US3844217A - Controlled range fuze - Google Patents

Controlled range fuze Download PDF

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Publication number
US3844217A
US3844217A US00292966A US29296672A US3844217A US 3844217 A US3844217 A US 3844217A US 00292966 A US00292966 A US 00292966A US 29296672 A US29296672 A US 29296672A US 3844217 A US3844217 A US 3844217A
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United States
Prior art keywords
conductors
counter
fuze
coupled
input terminal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
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US00292966A
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English (en)
Inventor
R Ziemba
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General Electric Co
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General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US00292966A priority Critical patent/US3844217A/en
Priority to IT29105/73A priority patent/IT993255B/it
Priority to GB4491973A priority patent/GB1450406A/en
Priority to DE2348365A priority patent/DE2348365C2/de
Priority to FR7334625A priority patent/FR2201452B1/fr
Priority to SE7313251A priority patent/SE409242B/sv
Priority to JP10860073A priority patent/JPS5712959B2/ja
Priority to US05/420,358 priority patent/US3955069A/en
Application granted granted Critical
Publication of US3844217A publication Critical patent/US3844217A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C11/00—Electric fuzes
    • F42C11/06—Electric fuzes with time delay by electric circuitry

Definitions

  • FIG. I is a schematic view of the chronology of the flight of a fuze embodying this invention.
  • FIG. 2A is a block diagram of the fuze of FIG. 1;
  • FIG. 2B is a block diagram of a detail of FIG. 2A;
  • FIG. 3 is a longitudinal view of a fuze embodying this invention.
  • FIG. 4 is a transverse view of a first embodiment of a mechanical encoder for the fuze of FIG. 2;
  • FIG. 5 is a longitudinal view of theencoder of FIG. 4.
  • FIG. 6 is a perpsective view of the encoder of FIG. 4.
  • FIGS. 7A, 7B and 7C illustrate the construction of a second embodiment of a mechanical encoder for the fuze of FIG. 2;
  • FIG. 8 is a table of numeric to digital logic for the encoder of FIG. 7C;
  • FIG. 9 illustrates the construction of a variant of the second embodiment of the encoder of FIG. '7C
  • FIG. 10 illustrates the penciling-in of a number on the encoder of FIG. 9.
  • FIG. 11 is a block diagram of a detail of a variant of the fuze of FIG. 2A.
  • the weapon system embodying this invention is similar in physical appearance to that shown in Ser. No. 843,478, now US. Pat. No. 3,7l4,898, except that the fuze I0 includes a mechanical encoder 12 to preset the main counter 14, which counter controls the interval of flight to detonation of the fuze.
  • the weapon system includes a command system which includes a ranging device, such as a laser 16, for ranging both the target and the projectile.
  • the ranging device is coupled to a computer 18 which controls a pulse transmitter 20 which feeds a transmitting antenna 22.
  • the weapon system further includes a projectile launching device such as a gun 24 which launches one or a plurality of projectiles, each containing a respective fuze 10, at the target.
  • the fuze may be manually or automatically mechanically set before projectile launch to a predicted interval of flight based upon fire control computed data.
  • the fuze will detonate the projectiles warhead at the end of that interval in the absence of a correction received by the fuze during its flight to the target.
  • This mechanical setting operation serves both as a coarse interval setting and as a back-up mode of operation in the event of a faulty electronic data link between and including the command system and the fuze.
  • the data link will provide corrected interval to detonation data to the fuze prior to the detonation time which was predetermined by the mechanical encoder.
  • the fuze 10 includes a housing 26, which may be secured into the warhead of the projectile, and which includes a receiver electronics assembly 28, a plurality of antenna ports 30, the encoder wheel assembly 12, a power supply here shown as an induction generator assembly 34, and a safing and arming mechanism 36.
  • the safimg and arming mechanism 36 may be of the type shown in my US. Pat. No. 3,608,494, issued Sept. 28, I97 I.
  • the induction generator assembly 34 may include a permanent magnet, a coil, a diode and a capaci tor, serving as the power supply to the fuze. The magnet is set back upon launch to generate a pulse in the coil which charges the capacitor.
  • the fuze 10 functionally includes an antenna 38, which in turn includes the ports 30, and which is coupled to the input terminal 40 of a detectoramplifier circuit 42 having an output terminal 44.
  • a launch-address register 46 has an input terminal 48 and an output group of terminals 50
  • a correctionaddress" register 52 has an input terminal 54 and an output group of terminals 56.
  • the two output groups of terminals 50 and 56 are coupled to respective input groups of terminals 58 and 60 of a comparitor circuit 62 which has an output terminal 64.
  • a local oscillator 66 has an output terminal 68 coupled to the input terminal 70 of a decade scaling circuit 72, whose. output terminal 74 is coupled to the input terminal 76 of the decade counter '14, whose output terminal 78 is coupled to the input terminal 80 of the firing circuit 82.
  • the decade mechanical encoder '12 is coupled to the decade counter 14 as shown in FIG. 6.
  • Time T which is the time of projectile launch, may be established for the purposes of the command system computer 18, by detecting the application of firing current to the round of ammunition when it is fired from the gun, and then allowing a predetermined interval for the projectile to leave the gun tube.
  • a pick-up coil may be located adjacent to the end of the gun tube to detect the passage of the projectile from the tube.
  • Time T is established for the purposes of the fuze by the set-back of the permanent magnet generating a pulse in the coil to charge the capacitor through the diode, and then allowing a predetermined interval for the projectile to leave the gun tube.
  • power may be supplied by a battery as shown in US. Pat. No. 3,608,494, supra.
  • Time T which is the time of detonation, is established by the full count configuration of the counter 14 created by the mechanical encoder l2, and the rate at which pulses are fed to the counter by the oscillator 66 via the scaler 72.
  • a random number address is to be inserted into the launch-address register 46 after launch and before the fuze enters the cloud of gun gas generated by the firing of the round.
  • This interval of time for addressing the register from the command system is defined by times T and T which are represented by signals which are tapped off from appropriate decades of the scaler 72 only during the first cycle of operation of the scaler. This is accomplished by a one-cycle only flip-flop assembly 84, which is shown in greater detail in P10. 23, and which has a T, input terminal 86, a T input terminal 88, and a T,T interval-on output terminal 90.
  • Terminal 90 is coupled to a first input terminal 92 of an AND gate 94, which has a second input terminal 96 coupled to the output terminal 44 of the detector amplifier 42, and an output terminal 98 coupled to the input terminal 48 of the launch-address register 46.
  • the AND gate 94 is enabled by the scaler 72, and is able to pass command pulses to the register 46.
  • the one-cycle-only flip-flop assembly 84 may be embodied as a first flip-flop 100, having a set input terminal 102, a reset input terminal 104, and a .l-output terminal 90; a second flip-flop 106 having a set input terminal 108, a reset input terminal 110, and a K-output terminal 112; and AND gate 114, having a first input terminal 86, a second input terminal 116, and an output terminal 118', and an OR gate 120, having a first input terminal 88, a second input terminal 122, and an output terminal 124.
  • Terminals 110 and 122 are coupled to the output terminal 126 of an infeed capacitor 128, and are turned on when power is initially applied to the circuit, thereby turning on terminal 112 and keeping terminal 90 off.
  • Terminals 118, 108 and 102 are intercoupled, and terminals 112 and 116 are intercoupled.
  • AND gate 114 conducts, turning on terminals 102 and 108, thereby turning on terminal 90 and turning off terminal 112, and thereby disabling the AND gate 114.
  • OR gate 120 conducts, turning on terminal 104, thereby turning off terminal 90.
  • terminal 112 remains off, and a T, signal cannot make the AND gate 114 conduct.
  • T T the projectile and the target may be tracked by the command system, and a corrected time to detonation may be determined.
  • a corrected time to detonation for a particular projectile in flight may be effected by forcing the counter 14 to a predetermined count at a predetermined interval of time prior to the corrected time of detonation.
  • a signal representative of time T is tapped off the counter 14 and coupled to the T input terminal 130 of flip-flop 132 which has a Joutput terminal 134.
  • Terminal 134 is coupled to a first input terminal 136 of an AND gate 138, having a second input terminal 140 coupled to the output terminal 44 of the detectoramplifier 42, and an output terminal 142 coupled to the input terminal 54 of the correction-address register 52.
  • the T tapoff may be chronological variable responsive to the interval set into the counter 14 by the mechanical encoder 12. From time T, on, the AND gate 138 is enabled, and the remote command system is able to transmit addresses into the correction-address register 52. Should the remote command system transmit an address into the register 52 which is identical to the ad dress initially inserted, during the interval T,T into the register 46, the comparitor 62 will detect this identity and provide an output signal, at a time defined as T.,, to the counter, forcing the counter, irrespective of the count already therein, to a count which is a predetermined count less than the full capacity of the counter.
  • the counter Since the counter is filled at a fixed rate by the oscillator 66 via the scaler 72, the counter will provide a signal at its output terminal 78, at a time T,, which occurs at a fixed interval of time after T,. This last interval may be in the order of a tenth of a second.
  • each fuze is given a different address during its respective T,-T, interval, which uniquely identifies it, and only that address, during the respective T T, interval, can cause the generation of the respective T signal to change the time of detonation of that fuze.
  • FIGS. 4, 5 and 6 A first embodiment of the mechanical encoder is shown in FIGS. 4, 5 and 6.
  • the encoder includes a stationary upper disk 100, a stationary lower disk 102, and an annulus 104 which is concentric with the disks and is journaled for rotation between the disks.
  • a resilient pressure wheel 106 is eccentric with the annulus and is journaled for rotation between the disks.
  • a plurality of electrically conductive, mutually isolated, conductors 108 are disposed on the periphery of the wheel 106 and bears against the inner wall 110 of the annulus.
  • a like plurality of contacts 112 is mounted on a contact block 114 and respectively bears against the plurality of conductors 108.
  • An outer C-shaped tape shield 116 is fixed between the disks and is open adjacent the zone of engagement.
  • An inner, C- shaped, tape shield 118 is also fixed between the disks and is open adjacent the zone of engagement between the wheel and the annulus.
  • a tape 120 is captured between the wheel 106 and the annulus wall 110. Each end of the tape is fixed to a respective pin 122, 124, which are respectively fixed between the disks.
  • the inner face 126 of the tape carries a plurality of transverse, conductive segments 128, adapted to engage various ones on the conductors 108 on the wheel, in code-combinations.
  • the outer face 130 of the tape carries a plurality of printed time indicia, each representative of the particular code-combination of segments on the reverse side.
  • the annulus 104 may be made of a translucent material such as a hard, clear plastic, whose inner surface is frosted. This will allow only that portion of the tape face 130 which is pressed against the inner surface of the annulus by the wheel 108 to be visible through this annulus. Thus only the indicia at that position will be legible, and that indicia will correspond to the codecombination established by the conductive segments of the tape and the conductors of the wheel, which codecombination will be picked up by the contacts 112, and carried out to counter 14. Rotation of the annulus causes translation of the tape behind it. The pins 122 and 124, however, anchor the ends of the tape, so that the tape cannot go beyond its minimum and maximum settings as the annulus is turned in either direction.
  • FIGS. 7 through 11 An alternative embodiment of the mechanical encoder is shown in FIGS. 7 through 11.
  • the encoder includes a plurality of assemblies 200, one for each decimal place.
  • Each assembly as shown in FIGS. 7A, 7B and 7C, includes a substrate 202 on which is fixed an electronic chip 204 containing a plurality of logic circuits and a plurality of leads 206, on which is disposed an array of seven conductors 208, which conductors are respectively connected by respective welded leads 210 to appropriate points in the logic circuits, the entire assembly being potted with the upper surfaces 212 of the conductors 208, and the leads 206, being exposed.
  • the chip 204 serves as a seven element to binary converter according to the logic shown in FIG. 8.
  • the gunner simply erases the previous penciling, and pencils on the new number.
  • the assembly 214 shown in FIG. 9, having pairs of conductors 216 may be utilized.
  • the number is generated by penciling across the appropriate pairs of conductors, as shown in FIG. 10.
  • the basic three digit display provides a setting mechanism having a resolution of 999 increments.
  • the scaler 72' contains at least two decades 220 and 222 and two AND gates 224 and 226.
  • a fuze for a projectile comprising: a pulse counter including an input terminal; an output terminal for providing an output signal;
  • first means coupled to said counter for presetting said counter to provide said output signal upon a first selected count
  • second means coupled to said input terminal of said counter for providing a series of pulses to be counted
  • third means coupled to said counter for forcing said counter to provide said output signal upon a second selected count
  • output function means coupled to said output terminal of said counter for providing an output function upon receipt of said counter output signal.
  • said first means includes an outer element, journaled for rotation, and having an inner surface
  • a dielectric tape disposed between and engaged by said inner surface of said outer element and said first plurality of conductors, and translatable by concurrent rotation of said outer and inner elements; said tape having a second plurality of spaced apart, electrically insulated, elongated conductors upon that surface of said tape which faces said inner element, so that, as a function of such translation different ones of said second plurality of conductors electrically interconnect ones of said first plurality of conductors;
  • a fuze according to claim 2 wherein: said tape has a fifth plurality of numerical indicia upon that surface of said tape which faces said outer element, said fourth plurality being topographically correlated to said second plurality of conductors, and said outer element provides limited rectilinear light transmission therethrough whereby only the indicia on said tape immediately adjacent the contact area between the inner and outer elements is visible through said outer element. 4.
  • said first means includes a dielectric substrate, a first plurality of conductors disposed in an array on said substrate, each of said conductors being insulated from the others of said conductors, logic circuitry intercoupling said conductors and said counter means, means for intercoupling selected ones of said conductors in different arrays, whereby to interconnect said respective logic circuitry in respective different arrays.
  • said fuze including a pulse counter including an input terminal, and an output terminal for providing an output signal; pulse providing means coupled to said input terminal of said counter;
  • first means coupled to said counter for presetting said counter to provide said output signal upon a first selected count
  • second means coupled to said input terminal of said counter for providing a series of pulses to be counted
  • third means coupled to said counter for forcing said counter to provide said output signal upon a second selected count
  • output function means coupled to said output terminal of said counter for providing an output function upon receipt of said counter output signal.
  • a system according to claim further including:
  • data link means coupled to said third means of said fuze for forcing said counter while said projectile is in flight.
  • said data link means includes enabling means for enabling said data link for a period of time which is shorter than the total time of flight of said projectile.
  • said data link means includes external means for providing unique numbers to internal means in said fuze for identifying said projectile, whereby each projectile in a series of projectiles may be uniquely identified.
  • said internal means for identifying said projectile includes enabling means
  • a first register coupled to said enabling means, for receiving and storing a unique number shortly after said projectile is launched
  • comparitor means coupled to an between said first and second registers and to said third means of said fuze for actuating said third means upon determining an identity between the number in said first register and the number in said second register.
  • an inner element journaled for rotation, and having an inner surface being a first plurality of parallel, spaced apart, electrically insulated, elongated conductors resiliently bearing against said inner surface of said outer element;
  • a weapon system disposed between and engaged by said inner surface of said outer element and said first plurality of conductors, and translatable by concurrent rotation of said outer and inner elements; said tape having a second plurality of spaced apart, electrically insulated, elongated conductors upon that surface of said tape which faces said inner element, so that, as a function of such translation, different ones of said second plurality of conductors electrically interconnect different ones of said first plurality of conductors; an additional element having a third plurality of spaced apart, electrical insulated, conductors, equal in number to said first plurality, each of said third plurality of conductors respectively engaged with a conductor of said first plurality of conductors; and a fourth plurality of conductors for electrically connecting said third plurality of conductors to said counter means.
  • said tape has a fifth plurality of numerical indicia upon that surface of said tape which faces said outer element, said fourth plurality being topographically correlated to said second plurality of conductors, and
  • said outer element provides limited rectilinear light transmission therethrough whereby only the indicia on said tape immediately adjacent the contact area between the inner and outer elements is visible through said outer element.
  • said first means includes a dielectric substrate, a first plurality of conductors disposed in an array on said substrate, each of said conductors being insulated from the others of said conductors, logic circuitry intercoupling said conductors and said counter means, means for intercoupling selected ones of said conductors in different arrays, whereby to interconnect said respective logic circuitry in respective different arrays.
  • a weapon system comprising: a projectile having a fuze; said fuze including a counting circuit having a first input terminal, a T output terminal for providing a signal at count 1, a T output terminal for providing a signal at count T2! a T output terminal for providing a signal at count a T input terminal for forcing said counting circuit to a predetermined count upon receipt of a signal thereat, and
  • a pulse generating circuit having an output terminal coupled to said first input terminal of said counting circuit
  • a firing circuit having an input terminal coupled to said final output terminal of said counting circuit
  • comparitor circuit having an output terminal coupled to said T input terminal of said counting circuit, and a first and a second input means;
  • a first register having an input terminal and an output means coupled to said first input means of said comparitor circuit
  • a second register having an input terminal and an output means coupled to said second input means of said comparitor circuit
  • an r.f. pulse transmitter having a transmitting antenna and transmitter control means; said control means for causing said transmitter to transmit a first pulse group to said fuze during the interval of count T, to T 15.
  • control means causes said transmitter to transmit said first pulse group again to said fuze during the time interval commencing at count T whereby said comparitor, upon determining an identity between said first and second registers, provides a signal at its output terminal which is coupled to said T input terminal of said counting circuit.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
US00292966A 1972-09-28 1972-09-28 Controlled range fuze Expired - Lifetime US3844217A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US00292966A US3844217A (en) 1972-09-28 1972-09-28 Controlled range fuze
IT29105/73A IT993255B (it) 1972-09-28 1973-09-19 Spoletta a raggio di azione controllato
GB4491973A GB1450406A (en) 1972-09-28 1973-09-25 Fuse for a projectile and weapon system incorporating the same
DE2348365A DE2348365C2 (de) 1972-09-28 1973-09-26 Zünder für ein Projektil
FR7334625A FR2201452B1 (de) 1972-09-28 1973-09-27
SE7313251A SE409242B (sv) 1972-09-28 1973-09-28 Tidstendror med efter projektilens avskjutning endringsbar tidbar
JP10860073A JPS5712959B2 (de) 1972-09-28 1973-09-28
US05/420,358 US3955069A (en) 1972-09-28 1973-11-29 Presettable counter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00292966A US3844217A (en) 1972-09-28 1972-09-28 Controlled range fuze

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US3844217A true US3844217A (en) 1974-10-29

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US00292966A Expired - Lifetime US3844217A (en) 1972-09-28 1972-09-28 Controlled range fuze

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US (1) US3844217A (de)
JP (1) JPS5712959B2 (de)
DE (1) DE2348365C2 (de)
FR (1) FR2201452B1 (de)
GB (1) GB1450406A (de)
IT (1) IT993255B (de)
SE (1) SE409242B (de)

Cited By (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2556250A1 (de) * 1974-12-17 1976-07-01 Gen Electric Elektrischer ruecksetzgenerator
DE2620642A1 (de) * 1975-05-14 1976-11-25 Gen Electric Anordnung zur steuerung eines projektilzuenders waehrend des fluges und zugehoerige unteranordnungen
US4026215A (en) * 1975-05-14 1977-05-31 General Electric Company Controlled range, multi-mode fuze
US4030420A (en) * 1974-11-01 1977-06-21 Ab Bofors Device for ground-controlled activation of proximity fuzes
US4044680A (en) * 1975-05-14 1977-08-30 General Electric Company Remotely controlled electronic fuze
US4083308A (en) * 1973-05-19 1978-04-11 Ferranti Limited Projectile fuzes
US4085680A (en) * 1977-02-17 1978-04-25 General Electric Company Fuze encoder
US4095529A (en) * 1977-02-17 1978-06-20 General Electric Company Setting ring stop
US4100856A (en) * 1977-02-17 1978-07-18 General Electric Company Fuze encoder
US4116133A (en) * 1975-11-25 1978-09-26 Mefina S.A. Electronic firing device for missiles
US4147109A (en) * 1977-02-17 1979-04-03 General Electric Company Controlled range fuze
US4212246A (en) * 1978-05-26 1980-07-15 The United States Of America As Represented By The Secretary Of The Navy Fuze electronic circuitry
US4267776A (en) * 1979-06-29 1981-05-19 Motorola, Inc. Muzzle velocity compensating apparatus and method for a remote set fuze
DE3042974A1 (de) * 1979-11-27 1981-09-03 General Electric Co., Schenectady, N.Y. Elektrischer zuender mit verschiedenen arbeitsweisen
US4567829A (en) * 1984-07-30 1986-02-04 General Electric Company Shaped charge projectile system
EP0193766A1 (de) * 1985-03-05 1986-09-10 Obisco Trading and Consulting SA Handfeuerwaffe sowie Schrotmunition hierfür
US4651647A (en) * 1985-04-01 1987-03-24 Werkzeugmaschinenfabrik Oerlikon-Buehrle Ag Adjustable range proximity fuze
DE3624348A1 (de) * 1986-07-18 1990-03-29 Asea Brown Boveri Verfahren und schaltung zur aktivierung einer station
US5322016A (en) * 1991-12-18 1994-06-21 Oerlikon-Contraves Ag Method for increasing the probability of success of air defense by means of a remotely fragmentable projectile
US5343795A (en) * 1991-11-07 1994-09-06 General Electric Co. Settable electronic fuzing system for cannon ammunition
US5415100A (en) * 1993-12-22 1995-05-16 Base Ten Systems, Inc. Apparatus and method for setting missile fuze delay
DE4412688A1 (de) * 1994-04-13 1995-10-19 Diehl Gmbh & Co Fernsteuereinrichtung zum Zünden des Gefechtskopfes eines Projektils
WO1997014931A1 (en) * 1995-10-17 1997-04-24 Foster-Miller, Inc. Ballistically deployed restraining net
US6142080A (en) * 1998-01-14 2000-11-07 General Dynamics Armament Systems, Inc. Spin-decay self-destruct fuze
US6145439A (en) * 1998-01-14 2000-11-14 General Dynamics Armament Systems, Inc. RC time delay self-destruct fuze
US6484115B1 (en) * 1998-10-08 2002-11-19 Oerlikon Contraves Pyrotec Ag Method of correcting the pre-programmed initiation of an event in a spin-stabilized projectile, device for executing the method and use of the device
US20030110972A1 (en) * 2001-12-19 2003-06-19 Porter Frank B. Time limited weapon system
US20080105113A1 (en) * 2006-10-04 2008-05-08 Arthur Schneider Supercapacitor power supply
KR20220163953A (ko) * 2020-02-27 2022-12-12 베누스 바이 마리아 타쉬, 인크. 피어싱 기술, 이를 위한 귀걸이, 및 그 제조 및 사용 방법

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5148600A (ja) * 1974-10-23 1976-04-26 Boeicho Gijutsu Kenkyu Honbuch Hodanyodenkishikijigenshinkanhoshiki
DE2940227C2 (de) * 1979-10-04 1983-08-18 Diehl GmbH & Co, 8500 Nürnberg Elektrischer Geschoßzünder
JPS59182246U (ja) * 1983-05-20 1984-12-05 双葉金属工業株式会社 机などの引出し支持装置
JPS6031845U (ja) * 1983-08-10 1985-03-04 東邦スチ−ル工業株式会社 棚体案内装置
FR2608267B1 (fr) * 1986-12-11 1992-12-31 Seat Bourges Sa Munition programmable par voie optique et systeme d'arme en comportant application

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2769975A (en) * 1945-10-29 1956-11-06 Rines Robert Harvey Electromagnetic object-tracking-anddestroying method and system
US3113305A (en) * 1951-05-04 1963-12-03 Edmund P Trounson Semi-active proximity fuze
US3500746A (en) * 1968-04-17 1970-03-17 Lear Siegler Inc Weapon system with an electronic time fuze
US3670652A (en) * 1970-05-11 1972-06-20 Gen Electric Controlled range proximity fuze
US3714898A (en) * 1969-07-22 1973-02-06 Gen Electric Fuze actuating system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3608494A (en) * 1969-03-05 1971-09-28 Gen Electric Time delay fuse
US3599016A (en) * 1969-07-22 1971-08-10 Gen Electric Automatic reset circuit

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2769975A (en) * 1945-10-29 1956-11-06 Rines Robert Harvey Electromagnetic object-tracking-anddestroying method and system
US3113305A (en) * 1951-05-04 1963-12-03 Edmund P Trounson Semi-active proximity fuze
US3500746A (en) * 1968-04-17 1970-03-17 Lear Siegler Inc Weapon system with an electronic time fuze
US3714898A (en) * 1969-07-22 1973-02-06 Gen Electric Fuze actuating system
US3670652A (en) * 1970-05-11 1972-06-20 Gen Electric Controlled range proximity fuze

Cited By (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4083308A (en) * 1973-05-19 1978-04-11 Ferranti Limited Projectile fuzes
US4030420A (en) * 1974-11-01 1977-06-21 Ab Bofors Device for ground-controlled activation of proximity fuzes
DE2556250A1 (de) * 1974-12-17 1976-07-01 Gen Electric Elektrischer ruecksetzgenerator
DE2620642A1 (de) * 1975-05-14 1976-11-25 Gen Electric Anordnung zur steuerung eines projektilzuenders waehrend des fluges und zugehoerige unteranordnungen
US4026215A (en) * 1975-05-14 1977-05-31 General Electric Company Controlled range, multi-mode fuze
US4044680A (en) * 1975-05-14 1977-08-30 General Electric Company Remotely controlled electronic fuze
US4116133A (en) * 1975-11-25 1978-09-26 Mefina S.A. Electronic firing device for missiles
US4147109A (en) * 1977-02-17 1979-04-03 General Electric Company Controlled range fuze
US4100856A (en) * 1977-02-17 1978-07-18 General Electric Company Fuze encoder
US4095529A (en) * 1977-02-17 1978-06-20 General Electric Company Setting ring stop
US4085680A (en) * 1977-02-17 1978-04-25 General Electric Company Fuze encoder
US4212246A (en) * 1978-05-26 1980-07-15 The United States Of America As Represented By The Secretary Of The Navy Fuze electronic circuitry
US4267776A (en) * 1979-06-29 1981-05-19 Motorola, Inc. Muzzle velocity compensating apparatus and method for a remote set fuze
DE3042974A1 (de) * 1979-11-27 1981-09-03 General Electric Co., Schenectady, N.Y. Elektrischer zuender mit verschiedenen arbeitsweisen
US4291627A (en) * 1979-11-27 1981-09-29 General Electric Company Electrical fuze with a plurality of modes of operation
US4567829A (en) * 1984-07-30 1986-02-04 General Electric Company Shaped charge projectile system
WO1986000979A1 (en) * 1984-07-30 1986-02-13 General Electric Company Shaped charge projectile system
US4864935A (en) * 1985-03-05 1989-09-12 Obisco Trading & Consulting S.A. Small-arm ammunition in shot form
EP0193766A1 (de) * 1985-03-05 1986-09-10 Obisco Trading and Consulting SA Handfeuerwaffe sowie Schrotmunition hierfür
US4852457A (en) * 1985-03-05 1989-08-01 Obisco Trading & Consulting S.A. Small-arm and ammunition in shot form for the same
US4651647A (en) * 1985-04-01 1987-03-24 Werkzeugmaschinenfabrik Oerlikon-Buehrle Ag Adjustable range proximity fuze
DE3624348A1 (de) * 1986-07-18 1990-03-29 Asea Brown Boveri Verfahren und schaltung zur aktivierung einer station
GB2231128A (en) * 1986-07-18 1990-11-07 Bbc Brown Boveri & Cie Activating a missile
US5343795A (en) * 1991-11-07 1994-09-06 General Electric Co. Settable electronic fuzing system for cannon ammunition
US5322016A (en) * 1991-12-18 1994-06-21 Oerlikon-Contraves Ag Method for increasing the probability of success of air defense by means of a remotely fragmentable projectile
US5415100A (en) * 1993-12-22 1995-05-16 Base Ten Systems, Inc. Apparatus and method for setting missile fuze delay
DE4412688C2 (de) * 1994-04-13 2000-10-05 Diehl Stiftung & Co Fernsteuereinrichtung für ein Leitstrahl-Projektil
DE4412688A1 (de) * 1994-04-13 1995-10-19 Diehl Gmbh & Co Fernsteuereinrichtung zum Zünden des Gefechtskopfes eines Projektils
WO1997014931A1 (en) * 1995-10-17 1997-04-24 Foster-Miller, Inc. Ballistically deployed restraining net
US5750918A (en) * 1995-10-17 1998-05-12 Foster-Miller, Inc. Ballistically deployed restraining net
US6142080A (en) * 1998-01-14 2000-11-07 General Dynamics Armament Systems, Inc. Spin-decay self-destruct fuze
US6145439A (en) * 1998-01-14 2000-11-14 General Dynamics Armament Systems, Inc. RC time delay self-destruct fuze
US6484115B1 (en) * 1998-10-08 2002-11-19 Oerlikon Contraves Pyrotec Ag Method of correcting the pre-programmed initiation of an event in a spin-stabilized projectile, device for executing the method and use of the device
US20030110972A1 (en) * 2001-12-19 2003-06-19 Porter Frank B. Time limited weapon system
US20080105113A1 (en) * 2006-10-04 2008-05-08 Arthur Schneider Supercapacitor power supply
US7946209B2 (en) * 2006-10-04 2011-05-24 Raytheon Company Launcher for a projectile having a supercapacitor power supply
KR20220163953A (ko) * 2020-02-27 2022-12-12 베누스 바이 마리아 타쉬, 인크. 피어싱 기술, 이를 위한 귀걸이, 및 그 제조 및 사용 방법

Also Published As

Publication number Publication date
IT993255B (it) 1975-09-30
DE2348365C2 (de) 1983-08-11
JPS5712959B2 (de) 1982-03-13
DE2348365A1 (de) 1974-04-04
GB1450406A (en) 1976-09-22
JPS4994200A (de) 1974-09-06
FR2201452A1 (de) 1974-04-26
FR2201452B1 (de) 1976-06-18
SE409242B (sv) 1979-08-06

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