Shock wave triggered target indicating system

• US 4,261,579 A
• Filed: 05/30/1979
• Issued: 04/14/1981
• Est. Priority Date: 05/30/1978
• Status: Expired due to Term

• Current Assignee: ATA Training AIDS AUST Pty Limited
• Original Assignee: Australasian Training AIDS Pty Limited
• Inventors: Bowyer, William H., Newnham, Robert
• Primary Examiner(s): Oechsle, Anton O.
• Application Number:
  US06/043,807
• Time in Patent Office: 685 Days
• Field of Search: 273/372, 35/25, 310/322, 310/334, 310/335, 310/340, 310/341, 310/344, 310/345, 310/346, 367/902, 367/906
• US Class Current: 273/372
• CPC Class Codes: B29C 70/70 Completely encapsulating inserts B29C70/86 takes precedence
• CPC Class Codes: F41J 5/06 Acoustic hit-indicating systems, i.e. detecting of shock waves F41J5/056 takes precedence
• CPC Class Codes: Y10S 367/902 Speed of sound compensation
• CPC Class Codes: Y10S 367/906 Airborne shock-wave detection

Abstract

To determine the position of a bullet relative to a target an array of at least six transducers is provided, the transducers being in two parallel rows of three in a common plane. The instants of detection of the shock wave generated by the bullet are measured and the position of the bullet is calculated from the measured values.

Claims

1. Apparatus for determining the location at which the trajectory of a supersonic projectile passes through a predetermined target area situated relative to a predetermined target, comprising:

a plurality of transducers located at respective spaced positions in two substantially linear rows, said rows being generally coparallel and spaced apart in a common plane which is generally perpendicular to and located adjacent a single edge of the target area, each said row comprising at least three said transducers, and each said transducer being operative to produce an output signal in response to detection of an airborne shock or pressure wave generated by the supersonic projectile;

individual threshold circuit means coupled to each transducer and responsive to said output signal for providing a digital signal when said output signal exceeds a predetermined threshold, the digital signal having a leading edge representing a time of detection of the shock or pressure wave by the associated transducer; and

digital processing means, provided with data representing the respective positions of the transducers and data relating to the speed of sound in air, and operative for

(1) measuring time differences between the leading edge of the digital signal associated with one of the transducers and the respective leading edges of the digital signals associated with each of the remainder of the transducers,

(2) calculating, from said measured time differences and from the data representing the transducer positions and the data relating to the speed of sound in air, the location at which the projectile trajectory passes through the target area and the velocity vector of the projectile at said location, and

(3) providing an indication of said calculated location,

whereby said location at which the projectile trajectory passes through the predetermined target area is determined by solving for such unknowns as the supersonic velocity of the projectile and the velocity vector thereof.

2. The apparatus of claim 1, wherein the transducers are evenly spaced along said substantially linear rows.

3. The apparatus of claim 2, wherein each transducer of one said row is aligned in said common plane in a direction generally perpendicular to said rows with a respective transducer of the other of said rows.

4. The apparatus of claim 1, wherein said common plane is horizontal.

5. The apparatus of claim 1, wherein said common plane is inclined.

6. The apparatus of claim 4 or claim 5, wherein said common plane is located adjacent a lower side edge of the predetermined target area, further comprising means for shielding said transducers from impact thereon by said projectile.

7. The apparatus of claim 1, wherein said common plane is vertical.

8. The apparatus of claim 1, further comprising means for determining and providing to said digital processing means data representing the speed of sound in ambient air in the region of the target area.

9. The apparatus of claim 8, wherein said speed of sound determining means comprises means for generating a pulse of sound and means for measuring the time taken for the pulse of sound to traverse a known distance.

10. The apparatus of claim 8, wherein said speed of sound determining means comprises means for measuring the temperature and relative humidity of the air in the region of the target area.

11. The apparatus of claim 1, further comprising means for measuring and providing to said digital processing means data relating to wind velocity and direction in the region of the target area, said digital processing means being further operative to employ said data relating to wind velocity and direction in calculating said location and said projectile velocity vector.

12. The apparatus of claim 11, wherein said wind velocity and direction measuring means comprises a source of sound, and one or more transducers for detecting sound from said source and coupled to provide to said digital processing means said data relating to wind velocity and direction.

13. The apparatus of claim 1, wherein each transducer comprises a piezo-electric member, and a solid member of rigid material having a base portion in firm contact with the piezo-electric member and a convex surface exposed to the airborne shock or pressure wave, said member of rigid material transmitting the shock or pressure wave to said piezo-electric member.

14. The apparatus of claim 13, wherein said convex surface is hemispherical.

15. The apparatus of claim 13, wherein said piezo-electric member is disc-shaped and is provided with conductive coatings on two opposing faces thereof, each said transducer further including respective conducting wires connected to said coatings and a member of insulating material having a recess to accommodate said disc and channels accommodating said conductive wires.