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Publication numberUS3445808 A
Publication typeGrant
Publication dateMay 20, 1969
Filing dateApr 5, 1968
Priority dateApr 5, 1968
Publication numberUS 3445808 A, US 3445808A, US-A-3445808, US3445808 A, US3445808A
InventorsFred P Johnson
Original AssigneeUs Army
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Small arms locator
US 3445808 A
Abstract  available in
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Claims  available in
Description  (OCR text may contain errors)

F. P. JOHNSON 3,445,808

SMALL ARMS LOCATOR May 20, 1969 Filed April 5, 1968 zi .1 I fe, @gw Y ATTORNEYJ.

United States Patent O 3,445,808 SMALL ARMS LOCATOR Fred P. Johnson, Pittsfield, Mass., assignor, by mesne assignments, to the United States of America as represented by the Secretary of the Army Filed Apr. 5, 1968, Ser. No. 719,137 Int. Cl. G01s 3/ 80 U.S. Cl. 340-16 5 Claims ABSTRACT F THE DISCLOSURE The direction of a bullet is ascertained by comparing the points at which it passed through two planes. Each point is pinpointed instantly by comparing the time element required for a sound, generated as the bullet passes through the plane, to reach various microphones at preselected points in each plane.

BRIEF SUMMARY Direction finders, comprising audio sensors, microphones or other energy sensors, have been used in various groupings to indicate the direction of a source of sound or energy generator. However, such direction finders have enjoyed only limited utility. In a given setting, such as in a battle, many sounds may be generated simultaneously, such as guns tiring, projectiles exploding, etc., thereby making it impossible or diicult to isolate a particular sound-source. Perhaps only one gun has found its target (your helicopter) and that gun should be pinpointed instantly for counterfire purposes or evasive action.

This invention helps pinpoint the direction from which came an object that has found its mark and scored a hit.

IN THE DRAWING FIGURE 1 is a diagrammatic illustration of the time differential principles involved;

FIGURE 2 is a diagrammatic illustration of the path a bullet passing through two planar sound-producing objects;

FIGURE 3 is a block-diagram of the computer system of the invention.

DETAILED DESCRIPTION Sensors 1, 2, 3 and 4 are placed at predetermined locations relative to a substantially planar object or sheet 5. As exemplary, four sensors, more or less, may be audio sensors or microphones and the sheet may be rectangular, four by eight feet.

An object, such as a bullet, strikes sheet 5 at point P and generates concentric sound waves progressing toward the sensors. The sound reaches the sensors at the same instant only if the bullet struck the center of the sheet. Otherwise, the time of arrival of the sound at the various sensors is different. A difference in the time of sound arrival at sensors 1 and 2 can be expressed as This time difference, A114, will not, by itself, locate the point of peneration P. It will describe a locus of points, hyperbola H1 2, that will contain the point P. The time difference between sensors 2 and 3 will describe a second locus of points, hyperbola H2 3, that will intersect H1 2 3,445,808 Patented May 20, 1969 ICC at P. Time data from sensor combination 3-4 and 4-1 can be used to correlate this location.

In FIGURE 2 two spaced apart sheets 5 and 5"-are illustrated. Sheet 5 has sensors 1 to 4 at its corners corresponding with `sensors 1 to 4 at the corners of sheet 5. These sheets should preferably be parallel to simplify computations. The bullet 6 penetrates these sheets at points P and P. A straight line interconnecting these points, when traced back to the ground or jungle below, indicates approximately where the bullet came from.

FIGURE 3 indicates the well-known pieces of electronic equipment used to bring out the desired data from the equipment described above. The sounds from the bullet are detected by the sensors 1-4 and 1'4'. The output of the senors is fed into computer means including the output of clock 7, threshold gate 8, counter 9 and computer 10. Computer 10 also may receive data as to vehicle (helicopter) speed, heading, altitude and vertical reference. The computer may correlate the data fed thereinto and computes the gun location data so that the pilot or gunner can pinpoint the gun position instantly for evasive or counterfire action. Theoretically it should be possible to feed the gun location data directly into gun control equipment on the vehicle which would automatically train the vehicle gun on the gun position from which the bullet came and quickly initiate counterfire. However, such system goes beyond the scope of the present system.

Sheets 5 and 5' are shown for purposes of illustration of the principles involved. These sheets may be separate elements carried by a vehicle. Of course they may be used in the area of a stationary gun emplacement on the ground. In such installation the sheets could be placed in vertical planes so that a projectile coming in on a nearhorizontal path would penetrate the sheets successively and the invention would pinpoint sniper or enemy gunlire ahead as it comes dangerously close.

In some installations there need be no separate sheets as such. For example, in a plane or helicopter, the skin of the craft, when pierced by `a bullet, will generate the sounds as it passes through the belly and the top of the craft. Microphones, properly positioned relative to these parts of the skin of the craft, will detect the sounds as previously described.

I claim:

1. The method of determining the direction of a passing object comprising placing a first plurality of energy sensors at preselected points substantially in a rst plane, placing a first substantially planar object substantially in said first plane, placing a second plurality of energy sensors substantially in a second plane, placing a second substantially planar object substantially in said second plane, using said first sensor to determine the location at which said passing object passed through said iirst plane, using said first sensors to determine the location at which said passing object passed through said second plane, and comparing the locations in the planes to determine the direction ofthe passing object.

2. Apparatus for determining the direction of a passing object comprising a first plurality of energy sensors placed at preselected points substantially in a first plane, a first substantially planar object substantially in said first plane, a second plurality of energy sensors substantially in a second plane, a second substantially planar object substantially in said second plane, computer means con- 3 t nected to said first sensors and said second sensors to indicate the location of said passing object as it passes through said rst and second planes and to compare the locations to thereby determine the direction of the passing object.

3. Apparatus as in claim 2 wherein said energy sensors comprise microphones, sensitive to energy waves generated as said passing object passes through said planar objects.

4. Apparatus as in claim 3 wherein said energy sensors comprise four microphones, substantially in each plane, substantially at the corners of a pair of rectangles.

l4 5. Apparatus as in claim 2 wherein said first and second planes are substantially parallel.

References Cited UNITED STATES PATENTS RICHARD A. FARLEY, Primary Examiner.

U.S. C1. X.R. ISI-.5; 340-6 22253310 UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,445,808 Dated 2O May 1969 Inventor(s) FRED P. JOHNSON It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:

Column 2, line 53, "sensor" should be sensors Column 2, line 55, "first" should be second SIGNED AND SEALED SEP 2 1959 (SEAL) Attest:

ard Edw M Flecher Ir WILLIAM E SCIHUYLER, JR- Attestmg Offlcer commissioner of Patents

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2925582 *Feb 18, 1957Feb 16, 1960Oflice Nat D Etudes Et De RechAcoustical firing indicator
US2958866 *Mar 4, 1953Nov 1, 1960Aerojet General CoElectronic signaling systems
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3585497 *Apr 7, 1969Jun 15, 1971Dalzell Eugene W JrBullet hole locator-open circuit type
US3656056 *Apr 7, 1969Apr 11, 1972Us ArmyBullet hole locator-resistance type
US3707699 *Aug 7, 1970Dec 26, 1972Del Mar Eng LabRemote scoring system for bombing or rocket range
US4261579 *May 30, 1979Apr 14, 1981Australasian Training Aids (Pty.), Ltd.Shock wave triggered target indicating system
US4308602 *Jan 4, 1979Dec 29, 1981Australasian Training Aids Pty., Ltd.Target equipment
US4313182 *Jul 16, 1980Jan 26, 1982Australasian Training Aids (Pty.) Ltd.Target equipment
US4686639 *Feb 7, 1985Aug 11, 1987Rockwell International CorporationMethod for inspecting an item
US4813877 *Jul 24, 1987Mar 21, 1989Del Mar AvionicsRemote strafe scoring system
US5241518 *Feb 18, 1992Aug 31, 1993Aai CorporationMethods and apparatus for determining the trajectory of a supersonic projectile
US5917775 *Feb 7, 1996Jun 29, 1999808 IncorporatedApparatus for detecting the discharge of a firearm and transmitting an alerting signal to a predetermined location
US5920522 *Jul 7, 1997Jul 6, 1999Levanon; NadavFor indicating information related to the trajectory of a projectile
US6109614 *Jul 17, 1997Aug 29, 2000Tardis Systems, Inc.Remote sensing apparatus of supersonic projectile
US6198694Mar 27, 1997Mar 6, 2001Håkan AppelgrenMethod and device for projectile measurements
EP0157397A2 *Mar 31, 1985Oct 9, 1985DRELLO, Ing. Paul Drewell GmbH & Co. KGArrangement to determine the impact point, the velocity and the angle of incidence of a projectile hitting a target at supersonic velocity
WO1993016395A1 *Feb 17, 1993Aug 19, 1993Aai CorpMethods and apparatus for determining the trajectory of a supersonic projectile
WO1997037194A1 *Mar 27, 1997Oct 9, 1997Haakan AppelgrenMethod and device for projectile measurements
U.S. Classification367/127, 367/129, 367/906
International ClassificationF41J5/06, G01S5/22
Cooperative ClassificationG01S5/22, F41J5/06, Y10S367/906
European ClassificationG01S5/22, F41J5/06