Target apparatus

• US 4,349,728 A
• Filed: 12/07/1979
• Issued: 09/14/1982
• Est. Priority Date: 12/07/1978
• Status: Expired due to Term

• Current Assignee: ATA Training AIDS AUST Pty Limited
• Original Assignee: Australasian Training AIDS Pty Limited
• Inventors: Bowyer, William H., Phillips, Robert B., Moxley, Bruce
• Primary Examiner(s): Gruber, Felix D.
• Application Number:
  US06/101,191
• Time in Patent Office: 1,012 Days
• Field of Search: 235/400, 367/127, 367/906, 273/371, 273/372, 273/373, 364/423, 434/1, 434/19
• US Class Current: 235/400
• CPC Class Codes: B06B 1/0681 and a damping structure
• CPC Class Codes: F41J 5/06 Acoustic hit-indicating systems, i.e. detecting of shock waves F41J5/056 takes precedence
• CPC Class Codes: G01S 5/22 Position of source determined by co-ordinating a plurality of position lines defined by path-difference measurements G01S5/28 takes precedence
• CPC Class Codes: Y10S 367/906 Airborne shock-wave detection

Abstract

A target apparatus, having a framework covered by sheets of material to form a chamber the sheets of material being penetrable by a projectile, such as a bullet, fired at the target. A plurality of transducers are positioned at respective spaced-apart locations within the chamber and lying on an arc of a circle, for detecting shock or pressure waves in the chamber caused upon penetration of the sheets of material by the projectile. Time differences between instants of detection of a shock or pressure wave by the transducers are measured, the location at which the projectile penetrated the sheet of material being determined from the time differences. Preferably, a bull'"'"'s-eye or aiming mark is provided on the target, the center of which is aligned with the center of the circle on which the transducers lie. Apparatus is also disclosed for determining the speed of sound in air within the chamber, enabling the projectile penetration point to be determined with particular accuracy.

Claims

1. Target apparatus, comprising:

a framework;

at least one sheet of material, capable of being penetrated by a projectile, covering said framework to form a chamber;

a plurality of transducers for detecting shock or pressure waves in said chamber caused upon penetration of said at least one sheet of material by said projectile, said transducers being positioned at respective spaced-apart locations within said chamber and lying on only a portion of an arc of a circle lying in a region where said transducers are protected from being hit by said projectile;

means responsive to said transducers for measuring time differences between instants of detection of a shock or pressure wave by said transducers; and

means responsive to said time difference measuring means for determining and indicating a location at which said projectile penetrated said at least one sheet of material.

2. Target apparatus according to claim 1, wherein three said transducers are provided.

3. Target apparatus according to claim 1, further comprising a bull'"'"'s-eye or aiming mark located relative to said sheet of material, wherein said bull'"'"'s-eye or aiming mark is aligned with a center point of said circle.

4. Target apparatus according to claim 1, wherein said location determining means further comprise means for measuring the propagation velocity of sound in air within said chamber.

5. Target apparatus according to claim 4, wherein said propagation velocity measuring means comprises:

means for transmitting a sound pulse;

means spaced from said transmitting means for detecting said sound pulse; and

means responsive to said sound pulse detecting means for measuring a time taken for said sound pulse to travel a known distance and for determining therefrom the propagation velocity of sound in air within said chamber.

6. Target apparatus according to claim 5, wherein said detecting means comprises a pair of transducers spaced at said known distance from one another.

7. Target apparatus according to claim 5, wherein said detecting means comprises a transducer spaced at said known distance from said sound pulse transmitting means.

8. The target apparatus of claim 5, wherein said means for transmitting a sound pulse consists of a spark gap discharge means for generating a fast rise time airborne pressure wave.

9. The target apparatus of claim 8, wherein said means for transmitting a sound pulse further comprises a high voltage pulse generator connected to said spark gap discharge means, said high voltage pulse generator consisting of:

an optical coupler;

an electric current control means connected to receive input signals from said optical coupler;

a high voltage impulse transformer for connecting said electric current control means to said spark gap discharge means.

10. The target apparatus of claim 5, wherein said means for detecting said sound pulse consists of:

an outer housing;

a coaxial connecting cable extending into an opening in said housing;

a piezoelectric disk positioned in a recess formed in said housing;

a finge gauge conductive wire connecting said piezoelectric disk to said coaxial connecting cable.

11. The target apparatus of claim 5, wherein each of said plurality of transducers has an associated low-noise, wide-band amplifier positioned proximate to its associated transducer.

12. The target apparatus of claim 5, wherein said means for transmitting a sound pulse and said means spaced from said transmitting means are positioned in a sensor support beam, said sensor support beam extending along a lower portion of said target chamber.

13. The target apparatus of claim 5, wherein said means responsive to said sound pulse detecting means includes means for amplifying, filtering and detecting signals from said sound pulse detecting means.

14. Target apparatus according to claim 4, wherein said propagation velocity measuring means comprises:

means for measuring the temperature and relative humidity or air within said chamber, and

means responsive to said means for measuring the temperature and relative humidity or air within said chamber, for calculating a value representing the propagation velocity of sound in air within said chamber.

15. Target apparatus according to one of claims 1 or 4, wherein said transducer locations vary with temperature, and said location determining and indicating means further compensates for variation of said transducer locations with temperature.

16. Target apparatus according to claim 4, wherein said propagation velocity measuring means comprises:

means for measuring the temperature of air within said chamber; and

means, responsive to said means for measuring the temperature of air within said chamber, for calculating a value representing the propagation velocity of sound in air within said chamber.

17. Target apparatus according to claim 1, wherein said chamber is substantially anechoic.

18. Target apparatus according to claim 1, further comprising an aiming mark located relative to said sheet of material and relative to a center point of said circle.

19. The target apparatus of claim 18, wherein the means for determining and indicating a location includes a programmed general-purpose computer.

20. The target apparatus of claim 1, wherein said plurality of transducers are mounted on a sensor support beam, said sensor support beam extending along a lower portion of said target chamber.

21. The target apparatus of claim 20, wherein at least some of said plurality of transducers are mounted on said sensor support beam by support brackets which space said transducer from said beam.

22. The target apparatus of claim 20, wherein said support beam is mounted to said frame by means of anti-vibration mountings.

23. The target apparatus of claim 1, wherein said means responsive to said transducers includes means for amplifying, filtering and detecting signals from said transducers.

24. The target apparatus of claim 1, wherein the arc of a circle on which said transducers are positioned has its center aligned with an aiming mark on said target.