within a landing diameter.

15. The directed energy device of claim 1 having at least one high voltage capacitor between at least one pair of conductive plates.

16. The directed energy device of claim 1 having voltage provided by at least one high voltage power supply between at least two conductive plates.

17. The directed energy device of claim 1 wherein some electron beams originate at different voltages to provide different electron energies.

18. The directed energy device of claim 1 wherein at least one charged plate has a conductive surface on a nonconductive substrate.

19. The directed energy device of claim 1 wherein at least one conductive plate is foldable for transportation into space.

20. The directed energy device of claim 1 wherein at least one conductive plate can be rolled up for transportation into space.

21. The directed energy device of claim 1 wherein power provided for at least one conductive plate by using stored rotational energy in at least one flywheel.

22. The directed energy device of claim 1 further comprising means for jettisoning an approximately equal positive charge as the electron beam carries away.

23. The directed energy device of claim 1 having at least two conductive plates mechanically aligned and attached one to another using at least one high voltage insulator.

24. The directed energy device of claim 1 wherein at least one conductive plate is free to move.

25. The directed energy device of claim 24 wherein at least one conductive plate is free to move with motion provided by gas jets.

26. The directed energy device of claim 24 wherein the at least one conductive plate alignment is measured by at least one laser beam directed down alignment apertures in at least one conductive plate.

27. The directed energy device of claim 24 wherein the at least one conductive plate alignment is measured by at least two laser beams directed down different size apertures for separate coarse and fine alignment.

28. The directed energy device of claim 1 wherein conductive plate-to-plate spacing is approximately equal between all plates.

29. The directed energy device of claim 1 wherein conductive plate-to-plate spacing is larger than the minimum spacing limited by breakdown electric field strength.

30. The directed energy device of claim 1 wherein steering of the beam after it exits from the last conductive plate uses magnetic fields.

31. The directed energy device of claim 1 wherein steering of the beam after it exits from the last conductive plate uses electric fields.

32. The directed energy device of claim 1 wherein the plurality of electron beams comprises at least 10 charged particle beams and at least 100 sequential conductive shaped plates, each plate being at least 1 meter in a diameter.

33. The directed energy device of claim 1 wherein positive charges are removed from the device by charging capacitors and jettisoning the positive plates in conjunction with electron beam operation.

34. The directed energy device of claim 1 further comprising an array of test targets appropriately positioned in space and periodically hit with a lower than 100 amp current but full-voltage beam for calibration of aiming.

35. The directed energy device of claim 1 further comprising an array of test targets appropriately positioned in space and periodically hit with a duration less than 0.1 msec but full-voltage beam for calibration of aiming.

36. The directed energy device of claim 1 wherein an array of magnetic field measuring devices are appropriately positioned to provide information on the local magnetic field for determining beam aiming to hit a target.

37. The directed energy device of claim 1 enclosed within a container that is evacuated by at least one vacuum pump.

38. The directed energy device of claim 1 wherein steering of the beam after it exits from the last conductive plate uses electric fields and magnetic fields.

39. The directed energy device of claim 1 wherein the device is used as an electron beam directed energy weapon.

40. The directed energy device of claim 1 wherein the device is used to destroy targets.

41. The directed energy device of claim 1 supported by a balloon within the earth'"'"'s atmosphere.

42. The directed energy device of claim 1 disposed in orbit above the earth'"'"'s atmosphere.

43. The directed energy device of claim 1 disposed in geosynchronous orbit above the earth'"'"'s atmosphere.

44. The directed energy device of claim 1 carried on an airplane within the earth'"'"'s atmosphere.

45. A directed energy device comprising:

an electron gun having at least one beam of electrons, said at least one beam of electrons disposed such that at least one beam axis is oriented towards the surface of the earth and is located at a position of up to 200 meters above the surface of the earth;

an electron accelerator, the electron accelerator operable to energize the electrons to between 10 MeV and 100 MeV; and

wherein the directed energy device is operable to deposit energy subsurface.

46. The directed energy device of claim 45 used to generate x-rays directed from beneath the surface of the earth.

47. The directed energy device of claim 45 used to provide back-illumination for detecting concealed explosives.

48. The directed energy device of claim 45 wherein the beam is scanned to provide multiple images for detecting concealed explosives.

49. The directed energy device of claim 45 wherein image shapes that do not correspond to known landmine shapes are rejected.

50. The directed energy device of claim 45 further comprising x-ray absorbing grids to attenuate scattered radiation.

51. The directed energy device of claim 45 further comprising x-ray absorbing grids to attenuate unscattered radiation.

52. The directed energy device of claim 45 used to locate valuable buried items.

53. The directed energy device of claim 45 further comprising a plasma valve to allow beam exit from vacuum to atmosphere.

54. The directed energy device of claim 45 wherein the device is used to destroy landmines.

55. The directed energy device of claim 45 wherein excess charge is jettisoned as the device operates.

56. The directed energy device of claim 45 further comprising a membrane window to allow beam exit from vacuum to atmosphere.

57. The directed energy device of claim 45 wherein the at least one beam of electrons are aimed toward a point 10-15 cm below the surface.

58. A method for impacting ballistic missiles using a directed energy device, comprising the steps of:

generating a plurality of electron beams, said plurality of electron beams disposed such that their beam axes are oriented in a pre-configured direction and separation to substantially overcome Coulomb repulsion at a point greater than 100 km distant;

positioning an electron accelerator consisting of a plurality of sequential conductive shaped plates, each conductive shaped plate containing at least one aperture per electron beam, wherein the apertures are positioned at the respective beam'"'"'s axis, and the shape of the conductive shaped plates being essentially normal to the electron beams, the approximate spacing of the plates from adjacent plates is larger than the electrical breakdown limit; and

applying voltages to each of the plurality of conductive shaped plates relative to the other of the plurality of conductive shaped plates.

59. A method for detecting landmines using a directed energy device, comprising the steps of:

providing an electron gun having at least one beam of electrons, said at least one beam of electrons disposed such that at least one beam axis is oriented towards the surface of the earth, the position of the electron gun being located at a position of up to 200 meters above the surface of the earth;

providing an electron accelerator operable to energize the electrons to between 10 MeV and 100 MeV; and

depositing the energy from the electrons at or below the surface of the earth.