US3653324A - Electronic device applicable to ordnance safety and arming systems - Google Patents

Electronic device applicable to ordnance safety and arming systems Download PDF

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US3653324A
US3653324A US10173A US3653324DA US3653324A US 3653324 A US3653324 A US 3653324A US 10173 A US10173 A US 10173A US 3653324D A US3653324D A US 3653324DA US 3653324 A US3653324 A US 3653324A
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signals
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electronic
arming
round
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John J Furlani
Harry J Davis
Philip Ingersoll
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US Department of Army
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00Electric fuzes
    • F42C11/06Electric fuzes with time delay by electric circuitry

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  • ABSTRACT An all-electronic device for the detection and processing of those environmental signatures associated with the launching of a munitions round.
  • the non-mechanical device imposes stringent requirements that the environmental signatures must meet before the device will issue a command signal to arm the round.
  • Two transducers are utilized to sense two distinct conditions that are peculiar to the rounds launching. in a particular embodiment, the two transducers used are a piezoelectric crystal that senses acceleration setback and a magnet and coil arrangement that is triggered when the round leaves the gun barrel.
  • the environmental signatures that are sensed must fall within certain voltage ranges and time intervals that have been preselected according to the particular weapon and round combination under consideration
  • the device will provide a useable signal for any subsequent delay and arming function of the round 7 Claims, 3 Drawing Figures SlGNAL N conomonme SDUCEQ DELAY AND MIMI NG ./-'ZO DEVlCE
  • the invention described herein may be manufactured, used, and licensed by or for the United States Government for governmental purposes without the payment to us of any royalty thereon.
  • This invention relates generally to safety and arming devices for use in ordnance fuzing and, more particularly, to an allelectronic device that senses signatures peculiar to a projectiles launching which can be used to arm that projectile.
  • Safety and arming devices in general are responsible for four basic functions: discriminating, delaying, switching, and arming.
  • the device of the present invention is primarily concerned with the first of these functions: discriminating between environmental signatures peculiar to launch and accidental spurious signals that closely approximate the desired signatures.
  • the safety of a munitions round rests, in a large part, on the ability of the associated discriminating system to positively determine when launching has occurred. Once the signals associated with launching are sensed, a safety and arming device will process the signals by a time delay and switching scheme in order to arm the projectile in manners well known in the art.
  • a further object of the present invention is to provide a nonmechanical device for use in safety and arming systems that has no moving parts therein and is thus subject to a minimum of deterioration and wear.
  • an electronic device for use in a munition fuze safety and arming system.
  • the device senses and processess electronic signatures derived from and peculiar to the projectiles launching conditions. These signatures are sensed and recognized by the device in an electronic discriminatory manner heretofore unobtained.
  • the device in a preferred embodiment form uses two transducers that must sense two distinct signatures associated with launching and that occur in a particular time sequence in order for the device to generate an arming signal.
  • Signal conditioning means that only pass signatures of certain preselected time or voltage levels act on the basic transducergenerated signals to discriminate against unwanted spurious signals and thus enhance the safety of the unit.
  • the discriminatory scheme of the invention is readily integrated with other electronic fuze safety elements. Fuzes incorporating the invention are sensitive, effective, and economical to manufacture.
  • FIG. 1 is a block diagram of a discriminatory scheme in accordance with the invention
  • FIG. 2 is a schematic diagram of a preferred embodiment of the device of FIG. 1;
  • FIG. 3 is a schematic diagram of the device of FIG. 2 further incorporating additional discriminatory circuitry to enhance the safety of the device.
  • FIG. 1 illustrates in a block diagram form the basic principle behind the electronic sensing and decision-making device suitable for ammunition use.
  • two transducers each of which is used to detect a distinct launching condition which is transformed into a useable signal by signal processing or conditioning means 14 and 16, respec tively.
  • the detectable launching conditions could be, for example, setback acceleration. shell vibrations, muzzle flash or an environmental change due to the shell leaving the gun's barrel.
  • a gate 18 is responsive to the outputs of transducers l0 and 12 such that it provides a signal to the delay and arming device 20 only when the signal conditioning circuits l4 and 16 deem the detected signatures valid.
  • Gate 18 can be made responsive only to a certain time sequence of the signatures generated by transducers l0 and 12 which would provide ad ditional discrimination against unwanted or spurious signa tures. Thus, in order for the delay and arming device 20 to receive any signal whatsoever, the signatures corresponding to the certain events during launch must occur in a certain order and within certain time intervals.
  • FIG. 2 shows a basic electronic schematic incorporating the features of FIG. 1, in which transducer 10 of FIG. 1 is a piezoelectric crystal 22 and transducer 12 of FIG. 1 is a coil and magnet 24. While experiencing setback generated by launching, crystal 22 generates a charge which energizes a firing capacitor C,. The signal generated by crystal 22 is rectified by a diode D, and the time required to charge capacitor C, is controlled by the time constant R,C,.
  • Coil and magnet 24 is arranged in the projectile so as to experience a change in its electrical reluctance when leaving the weapons barrel.
  • An example of such a sensing device can be found in U.S. Pat. No. 3,417,700 by .I. J. Furlani entitled Fuze Arming System.
  • the change in reluctance of coil 24 generates a voltage which turns ON the silicon controlled rectifier 5,, thus delivering the energy stored in the capacitor C, to the output terminals 28.
  • the silicon controlled rectifier S operates in the manner of a switch in that a signal appearing at the anode 30 of S, will not travel through the device until a control signal is received on the gate 26. Upon receipt of such a control signal, the device 8, will conduct current, switching from an OFF condition to an ON condition.
  • a resistor R will dissipate any charge stored by capacitor C, in the event switch S, does not receive a signal on its gate 26 within the time interval given by time constant R C,. If a signal is received by gate 26, the resultant electrical energy appearing at output terminals 28 is used to initiate the operation of delay and arming device 20. This energy may for example initiate a chemical or explosive transducer, or provide a start ing pulse for a timer, or be used for any number of wellestablished arming schemes known in the art. It is seen in the embodiment of FIG. 2 that setback must first occur and then the projectile must leave the weapons barrel in order for an arming signal to be generated and released.
  • the chargedischarge time constants controlled by the values of the resistive and capacitive components R,, R and C, provide simple signal conditioning means corresponding to block 14 of FIG. 1 whereby bore and storage safety can be assured.
  • FIG. 3 can be found a more sophisticated embodiment which illustrates an electronic circuit that imposes more stringent requirements that a signal sensed by either transducer must meet prior to its being detectable as a valid command signal. It is assumed that the various parameters involved with the particular weapon, barrel and shell have already been carefully taken into consideration in that the detectable voltage limits of acceleration setback and barrel exit velocity have been established for a particular combination of the above parameters and have been used judiciously in the selection of component values for a particular circuit of the type as presented in FIG. 3.
  • the output of the setback sensing crystal 22 is rectified by a diode D, and time integrated by a resistor R, and a capacitor C,. If the acceleration sensed by crystal 22 is greater than the specified upper limit, the amplitude of the resultant signal will cause a Zener diode Z, to conduct which will turn ON switch 8,, by means of gate 36 just long enough to dump the charge stored on capacitor C, as a result of the false signal. On the other hand, if the signal developed by crystal 22 falls below the upper limit and above the lower limit, i.e. if the acceleration meets the minimum specification, the resultant signal will cause Zener diode Z to conduct which closes switch S by means of gate 38, thus providing a signal at the anode 30 of switch 5,.
  • switch S remains OFF until such time as a signal is received by gate 26.
  • capacitor C will gradually discharge through resistor R and also through Zener diode Z and resistor R
  • the gate 26 must be triggered before capacitor C, discharges and while Zener diode Z is conducting in order for the delay and arming device to receive a command signal by way oflines 28.
  • the magnet and coil arrangement at 24 is responsible for generating the voltage necessary to close switch S, by way of gate 26.
  • Capacitor C will be charged up by the voltage generated when the round leaves the end of the gun barrel. Ifa voltage is generated by coil 24 that is greater than that specified for the specific gun-barrel arrangement, i.e. if a high voltage spurious signal is detected, Zener diode Z will conduct current through gate 40 and thus turn ON switch S, which acts to short circuit coil 24 and thus discharge capacitor C However, if the generated voltage falls below the upper limit and above the lower limit. i.e.
  • Zener diode Z will swing into conduction and turn ON transistor T, which provides current amplification for the signal and turns ON switch S, by Way of gate 26. If gate 26 has received a signal, i.e. if the round has left the gun barrel, before the charge on capacitor C, drops below the threshold of Zener diode Z current will flow through switch S, to actuate the delay and arming device 20 by way ofwires 28.
  • circuit of FIG. 3 is only typical of an entire family of circuits that may be built to perform the functions according to FIG. I.
  • the threshold devices would probably be biased amplifiers rather than Zener diodes.
  • switch S of FIG. 3 could be connected so as to enable another transducer such as a fluidic power supply.
  • other transducers could be substituted or added to the present scheme in order to increase the safety of the system.
  • a strain gauge could be added that would sense shell vibrations, or an optical sensor which would see muzzle flash could be substituted for either transducer.
  • a single multipurpose transducer could be utilized in a series configuration as a discriminatory device to activate the logic circuitry.
  • Another basic modification would be to utilize external power supplies to power the system rather than the selfgenerating transducers l0 and 12 of FIG. 1.
  • passive transducers could be substituted for either transducer shown.
  • certain power requirements would permit the use of the output of the self-generating transducers as the power supply for the system.
  • the signal conditioning means could be extended to include, for example, doubly-integrating a signal received from acceleration sensitive transducers. The integrated signal would be an indication of the distance the shell has traveled from the weapon and would provide a delay function for the safety and arming device.
  • An electronic device for use in an ordnance fuze safety and arming system comprising:
  • first and second transducers responsive to launching conditions of said ordnance fuze for generating signals providing first and second environmental signatures
  • first and second signal processing means adapted to act on said first and second environmental signature signals, respectively, in order to electronically discriminate against and prohibit passage of signals indicative of nonlaunch signatures;
  • an electronic gate adapted to receive said first and second environmental signature signals from said first and second signal processing means, respectively, and to provide an output signal for arming means only upon plural receipt of said signatures.
  • said first transducer comprises a piezoelectric crystal adapted to sense the acceleration setback of said ordnance fuze and to generate said signals of the first environmental signature in proportion thereto.
  • said second transducer comprises a magnet and coil adapted to sense when said ordnance fuze exits from the gun barrel from which it is launched and to generate said signals of the second environmental signature in proportion thereto.
  • said electronic gate comprises a silicon controlled rectifier adapted to receive said signals of the first environmental signature on its anode and said signals of the second environmental signature on its gate whereby said output signal issues from its cathode only upon plural receipt of said signals of the first and second environmental signatures.
  • said first signal processing means comprises a storage capacitor to store a charge generated by said first transducer, a plurality of electronic switches and threshold devices to prohibit passage of any electronic signal that does not fall within prespecified voltage levels and time intervals, and which delivers passable signals to said anode of said silicon controlled rectifier.
  • said second signal processing means comprises a storage capacitor to store a charge generated by said second transducer, a plurality of electronic switches and threshold devices to prohibit passage of any electronic signal that does not fall within prespecified voltage levels and time intervals, and which delivers passable signals to said gate of said silicon controlled rectifier, whereby the receipt of said signal on said gate will release said signal on said cathode and deliver said output signal for the arming means.
  • a. means for generating a plurality of electronic signals arming means for receiving a Signal from Said gating when id ordnance f i launched; means only upon the plural receipt by said gating means of all of said plurality of electronic signals.

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Abstract

An all-electronic device for the detection and processing of those environmental signatures associated with the launching of a munitions round. The non-mechanical device imposes stringent requirements that the environmental signatures must meet before the device will issue a command signal to arm the round. Two transducers are utilized to sense two distinct conditions that are peculiar to the round''s launching. In a particular embodiment, the two transducers used are a piezoelectric crystal that senses acceleration setback and a magnet and coil arrangement that is triggered when the round leaves the gun barrel. Furthermore, the environmental signatures that are sensed must fall within certain voltage ranges and time intervals that have been preselected according to the particular weapon and round combination under consideration. When the various signals meet all requirements, the device will provide a useable signal for any subsequent delay and arming function of the round.

Description

States atet Furlani et a1.
3,359,904 12/1967 Nerheim. 2,555,384 6/1951 Watt 2,640,417 6/1953 Bjork et a1 102/702 GA ELECTRONIC DEVICE APPLICABLE TO ORDNANCE SAFETY AND ARMING SYSTEMS Inventors: John J. Furlani, Rockville; Harry J. Davis, Wheaten, both of Md.; Philip Ingersoll, Fairfax, Va.
Assignee: The United States of America as represented by the Secretary of the Army Filed: Feb. 10, 1970 App1.N0.: 110,173
US. Cl. ..l02/70.2 R
Int. Cl ..F42e l1/02, F42c 1l/06, F42c 15/40 Field of Search ..102/70.2 G
References Cited UNITED STATES PATENTS Haiken ..102/70.2 GA
Primary Examiner-Samuel F einberg Assistant Examiner-Thomas H. Webb Attorney-Harry M. Saragovitz, Edward J. Kelly, Herbert Her] and J. D. Edgerton [5 7] ABSTRACT An all-electronic device for the detection and processing of those environmental signatures associated with the launching of a munitions round. The non-mechanical device imposes stringent requirements that the environmental signatures must meet before the device will issue a command signal to arm the round. Two transducers are utilized to sense two distinct conditions that are peculiar to the rounds launching. in a particular embodiment, the two transducers used are a piezoelectric crystal that senses acceleration setback and a magnet and coil arrangement that is triggered when the round leaves the gun barrel. Furthermore, the environmental signatures that are sensed must fall within certain voltage ranges and time intervals that have been preselected according to the particular weapon and round combination under consideration When the various signals meet all requirements, the device will provide a useable signal for any subsequent delay and arming function of the round 7 Claims, 3 Drawing Figures SlGNAL N conomonme SDUCEQ DELAY AND MIMI NG ./-'ZO DEVlCE The invention described herein may be manufactured, used, and licensed by or for the United States Government for governmental purposes without the payment to us of any royalty thereon.
BACKGROUND OF THE INVENTION This invention relates generally to safety and arming devices for use in ordnance fuzing and, more particularly, to an allelectronic device that senses signatures peculiar to a projectiles launching which can be used to arm that projectile.
Safety and arming devices in general are responsible for four basic functions: discriminating, delaying, switching, and arming. The device of the present invention is primarily concerned with the first of these functions: discriminating between environmental signatures peculiar to launch and accidental spurious signals that closely approximate the desired signatures. The safety of a munitions round rests, in a large part, on the ability of the associated discriminating system to positively determine when launching has occurred. Once the signals associated with launching are sensed, a safety and arming device will process the signals by a time delay and switching scheme in order to arm the projectile in manners well known in the art.
Most discriminatory devices currently in use are mechanical in nature, employing such schemes as a mass suspended in a viscous fluid to sense a predetermined acceleration level of the projectile, or a spring or magnetically held mass that is responsive to the setback force at launch or the centrifugal forces encountered by a spin-operated projectile Due to mechanical complexity and to the fact that appreciable movement is involved, these devices tend to lack ruggedness. Additionally, accidental dropping or the like may be sufflcient to cause such a device to arm. These problems have led to the use of supplementary mechanical means that must, for example, be manually operated before the projectile is placed in the launcher for firing. Such auxiliary means often merely add to the complexity of the device while offering little additional protection against severe vibrations or shocks that the projectile may be subjected to prior to firing. Additionally, such mechanical devices are apt to lose efficiency and reliability upon exposure to environmental temperature and pressure extremes.
Accordingly, it is a primary object of this invention to provide a nonmechanical device for use in a safety and arming system that is insensitive to spurious shock and vibration prior to launching.
It is another object of this invention to provide a nonmechanical device for use in safety and arming systems that electronically senses and discriminates in favor of conditions peculiar to a projectiles launching as prerequisites to the arming ofthe projectile.
A further object of the present invention is to provide a nonmechanical device for use in safety and arming systems that has no moving parts therein and is thus subject to a minimum of deterioration and wear.
SUMMARY OF THE INVENTION Briefly, in accordance with the invention, an electronic device is provided for use in a munition fuze safety and arming system. The device senses and processess electronic signatures derived from and peculiar to the projectiles launching conditions. These signatures are sensed and recognized by the device in an electronic discriminatory manner heretofore unobtained. The device in a preferred embodiment form uses two transducers that must sense two distinct signatures associated with launching and that occur in a particular time sequence in order for the device to generate an arming signal. Signal conditioning means that only pass signatures of certain preselected time or voltage levels act on the basic transducergenerated signals to discriminate against unwanted spurious signals and thus enhance the safety of the unit. The discriminatory scheme of the invention is readily integrated with other electronic fuze safety elements. Fuzes incorporating the invention are sensitive, effective, and economical to manufacture.
BRIEF DESCRIPTION OF THE DRAWINGS The specific nature of the invention as well as other objects. aspects, uses, and advantages thereof will clearly appear from the following description and from the accompanying draw ing, in which:
FIG. 1 is a block diagram of a discriminatory scheme in accordance with the invention;
FIG. 2 is a schematic diagram ofa preferred embodiment of the device of FIG. 1; and
FIG. 3 is a schematic diagram of the device of FIG. 2 further incorporating additional discriminatory circuitry to enhance the safety of the device.
DESCRIPTION OF PREFERRED EMBODIMENT FIG. 1 illustrates in a block diagram form the basic principle behind the electronic sensing and decision-making device suitable for ammunition use. At 10 and 12 are shown two transducers, each of which is used to detect a distinct launching condition which is transformed into a useable signal by signal processing or conditioning means 14 and 16, respec tively. The detectable launching conditions could be, for example, setback acceleration. shell vibrations, muzzle flash or an environmental change due to the shell leaving the gun's barrel. A gate 18 is responsive to the outputs of transducers l0 and 12 such that it provides a signal to the delay and arming device 20 only when the signal conditioning circuits l4 and 16 deem the detected signatures valid. Gate 18 can be made responsive only to a certain time sequence of the signatures generated by transducers l0 and 12 which would provide ad ditional discrimination against unwanted or spurious signa tures. Thus, in order for the delay and arming device 20 to receive any signal whatsoever, the signatures corresponding to the certain events during launch must occur in a certain order and within certain time intervals.
FIG. 2 shows a basic electronic schematic incorporating the features of FIG. 1, in which transducer 10 of FIG. 1 is a piezoelectric crystal 22 and transducer 12 of FIG. 1 is a coil and magnet 24. While experiencing setback generated by launching, crystal 22 generates a charge which energizes a firing capacitor C,. The signal generated by crystal 22 is rectified by a diode D, and the time required to charge capacitor C, is controlled by the time constant R,C,.
Coil and magnet 24 is arranged in the projectile so as to experience a change in its electrical reluctance when leaving the weapons barrel. An example of such a sensing device can be found in U.S. Pat. No. 3,417,700 by .I. J. Furlani entitled Fuze Arming System. The change in reluctance of coil 24 generates a voltage which turns ON the silicon controlled rectifier 5,, thus delivering the energy stored in the capacitor C, to the output terminals 28. The silicon controlled rectifier S, operates in the manner of a switch in that a signal appearing at the anode 30 of S, will not travel through the device until a control signal is received on the gate 26. Upon receipt of such a control signal, the device 8, will conduct current, switching from an OFF condition to an ON condition. Hereinafter, we shall refer to the silicon controlled rectifiers as simply switches.
A resistor R will dissipate any charge stored by capacitor C, in the event switch S, does not receive a signal on its gate 26 within the time interval given by time constant R C,. If a signal is received by gate 26, the resultant electrical energy appearing at output terminals 28 is used to initiate the operation of delay and arming device 20. This energy may for example initiate a chemical or explosive transducer, or provide a start ing pulse for a timer, or be used for any number of wellestablished arming schemes known in the art. It is seen in the embodiment of FIG. 2 that setback must first occur and then the projectile must leave the weapons barrel in order for an arming signal to be generated and released. The chargedischarge time constants, controlled by the values of the resistive and capacitive components R,, R and C,, provide simple signal conditioning means corresponding to block 14 of FIG. 1 whereby bore and storage safety can be assured.
In FIG. 3 can be found a more sophisticated embodiment which illustrates an electronic circuit that imposes more stringent requirements that a signal sensed by either transducer must meet prior to its being detectable as a valid command signal. It is assumed that the various parameters involved with the particular weapon, barrel and shell have already been carefully taken into consideration in that the detectable voltage limits of acceleration setback and barrel exit velocity have been established for a particular combination of the above parameters and have been used judiciously in the selection of component values for a particular circuit of the type as presented in FIG. 3.
In operation, the output of the setback sensing crystal 22 is rectified by a diode D, and time integrated by a resistor R, and a capacitor C,. If the acceleration sensed by crystal 22 is greater than the specified upper limit, the amplitude of the resultant signal will cause a Zener diode Z, to conduct which will turn ON switch 8,, by means of gate 36 just long enough to dump the charge stored on capacitor C, as a result of the false signal. On the other hand, if the signal developed by crystal 22 falls below the upper limit and above the lower limit, i.e. if the acceleration meets the minimum specification, the resultant signal will cause Zener diode Z to conduct which closes switch S by means of gate 38, thus providing a signal at the anode 30 of switch 5,. As previously pointed out, switch S, remains OFF until such time as a signal is received by gate 26. As long as S, is OFF, capacitor C, will gradually discharge through resistor R and also through Zener diode Z and resistor R Thus the gate 26 must be triggered before capacitor C, discharges and while Zener diode Z is conducting in order for the delay and arming device to receive a command signal by way oflines 28.
The magnet and coil arrangement at 24 is responsible for generating the voltage necessary to close switch S, by way of gate 26. Capacitor C will be charged up by the voltage generated when the round leaves the end of the gun barrel. Ifa voltage is generated by coil 24 that is greater than that specified for the specific gun-barrel arrangement, i.e. if a high voltage spurious signal is detected, Zener diode Z will conduct current through gate 40 and thus turn ON switch S, which acts to short circuit coil 24 and thus discharge capacitor C However, if the generated voltage falls below the upper limit and above the lower limit. i.e. if the rounds exit velocity is satisfactory, a Zener diode Z will swing into conduction and turn ON transistor T, which provides current amplification for the signal and turns ON switch S, by Way of gate 26. If gate 26 has received a signal, i.e. if the round has left the gun barrel, before the charge on capacitor C, drops below the threshold of Zener diode Z current will flow through switch S, to actuate the delay and arming device 20 by way ofwires 28.
Accidentally generated signals that might occur during the normal course of handling of a particular round would result in the charging of capacitors C, and C However, such a series of below threshold signals cannot gradually accumulate on these capacitors to a dangerous level due to the presence of resistors R and R which will dissipate any such low level signals, thus providing additional pre-launch safety.
It should be noted that the circuit of FIG. 3 is only typical of an entire family of circuits that may be built to perform the functions according to FIG. I. For example, if the circuit of FIG. 3 were to be built into an integrated circuit the threshold devices would probably be biased amplifiers rather than Zener diodes. Also, switch S of FIG. 3 could be connected so as to enable another transducer such as a fluidic power supply. Additionally, other transducers could be substituted or added to the present scheme in order to increase the safety of the system. For example, a strain gauge could be added that would sense shell vibrations, or an optical sensor which would see muzzle flash could be substituted for either transducer. Or, a single multipurpose transducer could be utilized in a series configuration as a discriminatory device to activate the logic circuitry. Another basic modification would be to utilize external power supplies to power the system rather than the selfgenerating transducers l0 and 12 of FIG. 1. In this case, passive transducers could be substituted for either transducer shown. Alternatively, certain power requirements would permit the use of the output of the self-generating transducers as the power supply for the system. Additionally, the signal conditioning means could be extended to include, for example, doubly-integrating a signal received from acceleration sensitive transducers. The integrated signal would be an indication of the distance the shell has traveled from the weapon and would provide a delay function for the safety and arming device.
We wish it to be understood that we do not desire to be limited to the exact details of construction shown and described, for obvious modifications will occur to a person skilled in the art.
We claim as our invention:
1. An electronic device for use in an ordnance fuze safety and arming system comprising:
a. first and second transducers responsive to launching conditions of said ordnance fuze for generating signals providing first and second environmental signatures;
b. first and second signal processing means adapted to act on said first and second environmental signature signals, respectively, in order to electronically discriminate against and prohibit passage of signals indicative of nonlaunch signatures; and
c. an electronic gate adapted to receive said first and second environmental signature signals from said first and second signal processing means, respectively, and to provide an output signal for arming means only upon plural receipt of said signatures.
2. The device according to claim 1 wherein said first transducer comprises a piezoelectric crystal adapted to sense the acceleration setback of said ordnance fuze and to generate said signals of the first environmental signature in proportion thereto.
3. The device according to claim 2 wherein said second transducer comprises a magnet and coil adapted to sense when said ordnance fuze exits from the gun barrel from which it is launched and to generate said signals of the second environmental signature in proportion thereto.
4. The device according to claim 1 wherein said electronic gate comprises a silicon controlled rectifier adapted to receive said signals of the first environmental signature on its anode and said signals of the second environmental signature on its gate whereby said output signal issues from its cathode only upon plural receipt of said signals of the first and second environmental signatures.
5. The device according to claim 4 wherein said first signal processing means comprises a storage capacitor to store a charge generated by said first transducer, a plurality of electronic switches and threshold devices to prohibit passage of any electronic signal that does not fall within prespecified voltage levels and time intervals, and which delivers passable signals to said anode of said silicon controlled rectifier.
6. The device according to claim 5 wherein said second signal processing means comprises a storage capacitor to store a charge generated by said second transducer, a plurality of electronic switches and threshold devices to prohibit passage of any electronic signal that does not fall within prespecified voltage levels and time intervals, and which delivers passable signals to said gate of said silicon controlled rectifier, whereby the receipt of said signal on said gate will release said signal on said cathode and deliver said output signal for the arming means.
7. An electronic device for use in an ordnance fuze safety 0. gating means for receiving those signals not inhibited by and arming system, comprising: said inhibiting means; and
a. means for generating a plurality of electronic signals arming means for receiving a Signal from Said gating when id ordnance f i launched; means only upon the plural receipt by said gating means of all of said plurality of electronic signals.
* t a: n:
b means for inhibiting those of said plurality of electronic 5 signals that fall beyond prespecified limits;

Claims (7)

1. An electronic device for use in an ordnance fuze safety and arming system comprising: a. first and second transducers responsive to launching conditions of said ordnance fuze for generating signals providing first and second environmental signatures; b. first and second signAl processing means adapted to act on said first and second environmental signature signals, respectively, in order to electronically discriminate against and prohibit passage of signals indicative of non-launch signatures; and c. an electronic gate adapted to receive said first and second environmental signature signals from said first and second signal processing means, respectively, and to provide an output signal for arming means only upon plural receipt of said signatures.
2. The device according to claim 1 wherein said first transducer comprises a piezoelectric crystal adapted to sense the acceleration setback of said ordnance fuze and to generate said signals of the first environmental signature in proportion thereto.
3. The device according to claim 2 wherein said second transducer comprises a magnet and coil adapted to sense when said ordnance fuze exits from the gun barrel from which it is launched and to generate said signals of the second environmental signature in proportion thereto.
4. The device according to claim 1 wherein said electronic gate comprises a silicon controlled rectifier adapted to receive said signals of the first environmental signature on its anode and said signals of the second environmental signature on its gate whereby said output signal issues from its cathode only upon plural receipt of said signals of the first and second environmental signatures.
5. The device according to claim 4 wherein said first signal processing means comprises a storage capacitor to store a charge generated by said first transducer, a plurality of electronic switches and threshold devices to prohibit passage of any electronic signal that does not fall within prespecified voltage levels and time intervals, and which delivers passable signals to said anode of said silicon controlled rectifier.
6. The device according to claim 5 wherein said second signal processing means comprises a storage capacitor to store a charge generated by said second transducer, a plurality of electronic switches and threshold devices to prohibit passage of any electronic signal that does not fall within prespecified voltage levels and time intervals, and which delivers passable signals to said gate of said silicon controlled rectifier, whereby the receipt of said signal on said gate will release said signal on said cathode and deliver said output signal for the arming means.
7. An electronic device for use in an ordnance fuze safety and arming system, comprising: a. means for generating a plurality of electronic signals when said ordnance fuze is launched; b. means for inhibiting those of said plurality of electronic signals that fall beyond prespecified limits; c. gating means for receiving those signals not inhibited by said inhibiting means; and d. arming means for receiving a signal from said gating means only upon the plural receipt by said gating means of all of said plurality of electronic signals.
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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3756157A (en) * 1971-07-30 1973-09-04 Westinghouse Electric Corp Solid state power supply activated by a pyrotechnic chain
US4019440A (en) * 1975-07-10 1977-04-26 General Dynamics, Pomona Division Impact discriminating apparatus for missiles and the like, and method for impact discrimination
US4141298A (en) * 1976-11-25 1979-02-27 Diehl Gmbh & Co. Electronic ignition circuit
FR2451135A1 (en) * 1979-03-05 1980-10-03 Mefina Sa DEVICE FOR TRANSMITTING SIGNALS TO A PROJECTILE ROCKET
EP0018246A1 (en) * 1979-04-20 1980-10-29 ETAT-FRANCAIS représenté par le Délégué Général pour l' Armement Igniter arrangement for omnidirectionally exploding antivehicle mines
US4311096A (en) * 1980-05-05 1982-01-19 Atlas Powder Company Electronic blasting cap
US4445435A (en) * 1980-05-05 1984-05-01 Atlas Powder Company Electronic delay blasting circuit
US5269223A (en) * 1992-10-06 1993-12-14 Ems-Patvag Piezoelectric fuse system with safe and arm device for ammunition
US5787785A (en) * 1995-09-28 1998-08-04 Oerlikon Contraves Pyrotec Ag Method and device for programming time fuses of projectiles
US20060090662A1 (en) * 2004-06-09 2006-05-04 Biggs Bradley M Method for detection of media layer by a penetrating weapon and related apparatus and systems
US20070204756A1 (en) * 2006-01-17 2007-09-06 Rastegar Jahangir S Energy harvesting power sources for generating a time-out signal for unexploded munitions
US20220120546A1 (en) * 2018-12-19 2022-04-21 Bae Systems Plc Techniques suitable for use with an object for moving through a fluid, such as a munition or reconnaissance projectile
US11859953B2 (en) 2018-12-19 2024-01-02 Bae Systems Plc Munition and munition assembly

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2555384A (en) * 1948-01-14 1951-06-05 Gordon J Watt Electrically set mechanical time fuse
US2640417A (en) * 1946-12-18 1953-06-02 Us Sec War Ignition safety device for induction fired rockets
US3353486A (en) * 1966-03-03 1967-11-21 Robert M Haiken Self-destructing fuze system for rotating projectiles
US3359904A (en) * 1966-07-05 1967-12-26 Honeywell Inc Piezoelectric projectile fuze

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2640417A (en) * 1946-12-18 1953-06-02 Us Sec War Ignition safety device for induction fired rockets
US2555384A (en) * 1948-01-14 1951-06-05 Gordon J Watt Electrically set mechanical time fuse
US3353486A (en) * 1966-03-03 1967-11-21 Robert M Haiken Self-destructing fuze system for rotating projectiles
US3359904A (en) * 1966-07-05 1967-12-26 Honeywell Inc Piezoelectric projectile fuze

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3756157A (en) * 1971-07-30 1973-09-04 Westinghouse Electric Corp Solid state power supply activated by a pyrotechnic chain
US4019440A (en) * 1975-07-10 1977-04-26 General Dynamics, Pomona Division Impact discriminating apparatus for missiles and the like, and method for impact discrimination
US4141298A (en) * 1976-11-25 1979-02-27 Diehl Gmbh & Co. Electronic ignition circuit
FR2451135A1 (en) * 1979-03-05 1980-10-03 Mefina Sa DEVICE FOR TRANSMITTING SIGNALS TO A PROJECTILE ROCKET
EP0018246A1 (en) * 1979-04-20 1980-10-29 ETAT-FRANCAIS représenté par le Délégué Général pour l' Armement Igniter arrangement for omnidirectionally exploding antivehicle mines
FR2454601A1 (en) * 1979-04-20 1980-11-14 France Etat IGNITION DEVICE FOR OMNIDIRECTIONAL ANTIHICLE MINES
US4311096A (en) * 1980-05-05 1982-01-19 Atlas Powder Company Electronic blasting cap
US4445435A (en) * 1980-05-05 1984-05-01 Atlas Powder Company Electronic delay blasting circuit
US5269223A (en) * 1992-10-06 1993-12-14 Ems-Patvag Piezoelectric fuse system with safe and arm device for ammunition
US5787785A (en) * 1995-09-28 1998-08-04 Oerlikon Contraves Pyrotec Ag Method and device for programming time fuses of projectiles
US20060090662A1 (en) * 2004-06-09 2006-05-04 Biggs Bradley M Method for detection of media layer by a penetrating weapon and related apparatus and systems
US7197982B2 (en) * 2004-06-09 2007-04-03 Alliant Techsystems Inc. Method for detection of media layer by a penetrating weapon and related apparatus and systems
US20070204756A1 (en) * 2006-01-17 2007-09-06 Rastegar Jahangir S Energy harvesting power sources for generating a time-out signal for unexploded munitions
US20100155473A1 (en) * 2006-01-17 2010-06-24 Rastegar Jahangir S Energy harvesting power sources for validating firing; determining the beginning of the free flight and validating booster firing and duration
US20100155472A1 (en) * 2006-01-17 2010-06-24 Rastegar Jahangir S Energy harvesting power sources for accidental drop detection and differentiation from firing
US7762192B2 (en) * 2006-01-17 2010-07-27 Omnitek Partners Llc Energy harvesting power sources for validating firing; determining the beginning of the free flight and validating booster firing and duration
US7762191B2 (en) * 2006-01-17 2010-07-27 Omnitek Partners, Llc Energy harvesting power sources for accidental drop detection and differentiation from firing
US20100251879A1 (en) * 2006-01-17 2010-10-07 Rastegar Jahangir S Energy harvesting power sources for assisting in the recovery/detonation of unexploded munitions governmental rights
US20110168046A1 (en) * 2006-01-17 2011-07-14 Omnitek Partners Llc Energy harvesting power sources for generating a time-out singal for unexploded munitions
US8191475B2 (en) * 2006-01-17 2012-06-05 Omnitek Partners Llc Energy harvesting power sources for generating a time-out signal for unexploded munitions
US8205555B1 (en) * 2006-01-17 2012-06-26 Omnitek Partners Llc Energy harvesting power sources for assisting in the recovery/detonation of unexploded munitions
US8701559B2 (en) * 2006-01-17 2014-04-22 Omnitek Partners Llc Energy harvesting power sources for detecting target impact of a munition
US20220120546A1 (en) * 2018-12-19 2022-04-21 Bae Systems Plc Techniques suitable for use with an object for moving through a fluid, such as a munition or reconnaissance projectile
US11846496B2 (en) * 2018-12-19 2023-12-19 Bae Systems Plc Techniques suitable for use with an object for moving through a fluid, such as a munition or reconnaissance projectile
US11859953B2 (en) 2018-12-19 2024-01-02 Bae Systems Plc Munition and munition assembly

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