EP0802390A1 - Procédé de tempage de désintégration en particulier pour un projectile programmable - Google Patents
Procédé de tempage de désintégration en particulier pour un projectile programmable Download PDFInfo
- Publication number
- EP0802390A1 EP0802390A1 EP96118039A EP96118039A EP0802390A1 EP 0802390 A1 EP0802390 A1 EP 0802390A1 EP 96118039 A EP96118039 A EP 96118039A EP 96118039 A EP96118039 A EP 96118039A EP 0802390 A1 EP0802390 A1 EP 0802390A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- equation
- speed
- target
- disassembly
- 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
Links
Images
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
Definitions
- the invention relates to a method for calculating the disassembly time, in particular of a programmable projectile, the calculation being based on at least one target distance to a target object determined from sensor data, a projectile speed measured at the muzzle of a gun barrel and a predetermined optimal disassembly distance between a meeting point and a disassembly point of the projectile is.
- a device which has a measuring device for the projectile velocity arranged at the mouth of a gun barrel.
- the measuring device consists of two ring coils arranged at a certain distance from one another.
- a pulse is generated in short succession in each ring coil due to the change in magnetic flux that occurs.
- the pulses are fed to an electronic evaluation system, in which the temporal distance of the impulses and the distance between the ring coils the bullet speed is calculated.
- a transmitting coil is arranged behind the measuring device for the speed, which co-operates with a receiving coil provided in the projectile.
- the receiving coil is connected to a counter via a high-pass filter, which is connected on the output side to a timer.
- a disassembly time is formed from the calculated bullet speed and a hit distance to a target object determined from sensor data, which is inductively transmitted to the bullet immediately after the measuring device has flown through. With this disassembly time, the time fuse is set so that the projectile can be disassembled in the area of the target object.
- an attacking target can be destroyed by multiple hits, as is known, for example, from a publication OC 2052 d 94 from the company Oerlikon-Contraves, Zurich, if, after the sub-projectiles have been ejected, Time of disassembly the expected area of the target is occupied by a cloud formed by the subprojectiles.
- the part carrying the subprojectiles is separated and torn open at predetermined breaking points.
- the ejected sub-projectiles describe a swirl-stabilized trajectory caused by the rotation of the projectile and lie evenly distributed on approximately semicircular curves of circular areas of a cone, so that a good chance of hitting or firing can be achieved.
- the invention has for its object to propose a method and a device according to the preamble, by means of which an optimal hit or shot probability can be achieved while avoiding the disadvantages mentioned above.
- a given optimal disassembly distance between a disassembly point of the projectile and a meeting point of the target is kept constant by correcting the disassembly time of the projectile.
- the correction is made by adding a correction factor multiplied by a speed difference to the disassembly time.
- the speed difference is formed from the difference between the current measured floor speed and a lead speed of the projectile, the lead speed being calculated from the mean of a number of previous successive floor speeds.
- the advantages achieved with the invention can be seen in the fact that a given disassembly distance is independent of the current measured bullet speed, so that a permanent optimal hit or shot probability can be achieved.
- the proposed correction factor for the correction of the disassembly time is based only on the shooting elements of the point of impact for the control of the weapon, namely the gun angles ⁇ , ⁇ , the time Tf and the lead speed V0v of the projectile. This enables simple integration into existing weapon control systems, which requires minimal effort.
- 1 denotes a fire control and 2 a gun.
- the fire control 1 consists of a search sensor 3 for the detection of a target 4 , a follow sensor 5 connected to the search sensor 3 for target detection, 3-D target tracking and 3-D target measurement, and a fire control computer 6 .
- the fire control computer 6 has at least one main filter 7 and a lead computing unit 9 .
- the main filter 7 is connected on the input side to the follow sensor 5 and on the output side to the lead computing unit 9 , the main filter 7 receiving the 3-D target data received from the follow sensor 5 in the form of estimated target data Z such as position, speed, acceleration, etc.
- Computing unit 9 forwards. Meteorological data can be supplied to the lead computing unit 9 via a further input Me. The meaning of the designations on the individual connections or connections is explained in more detail below on the basis of the functional description.
- a computer of the gun 2 has an evaluation circuit 10 , an update computing unit 11 and a correction computing unit 12 .
- the evaluation circuit 10 is connected on the input side to a measuring device 14 for the projectile velocity, which is arranged at the mouth of a gun barrel 13 and is described in more detail below with reference to FIG . 2 , and is connected on the output side to the lead computing unit 9 and the update computing unit 11 .
- the update computing unit 11 is connected on the input side to the reserve and to the correction computing unit 9, 12 and is connected on the output side to a programmer integrated in the measuring device 14 .
- the correction computing unit 12 is connected on the input side to the lead computing unit 9 and on the output side to the updating computing unit 11 .
- a gun servo 15 and a triggering device 16 responding to a fire command are also connected to the lead computing unit 9 .
- the connections between the fire control 1 and the gun 2 are combined to form a data transmission, which is designated by 17 .
- the meaning of the designations on the individual connections between the computing units 10, 11, 12 and between the fire control system 1 and the gun 2 is explained in more detail below on the basis of the functional description.
- 18 and 18 ' denote a floor which is shown during a programming phase ( 18 ) and at the time of disassembly ( 18' ).
- the projectile 18 is a programmable projectile with primary and secondary ballistics, which is equipped with an ejection charge and a time fuse and is filled with sub-projectiles 19 .
- a support tube 20 attached to the muzzle of the gun barrel 13 consists of three parts 21, 22, 23 . Between the first part 21 and the second or third part 22, 23 , ring coils 24, 25 are arranged for measuring the projectile speed. On the third part 23 — also called the programming part — a transmission coil 27 held in a coil body 26 is fastened. The type of attachment of the support tube 20 and the three parts 21, 22, 23 to each other is not shown and described. Lines 28, 29 are provided for supplying the ring coils. Soft iron rods 30 are arranged on the circumference of the support tube 20 for the purpose of shielding against magnetic fields which interfere with the measurement.
- the projectile 18 has a receiving coil 31 which is connected to a timer 34 via a filter 32 and a counter 33 .
- a pulse is generated in short succession in each ring coil.
- These pulses are fed to the evaluation circuit 10 ( FIG. 1 ), in which the projectile speed is calculated from the time interval of the pulses and a distance a between the ring coils 24, 25 .
- a disassembly time is calculated, as described in more detail below, which is transmitted inductively to the receiving coil 31 in digital form when the bullet 18 passes through the transmitting coil 27 for the purpose of setting the counter 32 .
- Pz denotes a point of disassembly of the projectile 18 .
- the ejected subprojectiles are, depending on the distance from the point of decomposition Pz, evenly distributed on approximately semicircular curves of (in perspective) circular areas F1, F2, F3, F4 of a cone C.
- F1, F2, F3, F4 of a cone C.
- the distance from the point of decomposition Pz is plotted in meters m
- the area sizes of the areas F1, F2, F3, F4 are plotted in square meters m 2 and their diameter in meters m.
- the warded off target designates the preceding in a meeting place or firing position (4) and in one of the meeting place or position firing position (4' is 4, and 4) is shown.
- the lead computation unit 9 calculates a target distance RT from a lead speed VOv and the target data Z, taking meteorological data into account for storeys with primary and secondary ballistics.
- the lead speed VOv is formed, for example, from the mean value of a number of measured projectile speeds Vm supplied via the data transmission 17 , which immediately precede the current measured projectile speed Vm.
- the lead computing unit 9 also determines a gun angle ⁇ of the azimuth and a gun angle I of the elevation.
- the quantities ⁇ , ⁇ , Tf and VOv are referred to as shooting elements of the meeting point and are fed to the correction computing unit 12 via the data transmission 17 .
- the shooting elements ⁇ and ⁇ are also fed to the gun servo 15 and the shooting elements VOv and Tf or Tz to the update computing unit 11 .
- the current (running) time (t) is interpolated or extrapolated.
- the correction arithmetic unit 12 calculates a correction actuator K at the beginning of each cycle i with the latest set of shooting elements ⁇ , ⁇ , Tz or Tf and VOv, for which purpose a determination equation for the correction factor K is developed as described in more detail below.
- v ⁇ rel the relative speed between floor and target and the derivation of the projectile position according to the amount of the initial speed.
- v o the relative speed between floor and target and the derivation of the projectile position according to the amount of the initial speed.
- Equation 11.1 The meeting condition is then The derivation of the equation Eq.10 after t o gives which is a breakdown of the target speed into the bullet speed and a vector C. ⁇ . represents, where is. It is known from general theory that under the given conditions the expression in equation Eq.11.1 is. In addition, the pipe speed small, so the vector in Equation 11.1 can be considered negligible. According to the general definition of the derivative, D 3 in Equation 11.1 applies If the elevation of the gun barrel 13 is neglected so that approximate results.
- Equation Eq.17 can be used to derive the flight time can be calculated by the fire control 1 using various mathematical methods. According to equation Eq. 13, ⁇ 2 is a known function of ⁇ ( t o ), ⁇ ( t o ) and ⁇ ( t o ). These sizes can either be calculated or measured directly on gun 2.
- the sizes are given by ballistics. There are functions in the first order of flight time and in the second order of pipe elevation, which can be negligible. For example, a solution according to d'Antonio can be used to determine these variables.
- the correction factor K results the sizes TG , ⁇ , ⁇ , ⁇ , ⁇ and v ⁇ o refer to the time t o .
- the disassembly distance Dz (Fig. 3, 4) can be independent of the scatter of the bullet speed be kept constant, so that an optimal meeting or Probability of shooting can be achieved.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Crushing And Grinding (AREA)
- Paper (AREA)
- Electrotherapy Devices (AREA)
- Washing And Drying Of Tableware (AREA)
- Toys (AREA)
- Gasification And Melting Of Waste (AREA)
- Fishing Rods (AREA)
- Testing Of Balance (AREA)
- Investigating, Analyzing Materials By Fluorescence Or Luminescence (AREA)
- Extrusion Moulding Of Plastics Or The Like (AREA)
- Debugging And Monitoring (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH100096 | 1996-04-19 | ||
CH1000/96 | 1996-04-19 | ||
CH100096 | 1996-04-19 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0802390A1 true EP0802390A1 (fr) | 1997-10-22 |
EP0802390B1 EP0802390B1 (fr) | 2000-10-18 |
Family
ID=4200121
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96118039A Expired - Lifetime EP0802390B1 (fr) | 1996-04-19 | 1996-11-11 | Procédé de détermination d'un temps de désintégration corrigé d'un projectile programmable et frangible |
Country Status (12)
Country | Link |
---|---|
US (1) | US5814755A (fr) |
EP (1) | EP0802390B1 (fr) |
JP (1) | JP4008520B2 (fr) |
KR (1) | KR100410719B1 (fr) |
AT (1) | ATE197090T1 (fr) |
AU (1) | AU716344B2 (fr) |
CA (1) | CA2190386C (fr) |
DE (1) | DE59606025D1 (fr) |
NO (1) | NO312143B1 (fr) |
SG (1) | SG83657A1 (fr) |
TR (1) | TR199600939A1 (fr) |
ZA (1) | ZA969543B (fr) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0992761A1 (fr) * | 1998-10-08 | 2000-04-12 | Oerlikon Contraves Pyrotec AG | Procédé de correction du déclenchement préprogrammé d'un processus dans un obus à stabilisation par rotation, dispositif de mise en oeuvre dudit procédé et utilisation dudit dispositif |
EP0992758A1 (fr) | 1998-10-08 | 2000-04-12 | Oerlikon Contraves Ag | Procédé et dispositif pour le calcul et la correction du temps de désintégration d'un projectile programmable stabilisé par rotation |
US6422119B1 (en) | 1998-10-08 | 2002-07-23 | Oerlikon Contraves Ag | Method and device for transferring information to programmable projectiles |
DE102011106198B3 (de) * | 2011-06-07 | 2012-03-15 | Rheinmetall Air Defence Ag | Verfahren zur Bestimmung der Mündungsaustrittsgeschwindigkeit eines Projektils |
DE102011018248B3 (de) * | 2011-04-19 | 2012-03-29 | Rheinmetall Air Defence Ag | Vorrichtung und Verfahren zur Programmierung eines Geschosses |
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 (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
DE102010006530B4 (de) * | 2010-02-01 | 2013-12-19 | Rheinmetall Air Defence Ag | Programmierbare Munition |
DE102010006528B4 (de) * | 2010-02-01 | 2013-12-12 | Rheinmetall Air Defence Ag | Verfahren und Vorrichtung zur Programmierung eines Projektils |
US11047663B1 (en) * | 2010-11-10 | 2021-06-29 | True Velocity Ip Holdings, Llc | Method of coding polymer ammunition cartridges |
DE102013007229A1 (de) * | 2013-04-26 | 2014-10-30 | Rheinmetall Waffe Munition Gmbh | Verfahren zum Betrieb eines Waffensystems |
US10883809B1 (en) * | 2019-05-07 | 2021-01-05 | U.S. Government As Represented By The Secretary Of The Army | Muzzle velocity correction |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4142442A (en) * | 1971-12-08 | 1979-03-06 | Avco Corporation | Digital fuze |
GB2107835A (en) * | 1981-10-20 | 1983-05-05 | Sfim | Correcting, from one shot to the next, the firing of a weapon |
US4449041A (en) * | 1980-10-03 | 1984-05-15 | Raytheon Company | Method of controlling antiaircraft fire |
EP0300255A1 (fr) | 1987-07-20 | 1989-01-25 | Werkzeugmaschinenfabrik Oerlikon-Bührle AG | Dispositif numérique de réglage d'un compteur servant à initier un détonateur à temporisation d'un obus |
EP0467055A1 (fr) * | 1990-07-19 | 1992-01-22 | Oerlikon-Contraves AG | Bobine réceptrice pour fusée programmable d'un projectile |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3575085A (en) * | 1968-08-21 | 1971-04-13 | Hughes Aircraft Co | Advanced fire control system |
US4267776A (en) * | 1979-06-29 | 1981-05-19 | Motorola, Inc. | Muzzle velocity compensating apparatus and method for a remote set fuze |
US4283989A (en) * | 1979-07-31 | 1981-08-18 | Ares, Inc. | Doppler-type projectile velocity measurement and communication apparatus, and method |
DE3309147A1 (de) * | 1983-03-15 | 1984-09-20 | Rainer Dipl.-Phys. 6901 Gaiberg Berthold | Verfahren und anordnung zur korrektur eines zuendzeitpunktes |
US4750423A (en) * | 1986-01-31 | 1988-06-14 | Loral Corporation | Method and system for dispensing sub-units to achieve a selected target impact pattern |
FR2609165A1 (fr) * | 1986-12-31 | 1988-07-01 | Thomson Brandt Armements | Projectile comportant des sous-projectiles a zone d'efficacite predefinie |
GB2226624B (en) * | 1987-12-12 | 1991-07-03 | Thorn Emi Electronics Ltd | Projectile |
DE3830518A1 (de) * | 1988-09-08 | 1990-03-22 | Rheinmetall Gmbh | Vorrichtung zur einstellung eines geschosszeitzuenders |
US5140329A (en) * | 1991-04-24 | 1992-08-18 | Lear Astronics Corporation | Trajectory analysis radar system for artillery piece |
EP0512856B1 (fr) * | 1991-05-08 | 1998-11-04 | Electronic Data Systems Corporation | Système d'arme |
CA2082448C (fr) * | 1991-05-08 | 2002-04-30 | Christopher Robert Gent | Systemes d'armes |
US5497704A (en) * | 1993-12-30 | 1996-03-12 | Alliant Techsystems Inc. | Multifunctional magnetic fuze |
-
1996
- 1996-11-08 NO NO19964756A patent/NO312143B1/no not_active IP Right Cessation
- 1996-11-11 AT AT96118039T patent/ATE197090T1/de active
- 1996-11-11 EP EP96118039A patent/EP0802390B1/fr not_active Expired - Lifetime
- 1996-11-11 DE DE59606025T patent/DE59606025D1/de not_active Expired - Lifetime
- 1996-11-13 AU AU71728/96A patent/AU716344B2/en not_active Ceased
- 1996-11-13 SG SG9611113A patent/SG83657A1/en unknown
- 1996-11-13 ZA ZA969543A patent/ZA969543B/xx unknown
- 1996-11-14 CA CA002190386A patent/CA2190386C/fr not_active Expired - Fee Related
- 1996-11-14 US US08/749,325 patent/US5814755A/en not_active Expired - Lifetime
- 1996-11-18 KR KR1019960054800A patent/KR100410719B1/ko not_active IP Right Cessation
- 1996-11-22 JP JP31172896A patent/JP4008520B2/ja not_active Expired - Fee Related
- 1996-11-22 TR TR96/00939A patent/TR199600939A1/xx unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4142442A (en) * | 1971-12-08 | 1979-03-06 | Avco Corporation | Digital fuze |
US4449041A (en) * | 1980-10-03 | 1984-05-15 | Raytheon Company | Method of controlling antiaircraft fire |
GB2107835A (en) * | 1981-10-20 | 1983-05-05 | Sfim | Correcting, from one shot to the next, the firing of a weapon |
EP0300255A1 (fr) | 1987-07-20 | 1989-01-25 | Werkzeugmaschinenfabrik Oerlikon-Bührle AG | Dispositif numérique de réglage d'un compteur servant à initier un détonateur à temporisation d'un obus |
EP0467055A1 (fr) * | 1990-07-19 | 1992-01-22 | Oerlikon-Contraves AG | Bobine réceptrice pour fusée programmable d'un projectile |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0992761A1 (fr) * | 1998-10-08 | 2000-04-12 | Oerlikon Contraves Pyrotec AG | Procédé de correction du déclenchement préprogrammé d'un processus dans un obus à stabilisation par rotation, dispositif de mise en oeuvre dudit procédé et utilisation dudit dispositif |
EP0992758A1 (fr) | 1998-10-08 | 2000-04-12 | Oerlikon Contraves Ag | Procédé et dispositif pour le calcul et la correction du temps de désintégration d'un projectile programmable stabilisé par rotation |
US6422119B1 (en) | 1998-10-08 | 2002-07-23 | Oerlikon Contraves Ag | Method and device for transferring information to programmable projectiles |
US6427598B1 (en) | 1998-10-08 | 2002-08-06 | Oerlikon Contraves Ag | Method and device for correcting the predetermined disaggregation time of a spin-stabilized programmable projectile |
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 |
DE102009011447B9 (de) * | 2009-03-03 | 2012-08-16 | Diehl Bgt Defence Gmbh & Co. Kg | Verfahren zum Zünden eines Gefechtskopfs einer Granate und Fahrzeug |
DE102011018248B3 (de) * | 2011-04-19 | 2012-03-29 | Rheinmetall Air Defence Ag | Vorrichtung und Verfahren zur Programmierung eines Geschosses |
WO2012143218A1 (fr) | 2011-04-19 | 2012-10-26 | Rheinmetall Air Defence Ag | Dispositif et procédé de programmation d'un missile |
DE102011106198B3 (de) * | 2011-06-07 | 2012-03-15 | Rheinmetall Air Defence Ag | Verfahren zur Bestimmung der Mündungsaustrittsgeschwindigkeit eines Projektils |
WO2012168190A1 (fr) | 2011-06-07 | 2012-12-13 | Rheinmetall Air Defence Ag | Procédé de détermination de la vitesse à la bouche d'un projectile |
Also Published As
Publication number | Publication date |
---|---|
CA2190386C (fr) | 2003-09-16 |
NO964756L (no) | 1997-10-20 |
JP4008520B2 (ja) | 2007-11-14 |
EP0802390B1 (fr) | 2000-10-18 |
TR199600939A1 (xx) | 1997-11-21 |
KR100410719B1 (ko) | 2004-05-06 |
ATE197090T1 (de) | 2000-11-15 |
SG83657A1 (en) | 2001-10-16 |
US5814755A (en) | 1998-09-29 |
AU7172896A (en) | 1997-10-23 |
JPH09280798A (ja) | 1997-10-31 |
DE59606025D1 (de) | 2000-11-23 |
NO964756D0 (no) | 1996-11-08 |
AU716344B2 (en) | 2000-02-24 |
CA2190386A1 (fr) | 1997-10-20 |
KR970070942A (ko) | 1997-11-07 |
NO312143B1 (no) | 2002-03-25 |
ZA969543B (en) | 1997-06-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0802391B1 (fr) | Procédé de détermination d'un temps de désintegration corrigé d'un projectile programmable et frangible | |
EP0802392B1 (fr) | Procédé et dispositif de détermination d'un temps de désintégration corrigé d'un projectile programmable et frangible | |
EP0802390B1 (fr) | Procédé de détermination d'un temps de désintégration corrigé d'un projectile programmable et frangible | |
EP0118122A1 (fr) | Procédé et dispositif de réglage d'une fusée d'amorçage chronométrique | |
DE2210277A1 (de) | Elektronisches Zündsystem | |
DE102007059397A1 (de) | Taumelzünder | |
EP1482311B1 (fr) | Dispositif et procédé de détermination de la vitesse initiale d'un projectile | |
DE3309147A1 (de) | Verfahren und anordnung zur korrektur eines zuendzeitpunktes | |
EP0411073A1 (fr) | Procede et dispositif d'amelioration de la precision du tir | |
DE2452586C3 (de) | Verfahren und Vorrichtung zur Festlegung der Dauer des Flugweges eines Geschosses | |
EP2699871B1 (fr) | Dispositif et procédé de programmation d'un missile | |
DE2528402C2 (de) | Passiver IR-Abstandszünder | |
DE1623362C3 (de) | Einrichtung zum Zünden einer Sprengladung bzw. zum Auslosen einer Funktion | |
EP0992758B1 (fr) | Procédé et dispositif pour la correction du temps de désintégration ou bien du nombre de rotations jusqu'à la désintégration d'un projectile programmable stabilisé par rotation | |
EP0992761B1 (fr) | Procédé de correction du déclenchement préprogrammé d'un processus dans un projectile à stabilisation par rotation, dispositif de mise en oeuvre dudit procédé et utilisation dudit dispositif | |
EP0992762B1 (fr) | Procédé et dispositif pour transmettre des informations à un projectile programmable | |
DE102011106198B3 (de) | Verfahren zur Bestimmung der Mündungsaustrittsgeschwindigkeit eines Projektils | |
DE60219564T2 (de) | Verfahren zum Einstellen eines Geschosszünders, Programmiereinrichtung und Zeitzünder die in einen solchem Verfahren verwendet werden | |
DE3716450C1 (en) | Setting electronic timer for munition detonator - entering type, temp. of drive charge weather and target data in fuse ignition computer | |
DE3925000C1 (de) | Verfahren zur Vorgabe einer Geschoß-Laufzeit und Vorrichtung zur Durchführung dieses Verfahrens | |
DE3903802C2 (fr) | ||
DE2658167C2 (de) | Verfahren und Vorrichtung zur Korrektur der Flugbahn eines Geschosses | |
EP0348985A2 (fr) | Fusée d'allumage pour des projectiles explosifs | |
DE102014015832B4 (de) | Verfahren zur Datenübertragung von Daten an ein Projektil während des Durchlaufes einer Waffenrohranordnung | |
DE102014015833A1 (de) | Verfahren zur Datenübertragung von Daten an ein Projektil während des Durchlaufes einer Waffenrohranordnung, wobei ein Programmiersignal mit den Daten von einer Programmiereinheit erzeugt wird |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE CH DE FR GB IT LI NL SE |
|
17P | Request for examination filed |
Effective date: 19971211 |
|
17Q | First examination report despatched |
Effective date: 19990526 |
|
RTI1 | Title (correction) |
Free format text: METHOD FOR IDENTIFYING THE DESINTEGRATION TIME OF A PROGRAMMABLE AND FRANGIBLE PROJECTILE |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: OERLIKON CONTRAVES AG |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
RTI1 | Title (correction) |
Free format text: METHOD FOR IDENTIFYING A CORRECTED DESINTEGRATION TIME OF A PROGRAMMABLE AND FRANGIBLE PROJECTILE |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE CH DE FR GB IT LI NL SE |
|
REF | Corresponds to: |
Ref document number: 197090 Country of ref document: AT Date of ref document: 20001115 Kind code of ref document: T |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REF | Corresponds to: |
Ref document number: 59606025 Country of ref document: DE Date of ref document: 20001123 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: OK PAT AG |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) |
Effective date: 20001109 |
|
ET | Fr: translation filed | ||
ITF | It: translation for a ep patent filed |
Owner name: FUMERO BREVETTI S.N.C. |
|
NLR4 | Nl: receipt of corrected translation in the netherlands language at the initiative of the proprietor of the patent | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 20101112 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20101118 Year of fee payment: 15 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R084 Ref document number: 59606025 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59606025 Country of ref document: DE Representative=s name: THUL PATENTANWALTSGESELLSCHAFT MBH, DE |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R084 Ref document number: 59606025 Country of ref document: DE Effective date: 20111021 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: BE Payment date: 20111110 Year of fee payment: 16 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59606025 Country of ref document: DE Representative=s name: THUL PATENTANWALTSGESELLSCHAFT MBH, DE |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 59606025 Country of ref document: DE Representative=s name: THUL PATENTANWALTSGESELLSCHAFT MBH, DE Effective date: 20111219 Ref country code: DE Ref legal event code: R082 Ref document number: 59606025 Country of ref document: DE Representative=s name: THUL PATENTANWALTSGESELLSCHAFT MBH, DE Effective date: 20120523 Ref country code: DE Ref legal event code: R081 Ref document number: 59606025 Country of ref document: DE Owner name: RHEINMETALL AIR DEFENCE AG, CH Free format text: FORMER OWNER: OERLIKON-CONTRAVES AG, ZUERICH, CH Effective date: 20120523 |
|
BERE | Be: lapsed |
Owner name: *OERLIKON CONTRAVES A.G. Effective date: 20121130 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 197090 Country of ref document: AT Kind code of ref document: T Effective date: 20121111 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20121111 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20121111 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20121130 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20121111 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20141119 Year of fee payment: 19 Ref country code: FR Payment date: 20141119 Year of fee payment: 19 Ref country code: SE Payment date: 20141119 Year of fee payment: 19 Ref country code: CH Payment date: 20141119 Year of fee payment: 19 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20141119 Year of fee payment: 19 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20141125 Year of fee payment: 19 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 59606025 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151130 Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151111 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151130 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MM Effective date: 20151201 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST Effective date: 20160729 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151112 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151201 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20160601 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151130 |