Method and apparatus for shockwave attenuation

• US 8,806,945 B2
• Filed: 11/22/2011
• Issued: 08/19/2014
• Est. Priority Date: 11/22/2011
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Tillotson, Brian J., Loudiana, Michael A.
• Primary Examiner(s): SAINT SURIN, JACQUES M
• Application Number:
  US13/302,614
• Publication Number:
  US 20130125656A1
• Time in Patent Office: 1,001 Days
• Field of Search: 735/99, 86/50
• US Class Current: 73/599
• 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 5/007 Reactive armour; Dynamic armour
• CPC Class Codes: F42D 5/045 Detonation-wave absorbing or damping means

Abstract

A method and apparatus for attenuating a shockwave propagating through a first medium. The method may include the steps of detecting a shockwave-producing event, determining a direction and distance of the shockwave relative to a defended target, and interposing a second medium between the shockwave and a defended object. The second medium is different from the first medium and the shockwave is attenuated in energy as it passes through the second medium prior to reaching the defended object.

Claims

1. A method for attenuating a shockwave propagating in a first medium, comprising:

detecting a shockwave-producing event;

determining a direction of a shockwave produced by said event relative to a defended object; and

interposing a second medium different from said first medium between said shockwave and said defended object such that said shockwave passes through said second medium and is attenuated in energy thereby prior to reaching said defended object.

2. The method of claim 1 wherein said second medium comprises a gas.

3. The method of claim 2 wherein said gas comprises a gas that differs from said first medium in at least one of composition, density, and temperature.

4. The method of claim 3 wherein said interposing step includes delivering said gas by using at least one projectile.

5. The method of claim 4 wherein said delivering step includes opening a valve in said projectile to dissipate said gas.

6. The method of claim 1 wherein said second medium comprises a reaction product.

7. The method of claim 6 wherein said interposing step includes igniting a chemical reaction in a projectile to produce said reaction product.

8. The method of claim 7 wherein said reaction product comprises a hot gas.

9. An apparatus for attenuating a shockwave propagating in a first medium, the apparatus comprising:

a sensor for detecting an event producing said shockwave, and determining a direction of said shockwave relative to a defended object;

a projectile having contents forming a second medium, different from said first medium, when released from said projectile; and

a launcher in communication with said sensor for launching said projectile to release said second medium between said shockwave and said defended object, whereby said second medium is impacted by said shockwave and thereby attenuates energy of said shockwave prior to said shockwave reaching said defended object.

10. The apparatus of claim 9 wherein said apparatus further comprises a plurality of said launchers, each of said launchers containing at least one of said projectiles therein.

11. The apparatus of claim 10 wherein said sensor includes a control for detecting an azimuthal angle of said shockwave source relative to said defended object and an output signal of said sensor contains information related to said azimuthal angle.

12. The apparatus of claim 11 wherein said apparatus further comprises an interpreter for firing one of said plurality of launchers in response to said signal of said sensor.

13. The apparatus of claim 9 wherein said sensor is adapted to detect a magnitude of said shockwave and an output of said sensor is related to said magnitude.

14. The apparatus of claim 13 wherein one of a time and a position for release of said second medium formed by said projectile is variable.

15. The apparatus of claim 14 wherein said one of the time and position for release of said second medium formed is selected in response to said magnitude of said shockwave-producing event.

16. The apparatus of claim 9 wherein said sensor is configured to detect an electromagnetic emission of said source.

17. The apparatus of claim 16 wherein said electromagnetic emission is selected from the group consisting of:

visible light, x-rays, gamma rays, infrared light, ultraviolet light, radio waves and microwaves.

18. The apparatus of claim 9 wherein said sensor is configured to detect neutrons.

19. A method for sensing and attenuating a shockwave produced by an event and propagated through a first medium comprising:

providing a sensor configured to detect a component of said event, a launcher, and a projectile for producing a second medium different from said first medium;

sensing by said sensor one or more electromagnetic indicia associated with said event and producing an output signal in response thereto;

transmitting said output signal to said launcher;

launching said projectile by said launcher in a direction to intercept said shockwave; and

detonating said projectile to create said second medium from said projectile,

wherein said shockwave is attenuated in intensity as it passes into, through, and out of said second medium.

20. The method of claim 19 wherein said shockwave continues to attenuate after passing out of said second medium at a rate greater than the attenuation rate before said shockwave entered said second medium.