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Publication numberUS3902172 A
Publication typeGrant
Publication dateAug 26, 1975
Filing dateMar 29, 1962
Priority dateMar 29, 1962
Publication numberUS 3902172 A, US 3902172A, US-A-3902172, US3902172 A, US3902172A
InventorsHolmes Daniel D, Weiss Albert
Original AssigneeUs Navy
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Infrared gated radio fuzing system
US 3902172 A
Abstract  available in
Previous page
Next page
Claims  available in
Description  (OCR text may contain errors)

United States Patent Weiss et al.

[ 1 Aug. 26, 1975 Primary Examiner-T. H. Tubbesing [54] INFRARED GATED RAD) FUZING 1. In an infrared gated radio fuzing system for use in a SYSTEM guided missile the combination comprising: [75] Inventors: Albert Weiss; Daniel D. Holmes, first ermal-energy .detecnilg means for both of Riverside Calm producing A an output signal 1n response to v intercepted thermal-energy radlated from a [73] Assignee: The United States of America as thermapen'ergy radiating object represented y the Secretary of the b. second circuit means for detecting radio energy Navy, Washington, reflected from said thermal-energy radiating 22 Filed: Mar. 29, 1962 oblect c. pulse generator means coupled to said l PP NOJ 183,681 thermal-energy detecting means for generating an output pulse having a time duration 52 US. Cl. 343/6 ND; 102/702 P; 343/7 PF aRpfioximtely equal 9 the time required for [51 l n F42C 13/04 missile to traverse a distance of half the length of 581 Field of Search 343/6 ND, 13 SA; Oblect,

102/702 P 7 PF d. switching means coupled to said pulse generator means and to said second circuit means and being [56] References Cited resporsive to said outpu:1 Luise for activating satid UNITED STATES PATENTS secon c1rcu1t means an emg responsive to t e cessation of sald pulse for de-actlvatmg said 3,010,102 ll/l96l Ketchlcdge et al. 343/6 ND second circuit means 3 046 892 7/1962 Cosse et al 343/13 SA X i e. third circuit means responsive to an output signal 3,108,270 l0/1963 Fairbanks 343/6 ND 3,169,726 2/1965 Jackson... 343/6 ND x 3 S fecond f fs 3568,1235 3/1971 Page 343/6 ND ewe F etecte predetermined time interval for actuatmg a detonation circuit.

Attorney, Agent, or Firm-Richard S. Sciascia; Joseph M. St.Amand; T. M. Phillips 2 Claims, 1 Drawing Figure EXEMPLARY CLAIM RADIO DETECTOR INFRARED DETECTOR CIRCUIT PATENTED M182 61975 I6 INFRARED RADIO DETECTOR DETECTOR Q I L I 20 24 I f Y AMPLIFIER V AND 52:1? SWITCH AMPLIFIER SHAPER DIETONATION CIRCUIT ALBERT WEISS DANIEL D. HOLMES INVENTORS ATTORNEYS INFRARED GATED RADIO FUZING SYSTEM The invention herein described may be manufactured and usedby or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.

The present invention relates to an infrared gated radio fuzing system and more particularly to an infrared gated radio fuzing system which will minimize the probability of premature fuze detonation or fuze deac tivation (dudding) because of the influence of undesired signals.

The primary objective of a fuzing system is to effect detonation of a warhead at the proper time to inflict maximum damage to the target. To insure the achievement of this objective, unrelated (to the target) signals must be prevented from triggering the firing circuit and causing premature detonation as in some cases deactivation (dudding). These undesired signals may originate internally because of microphony or other circuit defects; or they may be caused by external influences such as false targets or enemy countermeasure action.

In all known systems using active, passive, semiactive channels or any combination of these, the overall system is susceptible to interference from internal and external disturbances such as microphony, shock and vibration, extraneous radiation within the system pass band, and enemy countermeasure action specifically designed to deactivate or prematurely detonate the warhead. Any of these disturbances can modify or negate the overall operation of the fuzing system and prevent it from responding to the desired signals from the missile target.

In the specific cases of those fuzing systems using active or semi-active channels, the energy radiation from or incident to these channels is susceptible to enemy detection at all times. This beacon effect enables the enemy to take appropriate countermeasures action against missile guidance and/or fuzing.

Accordingly an object of the present invention is the provision of a fuzing system which reduces to a minimum the probability or premature fuze detonation or fuze deactivation because of the influence of undesired signals.

Another object is to provide a fuzing system which reduces to a minimum the probability of premature fuze detonation or fuze deactivation because of the influence of active or enemy countermeasures, external disturbances from sources other than the desired target and internal disturbances from microphonics of circuitry and associated components or other undesired internal signals.

Other objects and many of the attendant advantages of this invention will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein there is shown in the single FIGURE a block diagram of the preferred embodiment of the invention.

Referring to the FIGURE there is shown an infrared channel and a radio channel 12. Channel 10 is passive and responds to energy radiated from target 14 represented by line 11 in the infrared range. Channel 12 is an active channel but is inoperative until turned on by a suitable signal from channel 10. Channel 10 includes a detector 16 for detecting infrared energy received from a target, an amplifier 18 for amplifying and shaping the detected signal and a pulse generator 20 for generating a pulse in response to the detected signal. Channel 12 includes a radio transmitter and detector 22 for transmitting and detecting radio energy, an amplifier 24 for amplifying the detected signals, and a detonation circuit 26 for activating the warhead fuze. Switch 28 is coupled between pulse generator 20 of channel 10 and radio transmitter and detector 22 of channel 12 for activating channel 12 when the appropriate pulse is received from pulse generator 20.

ln operation, the optical portion of detector 16 should be arranged to detect target radiation at a lock forward angle of about.45. The look angle being so restricted that the radiation is detected in the interval slightly prior to the actual missile target intercept. Energy radiation from target 14 is detected and converted by detector 16 into a voltage pulse which is amplified and shaped in amplifier 18 which may be of any well known type to a waveshape suitable to trigger pulse generator 20. When triggered, pulse generator 20 which may be a monastable multivibrator similar to circuit 15 and page 12 of Military Standard Circuits (Mil-STD-439A(WEP), Government Printing Office, produces a pulse of a duration, T approximately equal to the time required for the missile to cover a distance of half the length of the shortest target expected to be encountered. The pulse from generator 20 actuates switch 28 which activates channel 12 for the duration, T Switch 28 may be any of the switching circuits shown in FIG. 60.2 on Page 6-50 of A Handbook of Selected Semiconductor Circuits; NAVSHlPS 93484, Department of the Navy. Switch 28 may turn on a power supply or remove a blocking bias which energizes transmitter and detector 22. Radio channel 12 will transmit and receive for the time, T,. The time for a radio wave to travel from the transmitter of channel 12 to a target and return is short as compared with the time, T Should a signal reflected from target 14 have the characteristics of a desired target, amplifier 24 passes and amplifies this signal to provide an input to detonation circuit 26 which detonates the warhead at a suitable point to kill the desired target. Transmitter and detector 22, amplifier 24 and detonation circuit 26 may be designed to discriminate against unwanted signals in any well known radio fuzing techniques. In its simplest form this could be the system used in the original proximity fuze shown and described in Radio Proximity Fuze Development by W. S Hinman and Cledo Brunetti, Proceedings Institute of Radio Engineers, 1946. Should detector 16 receive radiation from a false target or should channel 10 be actuated by internal noise or malfunction, in the absence of a target which channel 12 will recognize as a desired target, no detonation signal will be produced. At the end of pulse T channel 12 is turned off and the system reverts to the original state of passive operation with only channel 10 operating.

Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.

What is claimed is:

1. In an infrared gated radio fuzing system for use in a guided missile the combination comprising:

a. first thermal-energy detecting means for producing an output signal in response to intercepted ther- 3 4 mal-energy radiated from a thermal-energy radiatsecond circuit means and being responsive to the ing object, cessation of said pulse for die-activating said second b. second circuit means for detecting radio energy Circuit mums reflected from said thermal-energy radiating obe. third circuit means responsive to an output signal from said second circuit means in the event a desired target is detected during said predetermined time interval for actuating a detonation circuit.

2. The system of claim 1 wherein said first circuit ject, 5 c. pulse generator means coupled to said thermalenergy detecting means for generating an output pulse having a time duration approximately equal to the time required for the missile to traverse a distance of half the length of the radiating object, means Includes an infrared optical detector oriented so d. switching means coupled to said pulse generator that it has a angle of 450 with respect to the means and to said second circuit means and being j K be detectedresponsive to said output pulse for activating said

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US3010102 *Jul 5, 1947Nov 21, 1961Bell Telephone Labor IncCombination radar and thermalenergy detection system
US3046892 *Jun 18, 1959Jul 31, 1962Trt Telecom Radio ElectrProximity fuse
US3108270 *Dec 23, 1954Oct 22, 1963North American Aviation IncInterlocked radar and infrared detector system
US3169726 *Oct 3, 1955Feb 16, 1965Jackson Charles HMissile guidance system
US3568185 *Mar 30, 1964Mar 2, 1971North American RockwellMapping signal display apparatus
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US4422075 *May 21, 1981Dec 20, 1983Honeywell Inc.Proximity monitor
US4627351 *Sep 4, 1984Dec 9, 1986U.S. Philips CorporationFuse for projectiles
US4651647 *Apr 1, 1985Mar 24, 1987Werkzeugmaschinenfabrik Oerlikon-Buehrle AgAdjustable range proximity fuze
US4765244 *Mar 6, 1986Aug 23, 1988Spectronix Ltd.Apparatus for the detection and destruction of incoming objects
US4991508 *Dec 18, 1989Feb 12, 1991General Electric CompanyWarhead of a missle engaging an airborne target
US5147977 *Aug 17, 1990Sep 15, 1992Sensys AgDevice for the detection of objects and the release of firing for ground-to-air mines to be fired in the helicopter combat
US5301613 *Sep 14, 1992Apr 12, 1994Hughes Aircraft CompanyPower supply for an electrical circuit mounted on a projectile
US5371502 *Sep 22, 1992Dec 6, 1994Diehl Gmbh & Co.Method for the activation of a mine
US5406287 *Dec 22, 1993Apr 11, 1995The United States Of America As Represented By The Secretary Of The Air ForceProgrammable airdrop infrared decoy
US5796029 *Jul 7, 1995Aug 18, 1998Daimler-Benz Aerospace AgProximity fuse/time fuse for missiles
US7400289 *Sep 27, 2006Jul 15, 2008Lockheed Martin CorporationPlume-to-hardbody offset compensation in boosting missiles
US8120524 *Oct 11, 2006Feb 21, 2012Bae Systems Information And Electronic Systems Integration Inc.Motion detection systems using CW radar in combination with additional sensors
EP0139322A1 *Sep 4, 1984May 2, 1985Philips Norden ABA fuse for projectiles
EP0308324A1 *Sep 14, 1988Mar 22, 1989Societe De Fabrication D'instruments De Mesure (S.F.I.M.)Doppler speed measurement apparatus for security
EP0418566A1 *Aug 20, 1990Mar 27, 1991SenSys AGDetection device for the typical signals of a helicopter and for firing ground-air mines
U.S. Classification342/53, 102/213, 102/214, 342/68
International ClassificationF42C13/00, F42C13/04
Cooperative ClassificationF42C13/04
European ClassificationF42C13/04