EP1726911A1 - Méthode et dispositif pour programmer et corriger le moment de détonation d'un projectile - Google Patents

Méthode et dispositif pour programmer et corriger le moment de détonation d'un projectile Download PDF

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Publication number
EP1726911A1
EP1726911A1 EP06002014A EP06002014A EP1726911A1 EP 1726911 A1 EP1726911 A1 EP 1726911A1 EP 06002014 A EP06002014 A EP 06002014A EP 06002014 A EP06002014 A EP 06002014A EP 1726911 A1 EP1726911 A1 EP 1726911A1
Authority
EP
European Patent Office
Prior art keywords
projectile
weapon
calculation
correcting
correction
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.)
Granted
Application number
EP06002014A
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German (de)
English (en)
Other versions
EP1726911B1 (fr
Inventor
Jens Dr. Seidensticker
Dietrich Stauffacher
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Air Defence AG
Original Assignee
Oerlikon Contraves AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Oerlikon Contraves AG filed Critical Oerlikon Contraves AG
Publication of EP1726911A1 publication Critical patent/EP1726911A1/fr
Application granted granted Critical
Publication of EP1726911B1 publication Critical patent/EP1726911B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C17/00—Fuze-setting apparatus
    • F42C17/04—Fuze-setting apparatus for electric fuzes
    • 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
    • F42C11/065—Programmable electronic delay initiators in projectiles

Definitions

  • the invention relates to a method and a device for programming a storable projectile or for correcting an ignition timing of a missile fired from a weapon.
  • a method and a device for transmitting information to programmable projectiles are the EP 0 992 762 B1 removable.
  • a method and apparatus for programming firefighters from projectiles are also used in the EP 0 769 673 B1 treated.
  • a predetermined muzzle velocity of the projectile and a predetermined distance to a target object are used.
  • a method for correcting the ignition timing and a circuit arrangement for carrying out the method is disclosed.
  • the device measures the actual bullet velocity over time only during a certain period of time. Thereafter, the further course of the speed is extrapolated. When the flight path determined in this way has reached a target value, the ignition is triggered.
  • a device for measuring the projectile velocity at the mouth of a barrel of a gun of high cadence comprises two spaced apart from each other on a support tube, responsive to change in a magnetic flux sensors that are in communication with a transmitter. Each sensor has a coil pair of two coils and a closed magnetic circuit. The measured projectile velocity or the ignition setting time that is updated with it is then generally given to the bullet as information before the projectile leaves the area of the mouth.
  • the aforementioned device is characterized by high accuracy, but is subject to mechanical and thermodynamic loads, since the measuring and programming unit u. a. are exposed to the muzzle gases.
  • the invention takes on the task to show a device or an improved programming system, which is no longer exposed to mechanical and thermodynamic wear.
  • claim 1 claim a method and claim 5 a device.
  • the invention is based on the idea of maintaining the advantages of measuring a muzzle velocity and a current compensated tempation, incorporating a microwave transmitter, preferably in the GHz range, into the system, which stores the current, for example, a Feuerleitrechner determined temping to an ammunition or a projectile sends.
  • a direct measurement of the current muzzle velocity can be dispensed with, since the real muzzle velocity is determined by information of the current airspeed of the projectile, that is, calculated back from this.
  • the ignition time of the projectile is then corrected with the aid of a standard muzzle velocity preset ignition time and used as the actual ignition timing.
  • the measurement of the airspeed takes place, for example, by means of Doppler shift of the transmission frequencies, preferably on the storey side.
  • the transmission frequency is fixed and measured the deviation. Since the time is known, which has covered the projectile each time, the current airspeed and also determines the real muzzle velocity of the projectile which possessed the projectile at the time of launch through the muzzle area. From these data, the current ignition timing is then determined and made available to the projectile.
  • RFID Radio Frequency Identification
  • the chip u. a. is programmable by the fire control unit with the current standard temping as well as with a correction value or a value determined only during the flight.
  • the timer on the ammunition (or in the ammunition) can then be counted down to zero over the (remaining) flight distance and then accomplish the desired disassembly before a target.
  • the calculated muzzle velocity can also be returned if this calculation is made on the projectile to account for any deviations in the fire pipe.
  • the microwave transmitter used can be fixed locally to the gun, where it is exposed neither to vent gases nor to mechanical loads.
  • the transmitter / receiver is electrically powered by the gun electrical system and supplied with data from the fire control. Any data returned from ammunition may be forwarded to and considered by the Fire Department.
  • the single FIGURE shows a programming system 1 or a generalized device for a storable projectile 2 or a malleable ammunition (etc).
  • a programmable chip 3 for example an RFID chip, which in combination preferably contains the receiver and transmitter circuit together with the memory.
  • a located in the floor 2 timer 4 is powered by this chip 3 with the necessary time information on site.
  • the chip 3 is connected to a calculation and / or correction unit 5, if this is provided in the projectile 2, which is then also connected to the timer 4.
  • Functionally downstream of the timer 4 is an igniter 6.
  • the energy supply to the assemblies of the projectile 2 can be supplied in a first way by means of the microwave radiation X or preferably solved conventionally, for example by an activatable, not shown battery.
  • the programming system 1 preferably attached to the gun barrel 11, a transmitter / receiver 12 for data transmission to the projectile 2 on.
  • This transmitter / receiver 12 is electrically connected to a fire control system or fire control computer 13 present in a weapons system.
  • the current disassembly time calculated according to the standard speed of the projectile 2, is transmitted to the projectile 2. With the Doppler method, the deviation from the standard speed in the projectile 2 is determined. Depending on the deviation, the current disassembly time is calculated in projectile 2 or on the protected side.
  • a correction of the Zündstellzeit for the igniter 6 can be made on the storey side, the timer 4 is acted upon with this information.
  • the correction made or the calculated, recalculated muzzle velocity can be transmitted via microwave radiation X to the transmitter / receiver 12 on the gun 10 and made available to a fire control system (not shown).
  • the target value of the detonator time (flying time) based on the actual muzzle velocity of the projectile 2 when fired via the microwave radiation X to the Projectile 2 transferred.
  • This Zündstellzeit is corrected and used as a new ignition timing in the second floor.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Heat Treatment Of Articles (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Fuses (AREA)
EP06002014A 2005-05-23 2006-02-01 Méthode et dispositif pour programmer et corriger le moment de détonation d'un projectile Not-in-force EP1726911B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102005024179A DE102005024179A1 (de) 2005-05-23 2005-05-23 Verfahren und Vorrichtung zur Tempierung und/oder Korrektur des Zündzeitpunktes eines Geschosses

Publications (2)

Publication Number Publication Date
EP1726911A1 true EP1726911A1 (fr) 2006-11-29
EP1726911B1 EP1726911B1 (fr) 2011-04-20

Family

ID=35901540

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06002014A Not-in-force EP1726911B1 (fr) 2005-05-23 2006-02-01 Méthode et dispositif pour programmer et corriger le moment de détonation d'un projectile

Country Status (9)

Country Link
US (1) US20070074625A1 (fr)
EP (1) EP1726911B1 (fr)
JP (1) JP5005954B2 (fr)
AT (1) ATE506594T1 (fr)
CA (1) CA2545300A1 (fr)
DE (2) DE102005024179A1 (fr)
DK (1) DK1726911T3 (fr)
ES (1) ES2365039T3 (fr)
ZA (1) ZA200604101B (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008098562A1 (fr) * 2007-02-12 2008-08-21 Krauss-Maffei Wegmann Gmbh & Co. Kg Procédé et dispositif de protection contre des éléments de munition d'attaque volants
EP2261591A1 (fr) * 2009-06-08 2010-12-15 Rheinmetall Air Defence AG Procédé de correction de la trajectoire d'une munition dirigée en phase finale
WO2011085758A1 (fr) 2010-01-15 2011-07-21 Rheinmetall Air Defence Ag Procédé pour corriger la trajectoire d'un projectile guidé en particulier en phase finale et projectile pour la mise en œuvre du procédé
DE102010006528A1 (de) 2010-02-01 2011-08-04 Rheinmetall Air Defence Ag Verfahren und Vorrichtung zur Programmierung eines Projektils
WO2011092023A1 (fr) 2010-02-01 2011-08-04 Rheinmetall Air Defence Ag Munition programmable
DE102009011447B9 (de) * 2009-03-03 2012-08-16 Diehl Bgt Defence Gmbh & Co. Kg Verfahren zum Zünden eines Gefechtskopfs einer Granate und Fahrzeug

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006058375A1 (de) 2006-12-08 2008-06-12 Oerlikon Contraves Ag Verfahren zur Messung der Mündungsgeschwindigkeit eines Projektils oder dergleichen
DE102007007404A1 (de) 2007-02-12 2008-08-14 Krauss-Maffei Wegmann Gmbh & Co. Kg Verfahren und Vorrichtung zur Fernauslösung eines Geschosses
DE102007044732A1 (de) 2007-09-18 2009-04-02 Oerlikon Contraves Ag Verfahren und Vorrichtung zur Erhöhung der Treffgenauigkeit einer insbesondere zeitgesteuerten Munitionszerlegung
SG155076A1 (en) * 2008-02-18 2009-09-30 Advanced Material Engineering In-flight programming of trigger time of a projectile
DE102008024574A1 (de) 2008-05-21 2010-06-17 Rheinmetall Air Defence Ag Vorrichtung und Verfahren zur Messung der Mündungsgeschwindigkeit eines Projektils oder dergleichen
DE102008052074A1 (de) * 2008-10-17 2010-04-22 Rheinmetall Landsysteme Gmbh Waffensystem mit einem Trägerfahrzeug und einem fahrzeuggebundenen Mörser
DE102008056108A1 (de) 2008-11-06 2010-05-12 Rheinmetall Waffe Munition Gmbh Waffe mit Rücklauf und einer diesen dämpfenden Bremseinrichtung
DE102008056112A1 (de) 2008-11-06 2010-05-12 Rheinmetall Waffe Munition Gmbh Mörser
US8935958B2 (en) * 2010-11-22 2015-01-20 Drs Technologies Canada, Ltd. Muzzle velocity sensor
DE102011018248B3 (de) * 2011-04-19 2012-03-29 Rheinmetall Air Defence Ag Vorrichtung und Verfahren zur Programmierung eines Geschosses
JP5979022B2 (ja) * 2012-01-27 2016-08-24 ダイキン工業株式会社 弾薬作動システム
CN102620603A (zh) * 2012-03-31 2012-08-01 中国人民解放军济南军区72465部队 防空高炮炮口初速测量线圈及时间装定线圈安装结构
DE102012022894A1 (de) * 2012-11-23 2014-05-28 Gabriele Lisa Trinkel Verfahren und System zur Personalisierung und Energieversorgung von Geschosse und Geschossabgabesysteme
DE102013007229A1 (de) 2013-04-26 2014-10-30 Rheinmetall Waffe Munition Gmbh Verfahren zum Betrieb eines Waffensystems
GB2522246B (en) * 2014-01-20 2016-05-11 Bae Systems Plc Fuze setting apparatus
WO2017141009A1 (fr) * 2016-02-16 2017-08-24 Bae Systems Plc Système d'amorce de projectile
EP3208569A1 (fr) * 2016-02-16 2017-08-23 BAE Systems PLC Activation d'un dispositif d'allumage
EP3417234B1 (fr) * 2016-02-16 2021-04-07 BAE Systems PLC Activation d'un dispositif d'allumage
KR101800843B1 (ko) * 2016-05-12 2017-12-21 주식회사 한국계측기기연구센터 포구속도 측정용 도플러 레이더 장비 교정장치 및 교정방법
KR102124083B1 (ko) * 2018-12-21 2020-06-17 주식회사 한화 터빈 발전기를 이용하는 전자식 신관의 안전 시간을 제어하는 장치 및 그 방법
CN118066954B (zh) * 2024-04-25 2024-07-09 江西红声技术有限公司 电子引信测试方法、系统、可读存储介质及计算机设备

Citations (6)

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US4267776A (en) 1979-06-29 1981-05-19 Motorola, Inc. Muzzle velocity compensating apparatus and method for a remote set fuze
DE3309147A1 (de) * 1983-03-15 1984-09-20 Rainer Dipl.-Phys. 6901 Gaiberg Berthold Verfahren und anordnung zur korrektur eines zuendzeitpunktes
DE3835656A1 (de) * 1988-10-20 1990-04-26 Asea Brown Boveri Verfahren zur korrektur des zuendzeitpunktes eines aus einer rohrwaffe abgefeuerten geschosses und schaltungsanordnung zur durchfuehrung des verfahrens
DE3835655A1 (de) * 1988-10-20 1990-04-26 Asea Brown Boveri Verfahren zur korrektur des zuendpunkts eines geschosses
CH691143A5 (de) 1995-03-17 2001-04-30 Contraves Ag Vorrichtung zur Messung der Geschossgeschwindigkeit an der Mündung eines Waffenrohres eines Geschützes hoher Kadenz.
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

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US3918061A (en) * 1973-09-25 1975-11-04 Terma Elektronisk Industri As Velocity measuring doppler radar
DE3307785A1 (de) * 1983-03-04 1984-09-06 Deutsch-Französisches Forschungsinstitut Saint-Louis, Saint-Louis Verfahren und vorrichtung zur einstellung eines geschoss-zeitzuenders
DE3830518A1 (de) * 1988-09-08 1990-03-22 Rheinmetall Gmbh Vorrichtung zur einstellung eines geschosszeitzuenders
DE59100529D1 (de) * 1990-07-19 1993-12-02 Contraves Ag Empfangsspule für einen programmierbaren Geschosszünder.
US5497704A (en) * 1993-12-30 1996-03-12 Alliant Techsystems Inc. Multifunctional magnetic fuze
EP0769673B1 (fr) * 1995-09-28 2002-03-20 Oerlikon Contraves Pyrotec AG Procédé et dispositif pour la programmation des fusées à temps de projectiles
FR2761767B1 (fr) * 1997-04-03 1999-05-14 Giat Ind Sa Procede de programmation en vol d'un instant de declenchement d'un element de projectile, conduite de tir et fusee mettant en oeuvre un tel procede
EP0918209B1 (fr) * 1997-11-19 2002-12-18 Oerlikon Contraves Ag Projectile avec fusée à temps programmable
EP0992762B1 (fr) * 1998-10-08 2002-03-06 Oerlikon Contraves Ag Procédé et dispositif pour transmettre des informations à un projectile programmable
DK0992758T3 (da) * 1998-10-08 2007-06-18 Contraves Ag Fremgangsmåde og anordning til korrektion af sönderdelingstiden eller sönderdelingsomdrejningstallet for et spinstabiliseret projektil
DE10236157A1 (de) * 2002-08-07 2004-02-26 Junghans Feinwerktechnik Gmbh & Co. Kg Programmierbarer Artilleriezünder
ATE391893T1 (de) * 2003-02-26 2008-04-15 Rwm Schweiz Ag Verfahren zur programmierung der zerlegung von projektilen und rohrwaffen mit programmiersystem
US20050126379A1 (en) * 2003-12-10 2005-06-16 Pikus Eugene C. RF data communications link for setting electronic fuzes
US7352319B2 (en) * 2005-06-10 2008-04-01 Honeywell International Inc. Methods and systems utilizing Doppler prediction to enable fusing

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4267776A (en) 1979-06-29 1981-05-19 Motorola, Inc. Muzzle velocity compensating apparatus and method for a remote set fuze
DE3309147A1 (de) * 1983-03-15 1984-09-20 Rainer Dipl.-Phys. 6901 Gaiberg Berthold Verfahren und anordnung zur korrektur eines zuendzeitpunktes
DE3835656A1 (de) * 1988-10-20 1990-04-26 Asea Brown Boveri Verfahren zur korrektur des zuendzeitpunktes eines aus einer rohrwaffe abgefeuerten geschosses und schaltungsanordnung zur durchfuehrung des verfahrens
DE3835655A1 (de) * 1988-10-20 1990-04-26 Asea Brown Boveri Verfahren zur korrektur des zuendpunkts eines geschosses
CH691143A5 (de) 1995-03-17 2001-04-30 Contraves Ag Vorrichtung zur Messung der Geschossgeschwindigkeit an der Mündung eines Waffenrohres eines Geschützes hoher Kadenz.
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

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008098562A1 (fr) * 2007-02-12 2008-08-21 Krauss-Maffei Wegmann Gmbh & Co. Kg Procédé et dispositif de protection contre des éléments de munition d'attaque volants
DE102009011447B9 (de) * 2009-03-03 2012-08-16 Diehl Bgt Defence Gmbh & Co. Kg Verfahren zum Zünden eines Gefechtskopfs einer Granate und Fahrzeug
EP2261591A1 (fr) * 2009-06-08 2010-12-15 Rheinmetall Air Defence AG Procédé de correction de la trajectoire d'une munition dirigée en phase finale
DE102009024508A1 (de) 2009-06-08 2011-07-28 Rheinmetall Air Defence Ag Verfahren zur Korrektur der Flugbahn einer endphasengelenkten Munition
US8288698B2 (en) 2009-06-08 2012-10-16 Rheinmetall Air Defence Ag Method for correcting the trajectory of terminally guided ammunition
WO2011085758A1 (fr) 2010-01-15 2011-07-21 Rheinmetall Air Defence Ag Procédé pour corriger la trajectoire d'un projectile guidé en particulier en phase finale et projectile pour la mise en œuvre du procédé
DE102010004820A1 (de) 2010-01-15 2011-07-21 Rheinmetall Air Defence Ag Verfahren zur Flugbahnkorrektur eines insbesondere endphasengelenkten Geschosses sowie Geschoss zur Durchführung des Verfahrens
US8558151B2 (en) 2010-01-15 2013-10-15 Rheinmetall Air Defence Ag Method for correcting the trajectory of a projectile, in particular of a terminal phase-guided projectile, and projectile for carrying out the method
WO2011092022A1 (fr) 2010-02-01 2011-08-04 Rheinmetall Air Defence Ag Procédé et dispositif pour programmer un projectile
DE102010006530A1 (de) 2010-02-01 2011-08-04 Rheinmetall Air Defence Ag Programmierbare Munition
WO2011092023A1 (fr) 2010-02-01 2011-08-04 Rheinmetall Air Defence Ag Munition programmable
DE102010006528A1 (de) 2010-02-01 2011-08-04 Rheinmetall Air Defence Ag Verfahren und Vorrichtung zur Programmierung eines Projektils
DE102010006528B4 (de) * 2010-02-01 2013-12-12 Rheinmetall Air Defence Ag Verfahren und Vorrichtung zur Programmierung eines Projektils
DE102010006530B4 (de) * 2010-02-01 2013-12-19 Rheinmetall Air Defence Ag Programmierbare Munition
US8746119B2 (en) 2010-02-01 2014-06-10 Rheinmetall Air Defence Ag Method and device for programming a projectile
US8984999B2 (en) 2010-02-01 2015-03-24 Rheinmetall Air Defence Ag Programmable ammunition

Also Published As

Publication number Publication date
ZA200604101B (en) 2007-02-28
JP5005954B2 (ja) 2012-08-22
ATE506594T1 (de) 2011-05-15
ES2365039T3 (es) 2011-09-21
DE502006009327D1 (de) 2011-06-01
DK1726911T3 (da) 2011-08-01
EP1726911B1 (fr) 2011-04-20
CA2545300A1 (fr) 2006-11-23
US20070074625A1 (en) 2007-04-05
JP2006329616A (ja) 2006-12-07
DE102005024179A1 (de) 2006-11-30

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