Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.

Patents

  1. Advanced Patent Search
Publication numberUS2405694 A
Publication typeGrant
Publication dateAug 13, 1946
Filing dateAug 11, 1942
Priority dateAug 11, 1942
Publication numberUS 2405694 A, US 2405694A, US-A-2405694, US2405694 A, US2405694A
InventorsNicolas Herzmark
Original AssigneeNicolas Herzmark
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Defense system
US 2405694 A
Abstract  available in
Images(3)
Previous page
Next page
Claims  available in
Description  (OCR text may contain errors)

mg 3, N N.,HERZMARK DEFENSE SYSTEM 'Filed Aug. 11, 1942 5 sheets sneet 1 INVENTOR.

' NICOLAS A ERZMARK BY flTTOP/VEY Aug, 13, 1946. N. HE ZMARK 2,405,694

DEFENSE SYSTEM Filed Aug. 11, 1942 3 Sheets-Sheet 2 700 A INVENTOR.

# TTOP/VEV Patented Aug. 13, 1946 UNITED STATES PATENT OFFICET 2,405,694 DEFENSE SYSTEM Nicolas Herzmark, Indianapolis, Ind.

Application August 11, 1942, Serial No. 454,393

This invention relates to a defense system and means employed therein for destroying missiles directed against objects, at a safe distance from and before they may reach such objects.

One of the objects of the present invention is the provision of co-ordinated sound responsive means for the detection of a missile approaching from any direction, and means for orientating a defense instrumentality against such missile, and further means for causing such instrumentality to destroy the missile at a predetermined, safe distance from the defended object.

Another object of the present invention is the provision of a defense system against projectiles or the like, wherein is employed a combination of at least three operatively interconnected and cooperating units for detecting and locating such projectile while it approaches its object, and wherein one of the units controls a defense instrumentality, such as a mortar or gun, and. wherein the two other units control the firing mechanism of such defense instrumentality so that when the projectile nears a certain danger zone the charge of the defense instrumentality is loosed in front and against the projectile for destroying it before it reaches the danger zone.

A still further object of the present invention is to provide a defense system against projectiles, such as torpedoes, and in which system are employed electrically energized, sound-sensitive units cooperating with one another, and wherein one of the units controls the training against such projectile of a mortar or gun, adapted to shoot depth charges or the like, whereas at least two other units control the firing of the gun, and wherein the gun is so mounted that it will be constantly maintained at a certain elevation, and in which elevation such gun may be swung in a circular curve within an angle of at least 180, and wherein the gun is adapted to eject its charge for a certain distance from the gun, and wherein electrically controlled means are provided to discharge the gun against an approaching projectile when it reaches a point near the predetermined shooting distance within the aforesaid half circle.

A still further object of this invention is to provide in a defense system against sound emitting projectiles or the like, such as torpedoes, a plurality of sound responsive control units adapted to react to the emission of sound emanating from such torpedoes, and wherein one of the units controls the constant training of a mortar or gun against the approaching torpedo, while the other units control the firing mechanism of such mortar or gun, and wherein each of the units employ pressureand velocity actuated mi- '2' Claims. (Cl. 8941) crophones or hydrophones, motive means for operating the latter, means for co-ordinating the operation of the units, and wherein two units at both sides of the gun controlling unit are equipped with variable condensers, connected in parallel, and wherein these condensers are so designed that their total capacity, which latter is being constantly checked against a predetermined or standard capacity of the co-ordinating means, remains constant when the condensers are simultaneously operated in such a way that the vertical center plane passing through the velocity microphones intersect at any point of a half circle, the radius of which corresponds to a predetermined shooting distance of the gun, and that their total capacity becomes different from the aforesaid standard capacity when the vertical planes passing through the microphones intersect at a point beyond such half circle.

Still another object of the present invention is to provide with my microphone-operated units the aforesaid condensers of a special design to render them functioning in the manner indicated, and to provide a formula for the proper construction of the rotor plates of the condensers.

A still further object of this invention is to provide a formula for the calculation of angles of ever-changing triangles formed between a constant base and two intersecting vertical planes, and wherein the base conforms with a line connecting two outer units, and which line passes through a central unit, and wherein the intersecting vertical planes correspond to the central planes passing through the pressure and velocity microphones of the outer units.

The foregoing and still further objects and important advantages of the present invention will become more fully understood from the ensuing description, taken in connection with the accompanying drawings, which latter, while showing specific arrangements of the present invention, by no means are intended to limit the disclosure to the actual showing, and wherein Fig. 1 is a diagrammatical top view of a vessel equipped with my defense system;

Fig. 2 is an enlarged end elevation of a vessel showing the arrangement of few of the component parts of my system;

Fig. 3 is a diagrammatical illustration of a vessel equipped with my defense instrumentalities, with the condensers employed in the end units thereof being shown in greater detail, together with a formula pertaining to their construction, and another formula for the calculation of certain angles;

Fig. s is an illustration of a diagram showing :ontrol units forming part of my system; and

Figs. 5, 6, '7 and 8 represent detail diagrams of some of the control devices employed in Fig. 4.

Up to the present time numerous attempts have been made for defending moving or stationary objects, such as ships, lighthouses, gun emplacements, etc., against torpedo attacks bysubmarines, and it has been determined that the best way of defense against torpedos is the destruction of such torpedos at a safe distance from, and before they may do any damage to the objects against which they are directed. Similarly, in the defense against submarines or any other attacking ships, depth charges ejected from mortars, guns or other devices to destroy the offenders have been found very effective.

The present invention utilizes the heretofore gained knowledge in an improved and most positive manner, and employs an automatic defense system whereby a projectile, such as a torpedo, may be detected and followed until it reaches a convenient, but'a sufiiciently safe distance from the defender, at which it may be destroyed before becoming effective.

Referring now to Figs. 1 and 2, numeral Illi] denotes the body of a ship, equipped at both port and starboard with a combination of at least three electrically energized control units, indicated at A, Al, B, Bl, C and CI. Each of these units is composed of a shaft iiil, HM and Nil (see Fig. 4), extending vertically alongside the ship, a combination of a pressure hydrophone l and a velocity hydrophone 4, and a lei-directional motor i, all mounted upon the respective shafts. The two end or exterior units A and C are additionally equipped with variable condensers 8. In-

terior unit B has no condenser. All of the 'units are provided, in addition to the pressure and velocity hydrophones and the motor, with electrically energized controls, responsive to sound vibrations received by the two hydrophones, composed of individual sets of high-pass-filters 2' and amplifiers and rectifiers 3 for each of the two types of hydrophones. The amplifierand rectifier 3 of both hydrophones in each unit are connected'with a rectifier bridge and a polarized relay 8. These relays control the operation of bi-directional motors l, and the direction of rotation at which they are to operate.

Condensers 3 of units A and C are in parallel with one another, and their combined lead con- 4 the gun in its mounting at the desired angular elevation.

Fig. 5 diagrammatically illustrates the interior arrangement of the high-pass-filter 2 employed in each of the units with each of the hydrophones, and is designed to pass impulses of a cernects with a bridge circuit it, which is energized a certain setting, Bridge circuit ii] is connected to an input amplifier and rectifier I I, from which extends a lead to a relay l2. This relay is connected with another relay l3, and through this relay to a third relay M. Amplifier 3 of pressure hydrophone I in unit A is also connected with relay l3. Third relay M connects with amplifier and rectifier 3 of pressure hydrophone l inunit Cand with firingrelay I5, which controls the firing mechanism of mortar or gun l8.

Mortar or gun i3 is turned by bi-directional motor i, through hydrophone shaft 10! of unit B, within an arc of at least 180 degrees, whereby its aim towards an approaching torpedo is constantly maintained. The gun is preferably supported in a ball and socket mounting, and its sighting angle is kept constant, against the rolling of the vessel by a heavy plumb bob, holding tain frequency only. In Fig. 6 the arrangement of rectifier bridge 5 is shown, together with the polarized relay 6, which controls the operation of motors 7. Fig. 7 illustrates a detail arrangement of oscillator 9, variable condensers 8, bridge circuit Ill, with its constant capacity 88, amplifier I l and its output to relay i2, while Fig. 8 is a diagrammatical illustration of relays l2, l3 and 1 l4 and their connection with firing relay l5. In

that figure a pilot light i6 and a manually operable cut-out switch H are also indicated. While the instrumentalities illustrated in Figs. 5 to 8 are specifically constructed for their intended purposes, the diagram shown in Fig. 4 includes additional devices enumerated in the legend of that figure. These additional devices, such as pressure and velocity hydrophones, amplifiers, rectifiers, etc., are well known in the art and require no further explanation. However, their arrangement and cooperation with one another and with the instrumentalities shown in detail in Figs. 5 to 8, as defined in the diagram of Fig. 4, comprises a novel combination designed to provide the desired new results as will become hereinafter evident.

Referring to Fig. 3, ship I06 is provided with a combination of control units A, B and C, ex- .tending downwardly alongside the ship. End units A and C are equipped with variable condensers shown diagrammatically and enlarged at 8. In this figure there is illustrated a triangle, the base of which forms a line extending between units A and C, and is indicated at Y. This line passes through unit 13. The two sides of the triangles AT and CT intersect at a point of circle D, indicating the danger zone. The radius of circle D corresponds to a line connecting apex T of the triangle with the center of base Y, at the unit B.

Fig. 3' contains two formulas, one for computing angles X and X of the variable triangle A, T and C, which angles correspond to those between the straight edges of the movable and stationary blades of the respective condensers of units A and C, and the other formula is intended'to facilitate the computation of the ef fective capacity areas a of each of the condensers. The derivation of the formula for angles at on a" is as follows:

In this formula angle Z (Fig. 3) is also called 0.

Assume that a perpendicular h. is drawn in Fig. 3 from point T against a left-hand extension of base y of triangle ATC.

The distance between point B and the point of intersection of h with the extension of y is b.

b-y/2=base of triangle having as one of its sides the normal h, the other side being line TA.

b+y/2=base of triangle having as one of its sides the normal h, the other side being line TC.

Tan :r=-tan (m) (Formula 1) (Formula 2) .R sin 0 From Formula 2 (Formula 4) R cos +y/2 The derivation of the formula for computing the effective condenser area a is as follows: 7

Let A equal the total efiective capacity area, that is when the variable plates fully coincide with or are completely opposite the fixed plates.

Let a be the effective capacity area, that is when the variable plates are not in completely opposite position to the fixed plates.

r+r'=diameter of variable plates Effective area a.-= included angle of sector,

in this case 180-x.

r (180x) l The effective area a of the variable plates:

1r a 1 r i 2 180-$ (1i') 180:c Z 2 2) X 180 T 2 360 The movable blades of variable condensers 8, 8 are intended to be operated simultaneously, and their total efiective capacity must remain constant and must match the fixed capacity of balancing condenser 88 in capacity bridge circuit l0 before gun 18 may be fired.

Such condition is efiected whenever the vertical center planes passing through the velocity hydrophones of the respective condensers meet at any point of danger circle D, such as at point T of triangle ATC. These vertical center planes are represented by the sides AT and CT of that triangle, and it is assumed that the straight edges of the movable blades of the respective condensers coincide with these planes.

When these planes meet at a point outside of circle D, the total effective capacity of the two condensers becomes different from the fixed capacity of balancing condenser 88, and gun I8 can not be fired.

The arrangement of the support for gun or mortar I8, controlled by unit B, is such that it permits not only the ready movement of the gun -within at least a half circle, but the mounting of the gun is so arranged that the gun will be constantly maintained at a uniform elevation in respect to the horizontal plane, so that when the gun is discharged it will place its missile at a distance approximating, but preferably somewhat short of the radius of danger circle D.

The mortar or gun is equipped with a firing device controlled by the combined arrangement shown in the lower portion of Fig. 4, and which comprises oscillator 9, capacity bridge circuit l0, amplifier and rectifier II, the three relays I2, [3 and I4 and the firing relay l5. Relay [2 is being energized by the output from amplifier and rectifier II, and makes contact when it is deenergized. Relay I3 is controlled by amplifierrectifier 3 for hydrophone l of unit A, and relay l4 by amplifier-rectifier 3 for hydrophone l of unit C. These relays make contact when their respective pressure-actuated hydrophones receive sound impulses of a sufficient intensity. When all three relays l2, l3 and 14 make contact at the same time, firing relay [5 becomes energized and operates the firing mechanism of gun l8.

Operation It has been determined that sound vibrations emitted from a passing ship, or from the moving vessel itself equipped with my system, are below a certain sound frequency, for instance below 5000 vibrations per second. It has been also established that projectiles, such as torpedoes, emit sound frequencies above the usual sound of ships, say above 5000 vibrations per second, due to the fact that their propellers are small and therefore are operating at a very high speed.

The pressure hydrophones employed in my system, as well as the velocity hydrophones, are designed to pick up sounds of any vibration, but to induce impulses in the electrical part of my system only when these vibrations exceed the range of normal, low vibration frequencies of ships, and approximate the high vibration frequencies of an approaching torpedo. Thus when pressure hydrophones I pick up a sound corresponding to that emitted by a torpedo, the

vibration impulses will be translated to the electric portion of my system and will cause the units to operate, that is shafts It, I 0| and I0! will be turned by motors 1 until the velocity hydrophones will be in line with the sound, at which moment the turning motion of the units stops.

To understand this operation in detail the following explanation is in place. Assume that an approaching torpedo emits a sound which is picked up by the pressure hydrophones of al1 three units. The sound is electrically transmitted to high-pass-filters 2 of the pressure hydrophones, passes to amplifiers and rectifiers 3 thereof, and from there to rectifier bridges 5 and polarized relays 6. These relays becoming energized will cause the operations of motors I, which will turn shafts l0], HM, and HM. Both pressure and velocity hydrophones turn with these shafts. The moment the velocity hydrophones are in a position to directly pick up the sound, which position may be called the zero reception, the impulses received by the velocity hydrophones are propagated through their highpass-filters 2, their amplifiers and rectifiers 3, to rectifier bridges 5, and to the polarized relays 6. At that moment both contacts in the relay break, see Fig. 6, in consequence thereof motors 1 stop the rotation of the shafts and of the hydrophones.

As the torpedo approaches nearer and the velocity hydrophones fail to receive the sound impulses, while the pressure hydrophones still are receiving such impulses, one of the contact points in the polarized relay 6 will close and cause the operation of motors I. Thus the entire hydrophone assembly'is turned in the direction towards the sound, until the velocity hydrophone again reaches zero reception position, at which moment the operation of the motors will stop. Bridges 5 and polarized relays 6 operate so that a direct current output is produced, the polarity of which depends upon the presence or absence of a phase inversion between the two signals received by the two hydrophones of each unit.

the switch in relay t will'open, and the operation of motors i will stop; Referring to Fig. 6, two inputs are indicated, one from pressure hydrophone 'l, the other from velocity hydrophone Both impulses are of alternating currents, which are converted by rectifier bridge 5 to produce direct current output to polarized relay 6. Depending upon whether or not the two alternating input voltages introduced into bridge 5 are in phase or out of phasdthe upper or lower switch contacts of relay 8 will close, while both contacts wil1 remain open if there is no current in either one or both inputs, or if the two currents differ in frequency. In consequence of the aforesaid phase inversion, each unit individually controlled by its polarized relay fiis caused to respond in its operation to the sound impulses received by each individual unit.

The variable condensers of units A and C and their relation to each other has been already explained, yet their operation must be repeated in order to present a clear picture of the function of the device. Their total} capacity remains constant when they are simultaneously so turned that the vertical planes passing through their respective velocity hydrophones meet at a constant predetermined distance from unit B. When, however, these two planes meet at a point outside of danger circle D, the total effective capacity of the condensers will differ. condensers are connected in parallel, and their total capacity is being continuously matched against the capacity of the capacity bridge circuit it], which is energized, by oscillator 9. While the condensers are at a position at which their total effective capacity does not match the capacity of fixed condenser 88 of the bridge circuit 50, the latter will not be balanced, and current will be delivered to the input amplifier and rectifier II. The amplified voltage being rectified, will keep relay [2 open.

When the condensers are in a position at which their total capacity equals the predetermined capacity value of bridge circuit ill, the latter becomes balanced and no voltage is passed to amplifier and rectifier l l'. At that moment relay i2 becomes de-energized and closes the firing circuit across the relay. At that position of relay l2, firing relay l5 may become energized and could actuate the firing mechanism of gun iii, which latter is constantly trained in the direction towards the target and is maintained at an elevation to place its charge, when fired, preferably in front of the approaching torpedo.

It is readily conceivable that the firing mechanism may be actuated when units A and C accidentally assume their correct position, at which the total capacity of their condensers equal the pre-determined or standard capacity 88 of bridge circuit I0. In order to avoid the firing of the gun, due to such accidental setting. of condensers relays l3 and Marc interposed. They are energized only when signals arereceived by the pressure hydrophonesof both units' A and C.

If relays l3 and [4 become energized while relay The 12! is de-energized and makescontaciy the ;cir-

cuit between relays l2, l3 and I4 isclosed, and firing relay l5 may then operate.

This arrangement may be readily understood by consulting Fig. 8 showing relays l2, l3 and I4, and their respective" arrangements. The operation of firing relay l5: may be prevented by opening manually operable switch II. A pilot light I6 is provided for indicating the closed or open position of the relay circuit.

It is to be borne inmind that sound emitted from sources other than those of projectiles or torpedoes must not'energize any one of the units. For this reason it was determined to employ a high-pass-filter 2, such as shown in detail in Fig. 5, which suppresses all signals below a certain minimum frequency. It has been found I that sound vibrations emitted from torpedoes exceed 5000 vibrations per second. Filter 2' is designed to block sound vibrations of less than 5000, thus preventing ship noises and other noises below this frequency from interfering with the operation of the mechanism.

The operation of the sound controlled units in respect to approaching torpedoes from different directions is clearly illustrated in Fig. 1. It will be seen that my system may detect, follow and effectively deal with torpedoes approaching at even acute angles, such as in the case of torpedo M, M at the left of the figure.

Similarly torpedoes N, N, O, O, and P, approaching from other directions, become vulnerable. At the moment any of these torpedoes approach a point near or at danger circle D,

. mortar or gun I8'fires a depth charge in front of the missile. Obviously, more than one group of units A, B and C would be required for effectively combatting a simultaneous attack by two or more torpedoes.

In the foregoing description specific arrangements of my system have been described. 'Similarly the drawings illustrate only one form .of a control mechanism, chiefly electrical in nature. In Figure 1 of the drawings is indicated but one set of units for each side of vessel I00. It is to be understood, of course, that more than two sets ofunits may be employed along'o'ne side of a vessel, and that the placement of such sets of units in relation to the body of the vessel may be chosen-for complete protection of its hull, so that no part thereof may remain vulnerable.

Inasmuch as ,all the aforesaid modifications are quite obvious and depend upon the basic three unit arrangement of my system, specific illustrations of such modified forms are not shown, nor are they specifically described. In any event, however, all possible modifications of my system will require the employment of a combination of cooperative means which will produce the desired results. These combinations will include the employment of at least one pressure hydrophone and a velocity hydrophone, or their equivalents, as well as motive means for turning the combined hydrophones, and means whereby these motive means may be operated in one or the other direction: in response to vibratory impulses received by the combination of the two hydrophones.

"In the specification particular emphasis is placed onthe defense of ships against approaching torpedos. The same or similar arrangements ma be readily employed for coastal defense or for the defense of stationary objects, and against missiles ,or projectiles which are not torpedos, but emit sounds which may be detectedby the instrumentalities employed, and which missiles may be destroyed before they reach the defender objects.

Having thus defined the high points of my invention, it will be quite readily understood that neither the specific description nor the specific illustrations are intended to limit my invention to the instant presentation, and that I shall have the right to make changes, improvements and rearrangements of the difierent instrumentalities employed, without departing from the broad scope of my invention, as set forth in the annexed claims.

I claim:

1. In a defense system against projectiles or the like, the combination of at least three spaced, electrically interconnected'sound detector units in cooperation with one another, and comprising two outer and one inner unit, a gun or the like, a mounting for the gun for constantly maintaining it at a certain angle of elevation and for facilitating its swing within an angle of at least 180, whereby the gun is adapted to shoot a charge for a predetermined distance, said inner unit being designed to train the gun towards an approaching projectile, said outer units being adapted to locate such projectile and to actuate the firing mechanism of the gun when the projectile reaches a point near the predetermined shooting distance of the gun, all of said units comprising pressure-and velocity-microphones mounted on a shaft and a reversible motor for actuating the shaft, said outer units also having variable condensers operative with their respective shafts, a high-pass filter and an.

amplifier and rectifier connected with each microphone of each unit, a rectifier bridge and a polarized relay forming parts of each unit, said polarized relays controlling the operation and the direction of operation of the respective motors of each unit; means for controlling the firing mechanism of the gun, said means comprising an oscillator, a bridge circuit energized by said oscillator and being controlled by said variable condensers of the outer units, an amplifier and rectifier, a relay controlled by the latter, another relay controlled by the amplifier and rectifier of the pressure microphone in one of the outer units, a third relay controlled by the amplifier and rectifier of the pressure microphone in the other outer unit, and a firing relay controlled by the three last-mentioned relays.

2. In a defense system against projectiles or the like, the combination of at least three spaced, electrically interconnected sound detector units in cooperation with one another, and comprising two outer and one inner unit, a gun or the like, a mounting for the gun for constantly maintaining it at a. certain angle of elevation and for facilitating its swing within an angle of at least whereby the gun is adapted to shoot a charge for a predetermined distance, said inner unit being designed to train the gun towards an approaching projectile, said outer units being adapted to locate such projectile and to actuate the firing mechanism of the gun when the projectile reaches a point near the predetermined shooting distance of the gun, all of said units comprising pressureand velocity-microphones mounted on a shaft and a reversible motor for actuating the shaft, said outer units also having variable condensers operative with their respective shafts, a high-pass filter and an amplifier and rectifier connected with each microphone of each unit, a rectifier bridge and a polarized relay forming parts of each unit, said polarized relays controlling the operation and the direction of operation of the respective motors of each unit; means for controlling the firing mechanism of the gun, said means comprising an oscillator, a bridge circuit energized by said oscillator and being controlled by said variable condensers of the outer units, an amplifier and rectifier, a relay controlled by the latter, another relay controlled by the amplifier and rectifier of the pressure microphone in one of the outer units, a third relay controlled by the amplifier and rectifier of the pressure microphone in the other outer unit, and a firing relay controlled by the three last-mentioned relays, said condensers being connected in parallel and being so designed that their total capacity, checked against a predetermined or standard capacity of said bridge circuit, remains constant when they are simultaneously operated in such a Way that the vertical central planes passing through the velocity microphones intersect at any point of a half-circle, the radius of which corresponds to the predetermined shooting distance of the gun, and that their total capacity becomes difierent from such standard capacity when the aforesaid microphone planes intersect at points beyond that half-circle.

NICOLAS HERZMARK.

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2504118 *Aug 2, 1945Apr 18, 1950George C EvansUnderwater sonic apparatus
US2535147 *May 29, 1948Dec 26, 1950Honeywell Regulator CoElectronic control circuits
US3050707 *Dec 8, 1960Aug 21, 1962Judd O BakerMethod and apparatus for torpedo direction locating
US3943870 *Oct 24, 1950Mar 16, 1976The United States Of America As Represented By The Secretary Of The NavyPinging controlled anti-torpedo device
US4313181 *Aug 29, 1962Jan 26, 1982The United States Of America As Represented By The Secretary Of The NavyTorpedo countermeasure
US5001984 *Jul 14, 1966Mar 26, 1991The United States Of America As Represented By The Secretary Of The NavyProximity fuze system
US5012742 *Jan 25, 1966May 7, 1991The United States Of America, As Represented By The Secretary Of The NavyProximity fuze
US8677881Apr 10, 2012Mar 25, 2014The Boeing CompanyMethod and system for attenuating shock waves via an inflatable enclosure
US8740071 *Apr 17, 2012Jun 3, 2014The Boeing CompanyMethod and apparatus for shockwave attenuation via cavitation
US8806945Nov 22, 2011Aug 19, 2014The Boeing CompanyMethod and apparatus for shockwave attenuation
Classifications
U.S. Classification89/41.8, 89/36.17, 367/1, 318/460, 102/416, 318/560, 102/428, 181/125
International ClassificationB63G9/00
Cooperative ClassificationB63G9/00
European ClassificationB63G9/00