FIRE SUPPRESSION SYSTEMS AND METHODS

• US 20100059236A1
• Filed: 09/10/2009
• Published: 03/11/2010
• Est. Priority Date: 09/11/2008
• Status: Abandoned Application

• Current Assignee: Integrated Systems Excellence Corporation
• Original Assignee: Integrated Systems Excellence Corporation
• Inventors: Yee, Francis
• Application Number:
  US12/556,665
• Publication Number:
  US 20100059236A1
• Time in Patent Office: Days
• US Class Current: 169/46
• CPC Class Codes: A62C 2/00 Fire prevention or containment A62C3/00 takes precedence; flame traps A62C4/00
• CPC Class Codes: A62C 99/009 Methods or equipment not provided for in groups A62C99/0009 - A62C99/0081

Abstract

Tools and techniques for suppressing fires. Such tools might transmit a signal that generates one or more waves (which might be mechanical waves, electromagnetic waves, and/or the like) that is sufficient to disrupt the relationship between the electrons in a fire and the ionized nuclei to which those electrons are attracted. The resulting repulsion (between the nuclei and/or the electrons) that form the plasma of the fire can serve to disperse the plasma, thereby suppressing the fire.

Claims

1. A method of suppressing fires, the method comprising:

identifying a fire comprising plasma; and

transmitting a signal proximate to the fire, wherein the signal is sufficient to disperse at least a portion of the plasma.

2. The method of claim 1, wherein the signal has a plasma dispersion frequency.

3. The method of claim 2, further comprising:

analyzing the plasma to identify a plasma frequency of the plasma; and

calculating a plasma dispersion frequency for the signal, based at least in part on the identified plasma frequency.

4. The method of claim 3, wherein calculating a plasma dispersion frequency for the signal comprises calculating a plasma dispersion frequency for the signal based at least in part on the identified plasma frequency and an orientation of a magnetic field of the plasma relative to the signal.

5. The method of claim 4, wherein transmitting the signal comprises transmitting the signal in a direction that is substantially parallel to the orientation of the magnetic field of the plasma.

6. The method of claim 4, wherein transmitting the signal comprises transmitting the signal in a direction that is substantially perpendicular to the orientation of the magnetic field of the plasma.

7. The method of claim 1, wherein transmitting a signal proximate to the fire comprises generating a set of one or more compression waves proximate to the fire, wherein the one or more compression waves collectively are sufficient to disperse at least a portion of the plasma.

8. The method of claim 7, further comprising releasing an endothermic substance in a rarefaction region of the one or more compression waves.

9. The method of claim 7, wherein generating one or more compression waves comprises:

generating a first set of one or more compression waves each having a first wave shape;

analyzing an amount of plasma dispersion caused by the first set of one or more compression waves;

selecting a second wave shape, based at least in part on an analysis of the amount of plasma dispersion caused by the first set of one or more compression waves; and

generating a second set of one or more compression waves having the second wave shape.

10. The method of claim 9, wherein the second wave shape produces a fast compression effect on the plasma.

11. The method of claim 9, wherein the first wave shape is defined by a first frequency and a first compression region, and wherein the second wave shape is defined by a second frequency and a second compression region.

12. The method of claim 11, wherein the first frequency and the second frequency are the same frequency.

13. The method of claim 11, wherein the first compression region and the second compression region are the same compression region.

14. The method of claim 9, wherein analyzing an amount of plasma dispersion comprises analyzing the amount of plasma dispersion using a digital signal processing technique selected from the group consisting of a double transform analysis, a correlation-phase velocity analysis, a fixed-probe correlation analysis, and a local wavenumber-frequency spectra analysis.

15. The method of claim 7, wherein generating a set of one or more compression waves comprises generating a set of one or more longitudinal compression waves.

16. The method of claim 7, wherein generating a set of one or more compression waves comprises generating a set of one or more pulsed transverse waves.

17. The method of claim 7, wherein generating a set of one or more compression waves comprises generating a set of one or more acoustic waves.

18. The method of claim 7, wherein generating a set of one or more compression waves comprises generating a set of one or more compression waves with a Doppler radar system.

19. The method of claim 7, wherein generating a set of one or more compression waves comprises generating a set of one or more compression waves with a phased array radar system.

20. The method of claim 19, wherein transmitting a signal comprises transmitting a plurality of signals, and wherein generating a set of one or more compression waves comprises beamforming a composite signal from the plurality of signals.

21. The method of claim 7, wherein generating a set of one or more compression waves comprises generating a set of one or more compression waves with a laser.

22. The method of claim 7, wherein identifying a fire comprises identifying a fuel source of the fire.

23. The method of claim 22, further comprising:

selecting a wave shape for the one or more compression waves, based at least in part on an ionization energy of the fuel source of the fire, wherein the selected wave shape produces a fast compression effect on the plasma;

wherein generating a set of one or more compression waves comprises wave shaping the set of one or more compression waves to have the selected wave shape.

24. The method of claim 1, wherein generating a set of one or more compression waves proximate to the fire comprises:

generating a sonic boom proximate to the fire.

25. The method of claim 24, wherein generating a sonic boom proximate to the fire comprises flying one or more aircraft, at a supersonic velocity, near the fire.

26. The method of claim 1, further comprising:

grounding a plurality of electrons from the plasma.

27. The method of claim 26, wherein grounding a plurality of electrons comprises grounding a plurality of electrons with a device selected from the group consisting of a Penning Trap, a Paul Trap, and a Malmberg-Penning Trap.

28. The method of claim 1, further comprising:

applying secondary compression to the fire.

29. The method of claim 28, wherein the secondary compression comprises an airbag.

30. The method of claim 1, wherein the fire is a wildfire.

31. The method of claim 1, wherein the fire is inside a building.

32. The method of claim 1, wherein the fire is inside a vehicle, an aircraft, a watercraft, or a spacecraft.

33. The method of claim 1, wherein the fire is generated by an explosion.

34. The method of claim 34, wherein the one or more compression waves collectively are sufficient to mitigate an shock wave created by the explosion.

35. The method of claim 34, wherein the one or more compression waves collectively are sufficient to reduce a velocity of at least some shrapnel produced by the explosion.

36. A system for suppressing a fire comprising plasma, the system comprising:

a signal generator for transmitting a signal proximate to the fire, wherein the signal is sufficient to disperse at least a portion of the plasma;

an active gain control circuit, in communication with the signal generator, for adjusting one or more characteristics of the signal; and

a computer system in communication with the active gain control circuit, the computer system comprising a processor and a set of instructions executable by the processor to calculate values for the one or more characteristics of the signal.

37. The system of claim 36, wherein the processor is a digital signal processor.

38. The system of claim 36, further comprising a probe for measuring one or more characteristics of the plasma.

39. The system of claim 38, wherein the probe comprises a thermocouple for sensing a temperature of the plasma.

40. The system of claim 38, wherein the probe comprises a frequency sensor for sensing a plasma frequency of the plasma.

41. The system of claim 38, wherein the set of instructions comprises:

instructions for calculating a plasma dispersion frequency for the fire, based at least in part on the one or more characteristics of the plasma; and

instructions to cause the active gain control circuit to adjust the frequency of the signal to the calculated plasma dispersion frequency.

42. The system of claim 36, wherein the signal generator comprises a compression wave generator for generating a set of one or more compression waves, wherein the one or more compression waves collectively are sufficient to disperse at least a portion of the plasma.

43. The system of claim 42, wherein the compression wave generator comprises one or more acoustic speakers.

44. The system of claim 42, wherein the compression wave generator comprises a Doppler radar system.

45. The system of claim 42, wherein the compression wave generator comprises a phased array radar system.

46. The system of claim 42, wherein the compression wave generator comprises a laser system.

47. The system of claim 46, wherein the laser system is an infrared pulsed laser system.

48. The system of claim 46, wherein the laser system comprise a carbon dioxide laser and a nitrogen laser.

49. The system of claim 42, wherein the set of instructions comprises:

instructions for calculating a wave shape for the one or more compression waves, based at least in part on an ionization energy of the fuel source of the fire, wherein the calculated wave shape produces a fast compression effect on the plasma.

50. The system of claim 42, wherein the set of one or more compression waves comprises a first set of one or more compression waves, each having a first wave shape, and a second set of one or more compression waves, and wherein the set of instructions comprises:

instructions for analyzing an amount of plasma dispersion caused by the first set of one or more compression waves; and

instructions for selecting a second wave shape for the second set of one or more compression waves, based at least in part on an analysis of the amount of plasma dispersion caused by the first set of one or more compression waves.

51. The system of claim 36, wherein the signal generator is mounted on the exterior of vehicle.

52. The system of claim 51, wherein the vehicle is an aircraft.

53. The system of claim 36, further comprising a secondary compression device.

54. The system of claim 53, wherein the secondary compression device comprises an airbag system.

55. The system of claim 36, further an electron grounding device for grounding electrons from the plasma.

56. The system of claim 55, wherein the electron grounding device comprises a device selected from the group consisting of a Penning Trap, a Paul Trap, and a Malmberg-Penning Trap.