EP0800053B1 - Functioning testing device for an ammunition launcher - Google Patents
Functioning testing device for an ammunition launcher Download PDFInfo
- Publication number
- EP0800053B1 EP0800053B1 EP97400518A EP97400518A EP0800053B1 EP 0800053 B1 EP0800053 B1 EP 0800053B1 EP 97400518 A EP97400518 A EP 97400518A EP 97400518 A EP97400518 A EP 97400518A EP 0800053 B1 EP0800053 B1 EP 0800053B1
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- EP
- European Patent Office
- Prior art keywords
- test
- measurement
- test device
- launcher
- electronics
- 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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- 238000012360 testing method Methods 0.000 title claims abstract description 55
- 238000010304 firing Methods 0.000 claims abstract description 18
- 238000005259 measurement Methods 0.000 claims description 39
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- 210000000056 organ Anatomy 0.000 description 1
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Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
- F41A19/58—Electric firing mechanisms
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B35/00—Testing or checking of ammunition
Definitions
- the technical field of the invention is that of devices for testing the proper functioning of a ammunition launcher.
- launch tubes are frequently used to deploy ammunition such as smoke grenades or anti-personnel.
- These launch tubes generally carry means for supply of electrical energy which cooperate with means receivers of electrical energy carried by ammunition.
- These means could be, for example, contacts electric or an inductive system (such as that described by FR2438820) or a capacitive system (such as described by patent FR2593908).
- the means of energy supply lead to the ammunition an electric current intended in particular for ensure the firing of a propellant ejection charge of the ammunition out of the tube.
- the firing trigger implements a current whose intensity must be (for reasons of safety) of at least 3 amps for at least 15 milliseconds.
- the patent US5050501 describes a device for testing launcher that has the form of ammunition. This device does not not the measurement of an intensity supplied by the tube but allows only to visualize the supply of a current of operation. In addition it incorporates a battery ensuring the power supply of the display means of the good operation.
- test device allows a simple, fast and reliable verification of correct operation of the launcher.
- the subject of the invention is a device allowing to test the proper functioning of a launcher consisting of a tube capable of receiving ammunition and inside which means are provided for supplying electrical energy to ammunition intended in particular to allow its setting fire, device consisting of a body having substantially the form of ammunition and comprising receiving means of electrical energy cooperating with the means of supply energy from the launch tube, receiving means connected to a test electronics inside the body, device characterized in that the test electronics are supplied with energy by the starter tube through energy receiving means.
- the test electronics may include at least minus a capacity which is charged with energy by the launcher, capacity ensuring the electrical supply of the test.
- the test electronics includes at least a first measurement channel making it possible to check that the intensity of the current received from the starter tube during of the firing is greater than a minimum intensity for a minimum duration.
- the test electronics includes at least a second measurement channel allowing check that the intensity which is received from the starter tube of permanently outside the firing is less than maximum intensity.
- test electronics include a electronic power switch for switching the current supplied by the energy receiving means electric to one or other of the measurement channels.
- the power switch closing time will be chosen at least equal to the minimum duration.
- the device advantageously includes a switch manual, carried by the body of the device, and allowing select one or other of the measurement channels.
- the measurement result can be given by a display attached to the body.
- the test device may include a sequencer ensuring the sequencing of switching operations, measurement and display of the measurement result.
- test device 1 according to the invention is shown placed in a tube ammunition launcher 2.
- the launcher tube 2 is integral with a wall 3 of a armored vehicle and it is closed at its rear by a bottom 4 (screwed or welded to the tube) which carries means 5 of supply of electrical energy.
- These means are constituted here by a coaxial connector comprising a central pin 5a and a crown peripheral 5b, separated by an insulator 5c.
- Such a connector is shown here only for Indicative because it does not constitute the subject of the invention.
- the test device 1 has the external shape and the size of real ammunition, which facilitates its storage and handling.
- It consists of a body comprising an envelope tubular 6 closed by a cover 7 and a base 8, fixed to the envelope 6 for example by screws (not shown).
- the base 8 carries energy receiving means electric 9 which are intended to cooperate with the means of 5 energy supply from the starter tube.
- These means are here constituted by a coaxial connector having a central pin 9a and a crown peripheral 9b separated by an insulator 9c.
- test device In the case of inductive means of transmission, the test device would carry a take-up reel which would find in inductive coupling with the emitting coil of the launcher tube.
- the cover 7 carries a manual switch with two positions 10, as well as a means of displaying the result of the test, means constituted here by two indicator lights 11a, 11b (diodes LED) of different colors (Green and Red).
- the cover 7 is set back at inside the envelope 6, this in order to ensure the protection of manual switch 10 and displays 11a, 11b.
- the body of the test device contains a card electronic carrying an electronic test circuit 12 which is connected to the contacts 9a, 9b of the connector 9 by the conductors 14a, 14b as well as the manual switch 10 and the LEDs 11a, 11b.
- All the free space inside the body of the device is filled with an insulating and shock absorbing plastic material 13 like a coating resin.
- the filling material is poured into the envelope 6 after positioning of circuit 12 and installation of electrical connections.
- the cover 7 is then fixed to the envelope by an appropriate connecting means not shown (e.g. screws).
- FIG. 2 is a block diagram of the circuit test electronics 12.
- One of the contacts 9b is the common point for the whole of the circuit, the other contact 9a supplies a capacitor 15 which is intended to supply energy to the entire circuit 12.
- test device does not contain no energy source (battery, battery) likely to degrade or discharge during storage.
- energy source battery, battery
- the energy needed to the operation of the circuits is borrowed from the network of on board the vehicle at the time of the test and stored in the capacity 15.
- the test circuit includes a first measurement channel 16 and a second measurement channel 17.
- the current supplied by the contacts is applied to a power switch 18 which has the function of switching the current supplied by the contacts in one or other of the measurement channels during the time required for measurement.
- This switch is constituted for example by a transistor of power.
- Each measurement channel 16,17 consists of a sensor current of known type which performs a measurement of intensity by measuring the voltage across a calibrated resistance.
- These sensors can be controlled by a control signal which triggers the start of the measurement and they provide a voltage representative of the measured current.
- the selection of the measurement to be carried out and therefore of the channel measurement to be activated is carried out via the manual switch 10.
- the first measurement channel 16 is intended to measure the firing current (I) which to be sufficient (allow ammunition) must be greater than one minimum intensity Im (of the order of 3 amperes) during one minimum duration Tm (of the order of 15 milliseconds).
- a first comparator 21 makes it possible to compare the value measured at a setpoint supplied by a reference circuit of voltage 20 which is composed for example of a diode of voltage reference associated with a potentiometric divider.
- the duration Tm of the measurement is obtained by a sequencer 19 of known type which includes a quartz oscillator and a counter.
- the signal resulting from the comparison between the measurement and the setpoint is sampled by the oscillator of the sequencer 19 to increment a counter 25, the sampling will for example be carried out using a AND logic gate.
- the counter does not increment each time clock slot only if the comparator provides a signal logic "1" signifying that the measured current is correct.
- a outputs of counter 25 which goes to a logic level "1" for a sufficient counting level taking into account the duration Tm (therefore when the current measured was correct during the duration Tm).
- the display circuit 22 is controlled by the sequencer 19 and it ensures the lighting of one or other of the Led displays (11a or 11b) depending on the signal supplied by the counter 25 at the end of the measurement time Tm (level “1" provided by the counter 25 controls the lighting of the green LED, the signal "0", the red LED lights up).
- the second measurement channel 17 has a similar operation. It is intended to measure the safety current which circulates in the ammunition when it is placed in the tube and when firing is not requested. To be correct (do not cause inadvertent ignition) this current (i) must not exceed a maximum value i M (i M of the order of 100 milliamps).
- Another voltage reference circuit 23 (mounting potentiometer) generates a voltage setpoint which is image of the maximum intensity value iM.
- a second comparator 24 compares this value with the measured value by measurement circuit 17 and provides a signal which is sampled by the sequencer 19 oscillator to increment the counter 25, which delivers the control signal of the display circuit 22.
- the power switch 18, as well as the measures 16 and 17 and the display circuit 22, are controlled by the sequencer 19 which, like a microprocessor, ensures the sequencing of different operations.
- Figure 3a is a timing diagram which represents the temporal sequence of operations when the first measurement channel is chosen.
- the user who installed the ammunition can first check that the vehicle's electrical system correctly detects the presence of the test ammunition (ignition an ammunition presence indicator on its control console).
- test circuit 16 After approximately 550 milliseconds (time required to stabilization of internal functions), the test circuit 16, controlled by the sequencer 19, performs the measurement (time slot 27).
- the display of the red or green indicator is controlled by the sequencer 19 (slot 28).
- This display persists for 1 to 2 seconds after release of the firing button. This duration corresponds to the discharge of the capacitor 15 in the organs of display (Led 11a or 11b).
- Figure 3b is a timing diagram which represents the temporal sequence of operations when the second measurement channel is chosen.
- the user has set the manual switch 10 to the position corresponding to the safety current measurement.
- the device then uses the energy supplied by the tube launch to load capacity 15.
- test circuit 17, controlled by the sequencer 19 performs the measurement of the safety current (slot 30), and this during a measurement time Tm.
- Button release detection is performed by another comparator circuit (not shown in the diagram of Figure 2) and which detects the disappearance of the energy supplied by the launch tube.
- the display of the red or green indicator is controlled by the sequencer 19 (slot 31).
- the display persists for one certain duration corresponding to the discharge of the capacitor 15 in the display devices (LED 11a or 11b).
- test device allows to carry out in an extremely simple way all the launcher test operations.
- the only action requested of the operator is to press the firing button and this as well for testing the firing current as for that of the safety current.
- the measurement result is presented to him in a simple way by the two LEDs.
- the test device is implemented as a normal ammunition and is not more bulky than this one, which allows it to be carried in all vehicles.
- test device with only one measurement channel (e.g. firing current).
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- General Engineering & Computer Science (AREA)
- Eye Examination Apparatus (AREA)
- Maintenance And Inspection Apparatuses For Elevators (AREA)
- Testing Electric Properties And Detecting Electric Faults (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
Le domaine technique de l'invention est celui des dispositifs permettant de tester le bon fonctionnement d'un lanceur de munition.The technical field of the invention is that of devices for testing the proper functioning of a ammunition launcher.
Pour assurer la protection rapprochée des véhicules blindés, on utilise fréquemment des tubes lanceurs permettant de déployer des munitions telles que des grenades fumigènes ou antipersonnel.To ensure close protection of vehicles armored, launch tubes are frequently used to deploy ammunition such as smoke grenades or anti-personnel.
Ces tubes lanceurs portent généralement des moyens de fourniture d'énergie électrique qui coopèrent avec des moyens récepteurs d'énergie électrique portés par la munition.These launch tubes generally carry means for supply of electrical energy which cooperate with means receivers of electrical energy carried by ammunition.
Ces moyens pourront être par exemple des contacts électriques ou bien un système inductif (tel celui décrit par le brevet FR2438820) ou encore un système capacitif (tel que décrit par le brevet FR2593908).These means could be, for example, contacts electric or an inductive system (such as that described by FR2438820) or a capacitive system (such as described by patent FR2593908).
Les moyens de fourniture d'énergie conduisent à la munition un courant électrique destiné en particulier à assurer la mise à feu d'une charge propulsive d'éjection de la munition hors du tube.The means of energy supply lead to the ammunition an electric current intended in particular for ensure the firing of a propellant ejection charge of the ammunition out of the tube.
Ils permettent aussi de vérifier la présence d'une munition dans le lanceur et éventuellement de déterminer le type de munition qui est présent.They also make it possible to verify the presence of a ammunition in the launcher and possibly determine the type of ammunition that is present.
Il est très difficile aujourd'hui d'assurer de façon simple, rapide et fiable le contrôle du bon fonctionnement de tels lanceurs.It is very difficult today to insure simple, fast and reliable checking the proper functioning of such launchers.
En effet, d'une part, en l'absence de tir, il doit circuler dans la munition un courant inférieur à 100 milliampères, courant permettant de détecter la présence de la munition et ne devant pas entraíner un tir intempestif.On the one hand, in the absence of a shot, it must circulate in the ammunition a current lower than 100 milliamperes, current to detect the presence of the ammunition and not to cause untimely shooting.
D'autre part, le déclenchement de tir met en oeuvre un courant dont l'intensité doit être (pour des raisons de sécurité) d'au moins 3 ampères pendant au moins 15 millisecondes.On the other hand, the firing trigger implements a current whose intensity must be (for reasons of safety) of at least 3 amps for at least 15 milliseconds.
Le bon fonctionnement du lanceur n'est effectif que lorsque ces deux conditions sont respectées.The proper functioning of the launcher is only effective when these two conditions are met.
Les moyens de contrôle connus mettent en oeuvre des bancs de mesure d'intensité qui sont encombrants, coûteux et difficiles à utiliser par des personnels non formés.Known control means use benches bulky, expensive and difficult to use by untrained personnel.
D'autres moyens de contrôles classiques utilisent une lampe test qui permet de vérifier la fourniture de courant par le tube lanceur.Other conventional control means use a test lamp to check the current supply by the starter tube.
Cependant ces derniers moyens ne permettent pas de vérifier le bon fonctionnement du lanceur, c'est à dire la conformité de ses deux intensités d'emploi (repos / tir) avec les valeurs normales.However, these latter means do not allow check the correct functioning of the launcher, i.e. the conformity of its two intensities of use (rest / shooting) with normal values.
Le brevet US5050501 décrit un dispositif de test de lanceur qui a la forme d'une munition. Ce dispositif n'assure pas la mesure d'une intensité fournie par le tube mais permet uniquement de visualiser la fourniture d'un courant de fonctionnement. De plus il incorpore une pile assurant l'alimentation en énergie des moyens de visualisation du bon fonctionnement.The patent US5050501 describes a device for testing launcher that has the form of ammunition. This device does not not the measurement of an intensity supplied by the tube but allows only to visualize the supply of a current of operation. In addition it incorporates a battery ensuring the power supply of the display means of the good operation.
C'est le but de l'invention que de proposer un dispositif de test ne présentant pas de tels inconvénients.It is the object of the invention to propose a device no such drawbacks.
Ainsi le dispositif de test selon l'invention permet une vérification simple, rapide et fiable du bon fonctionnement du lanceur.Thus the test device according to the invention allows a simple, fast and reliable verification of correct operation of the launcher.
Il peut être mis en oeuvre par un personnel non qualifié et il est à la fois peu encombrant et peu coûteux.It can be implemented by unqualified personnel and it is both space-saving and inexpensive.
Il peut être stocké durant de longues périodes sans perdre sa précision et peut être conservé dans tout véhicule blindé en plus de la dotation en munitions.It can be stored for long periods without lose accuracy and can be stored in any vehicle armored in addition to the ammunition endowment.
Ainsi l'invention a pour objet un dispositif permettant de tester le bon fonctionnement d'un lanceur constitué d'un tube pouvant recevoir une munition et à l'intérieur duquel sont disposés des moyens de fourniture d'énergie électrique à la munition destinés en particulier à permettre sa mise à feu, dispositif constitué par un corps ayant sensiblement la forme d'une munition et comportant des moyens récepteurs d'énergie électrique coopérant avec les moyens de fourniture d'énergie du tube lanceur, moyens récepteurs reliés à une électronique de test disposée à l'intérieur du corps, dispositif caractérisé en ce que l'électronique de test est alimentée en énergie par le tube lanceur au travers des moyens récepteurs d'énergie.Thus the subject of the invention is a device allowing to test the proper functioning of a launcher consisting of a tube capable of receiving ammunition and inside which means are provided for supplying electrical energy to ammunition intended in particular to allow its setting fire, device consisting of a body having substantially the form of ammunition and comprising receiving means of electrical energy cooperating with the means of supply energy from the launch tube, receiving means connected to a test electronics inside the body, device characterized in that the test electronics are supplied with energy by the starter tube through energy receiving means.
En particulier, l'électronique de test peut comporter au moins une capacité qui est chargée en énergie par le lanceur, capacité assurant l'alimentation électrique du dispositif de test.In particular, the test electronics may include at least minus a capacity which is charged with energy by the launcher, capacity ensuring the electrical supply of the test.
Selon une autre caractéristique, l'électronique de test comporte au moins une première voie de mesure permettant de vérifier que l'intensité du courant reçu du tube lanceur lors de la mise à feu est supérieure à une intensité minimale pendant une durée minimale.According to another characteristic, the test electronics includes at least a first measurement channel making it possible to check that the intensity of the current received from the starter tube during of the firing is greater than a minimum intensity for a minimum duration.
Selon une autre caractéristique, l'électronique de test comporte au moins une deuxième voie de mesure permettant de vérifier que l'intensité qui est reçue du tube lanceur de façon permanente en dehors de la mise à feu est inférieure à une intensité maximale.According to another characteristic, the test electronics includes at least a second measurement channel allowing check that the intensity which is received from the starter tube of permanently outside the firing is less than maximum intensity.
Avantageusement, l'électronique de test comprend un commutateur électronique de puissance permettant de commuter le courant fourni par les moyens récepteurs d'énergie électrique vers l'une ou l'autre des voies de mesure.Advantageously, the test electronics include a electronic power switch for switching the current supplied by the energy receiving means electric to one or other of the measurement channels.
Le temps de fermeture du commutateur de puissance sera choisi au moins égal à la durée minimale.The power switch closing time will be chosen at least equal to the minimum duration.
Le dispositif comporte avantageusement un commutateur manuel, porté par le corps du dispositif, et permettant de sélectionner l'une ou l'autre des voies de mesures.The device advantageously includes a switch manual, carried by the body of the device, and allowing select one or other of the measurement channels.
Le résultat des mesures peut être donné par un afficheur solidaire du corps.The measurement result can be given by a display attached to the body.
Le dispositif de test pourra comporter un séquenceur assurant le séquencement des opérations de commutation, de mesure et d'affichage du résultat de la mesure.The test device may include a sequencer ensuring the sequencing of switching operations, measurement and display of the measurement result.
L'invention sera mieux comprise à la lecture de la description qui va suivre d'un mode particulier de réalisation, description faite en référence aux dessins annexés et dans lesquels:
- la figure 1 est un vue en coupe d'un dispositif de test selon l'invention mis en place dans un tube lanceur,
- la figure 2 est un schéma synoptique du dispositif de test selon l'invention,
- les figures 3a et 3b sont des chronogrammes montrant les séquences de fonctionnement, respectivement pour les mesures des courants de mise à feu et de sécurité.
- FIG. 1 is a sectional view of a test device according to the invention placed in a launch tube,
- FIG. 2 is a block diagram of the test device according to the invention,
- Figures 3a and 3b are timing diagrams showing the operating sequences, respectively for the measurement of firing and safety currents.
En se reportant à la figure 1, un dispositif de test 1
selon l'invention est représenté mis en place dans un tube
lanceur 2 de munition.Referring to Figure 1, a test device 1
according to the invention is shown placed in a
Le tube lanceur 2 est solidaire d'une paroi 3 d'un
véhicule blindé et il est fermé à sa partie arrière par un
fond 4 (vissé ou soudé au tube) qui porte des moyens 5 de
fourniture d'énergie électrique. The
Ces moyens sont constitués ici par un connecteur coaxial
comportant une broche centrale 5a et une couronne
périphérique 5b, séparées par un isolant 5c.These means are constituted here by a coaxial connector
comprising a central pin 5a and a crown
peripheral 5b, separated by an
Un tel connecteur n'est représenté ici qu'à titre Indicatif car il ne constitue pas l'objet de l'invention.Such a connector is shown here only for Indicative because it does not constitute the subject of the invention.
Il peut être remplacé par tous types de contacts électriques ayant une autre structure (par exemple des contacts à baïonnette) ou encore par un moyen de fourniture d'énergie de nature différente, formé par exemple par une bobine d'induction.It can be replaced by all types of contacts having another structure (e.g. bayonet contacts) or by a means of supply energy of different nature, formed for example by a induction coil.
Le dispositif de test 1 a la forme externe et l'encombrement d'une munition réelle, ce qui facilite son stockage et sa manipulation.The test device 1 has the external shape and the size of real ammunition, which facilitates its storage and handling.
Il est constitué par un corps comprenant une enveloppe
tubulaire 6 fermée par un couvercle 7 et un culot 8, fixés à
l'enveloppe 6 par exemple par des vis (non représentées).It consists of a body comprising an envelope
tubular 6 closed by a cover 7 and a
Le culot 8 porte des moyens récepteurs d'énergie
électrique 9 qui sont destinés à coopérer avec les moyens de
fourniture d'énergie 5 du tube lanceur.The
Ces moyens sont ici constitués par un connecteur coaxial
présentant une broche centrale 9a et une couronne
périphérique 9b séparées par un isolant 9c.These means are here constituted by a coaxial connector
having a
Dans le cas de moyens de transmission inductifs, le dispositif de test porterait une bobine réceptrice qui se trouverait en couplage inductif avec la bobine émettrice du tube lanceur.In the case of inductive means of transmission, the test device would carry a take-up reel which would would find in inductive coupling with the emitting coil of the launcher tube.
Le couvercle 7 porte un commutateur manuel à deux
positions 10, ainsi qu'un moyen d'affichage du résultat du
test, moyen constitué ici par deux voyants 11a, 11b (diodes
LED) de couleurs différentes (Verte et Rouge).The cover 7 carries a manual switch with two
Avantageusement le couvercle 7 est disposé en retrait à
l'intérieur de l'enveloppe 6, cela afin d'assurer la
protection du commutateur manuel 10 et des afficheurs
11a, 11b.Advantageously, the cover 7 is set back at
inside the
Le corps du dispositif de test renferme une carte
électronique portant un circuit électronique de test 12 qui
est relié aux contacts 9a, 9b du connecteur 9 par les
conducteurs 14a,14b ainsi qu'au commutateur manuel 10 et aux
voyants 11a, 11b.The body of the test device contains a card
electronic carrying an
Tout l'espace libre à l'intérieur du corps du dispositif
est rempli d'un matériau plastique 13 isolant et amortisseur
tel une résine d'enrobage.All the free space inside the body of the device
is filled with an insulating and shock absorbing
Le matériau de remplissage est versé dans l'enveloppe 6
après positionnement du circuit 12 et mise en place des
liaisons électriques. Le couvercle 7 est ensuite fixé à
l'enveloppe par un moyen de liaison approprié non représenté
(par exemple des vis).The filling material is poured into the
La figure 2 est un schéma synoptique du circuit
électronique de test 12.Figure 2 is a block diagram of the
Un des contacts 9b est le point commun à l'ensemble du
circuit, l'autre contact 9a alimente une capacité 15 qui est
destinée à fournir de l'énergie à l'ensemble du circuit 12.One of the
Ainsi le dispositif de test selon l'invention ne contient
aucune source d'énergie (pile, batterie) susceptible de se
dégrader ou décharger lors du stockage. L'énergie nécessaire
au fonctionnement des circuits est empruntée au réseau de
bord du véhicule au moment du test et stockée dans la
capacité 15.Thus the test device according to the invention does not contain
no energy source (battery, battery) likely to
degrade or discharge during storage. The energy needed
to the operation of the circuits is borrowed from the network of
on board the vehicle at the time of the test and stored in the
Il en résulte une excellente tenue au stockage du dispositif de test et une simplification de la logistique.This results in excellent storage behavior of the test device and simplification of logistics.
Le circuit de test comprend une première voie de mesure
16 et une deuxième voie de mesure 17.The test circuit includes a
Le courant fourni par les contacts est appliqué à un
commutateur de puissance 18 qui a pour fonction de commuter
le courant fourni par les contacts dans l'une ou l'autre des
voies de mesure durant le temps nécessaire à la mesure. Ce
commutateur est constitué par exemple par un transistor de
puissance.The current supplied by the contacts is applied to a
Chaque voie de mesure 16,17 est constituée par un capteur
de courant de type connu qui réalise une mesure de
l'intensité par la mesure de la tension aux bornes d'une
résistance calibrée.Each
Ces capteurs sont pilotables par un signal de commande qui déclenche le début de la mesure et ils fournissent une tension représentative de l'intensité mesurée.These sensors can be controlled by a control signal which triggers the start of the measurement and they provide a voltage representative of the measured current.
La sélection de la mesure à effectuer et donc de la voie
de mesure à activer s'effectue par l'intermédiaire du
commutateur manuel 10.The selection of the measurement to be carried out and therefore of the channel
measurement to be activated is carried out via the
La première voie de mesure 16 est destinée à mesurer le
courant de mise à feu (I) qui pour être suffisant (permettre
la mise à feu de la munition) doit être supérieur à une
intensité minimale Im (de l'ordre de 3 ampères) pendant une
durée minimale Tm (de l'ordre de 15 millisecondes).The
Un premier comparateur 21 permet de comparer la valeur
mesurée à une consigne fournie par un circuit de référence de
tension 20 qui est composé par exemple d'une diode de
référence de tension associée à un diviseur potentiométrique.A
La durée Tm de la mesure est obtenue par un séquenceur 19
de type connu qui comprend un oscillateur à quartz et un
compteur.The duration Tm of the measurement is obtained by a
Durant la durée Tm, le signal résultant de la comparaison
entre la mesure et la consigne est échantillonné par
l'oscillateur du séquenceur 19 pour incrémenter un compteur
25, l'échantillonnage sera par exemple réalisé à l'aide d'une
porte logique ET. Le compteur ne s'incrémente donc à chaque
créneau d'horloge que si le comparateur fournit un signal
logique "1" signifiant que le courant mesuré est correct.During the duration Tm, the signal resulting from the comparison
between the measurement and the setpoint is sampled by
the oscillator of the
Pour commander un circuit d'affichage 22, on utilise une
des sorties du compteur 25 qui passe à un niveau logique "1"
pour un niveau de comptage suffisant compte tenu de la durée
Tm (donc lorsque le courant mesuré a été correct pendant la
durée Tm).To control a
Le circuit d'affichage 22 est piloté par le séquenceur 19
et il assure l'allumage de l'un ou l'autre des afficheurs Led
(11a ou 11b) en fonction du signal fourni par le compteur 25
à l'issue de la durée de mesure Tm (le niveau "1" fourni par
le compteur 25 commande l'allumage de la Led verte, le signal
"0", l'allumage de la Led rouge).The
La deuxième voie de mesure 17 a un fonctionnement
analogue. Elle est destinée à mesurer le courant de sécurité
qui circule dans la munition lorsqu'elle est mise en place
dans le tube et que la mise à feu n'est pas demandée. Pour
être correct (ne pas provoquer de mise à feu intempestive) ce
courant (i) ne doit pas dépasser une valeur maximale iM (iM
de l'ordre de 100 milliampères).The
Une autre circuit de référence de tension 23 (montage
potentiomètrique) génère une consigne de tension qui est
image de la valeur de l'intensité maximale iM. Un deuxième
comparateur 24 compare cette valeur avec la valeur mesurée
par le circuit de mesure 17 et fournit un signal qui est
échantillonné par l'oscillateur du séquenceur 19 pour
incrémenter le compteur 25, qui délivre le signal de commande
du circuit d'affichage 22.Another voltage reference circuit 23 (mounting
potentiometer) generates a voltage setpoint which is
image of the maximum intensity value iM. A
Le commutateur de puissance 18, ainsi que les voies de
mesure 16 et 17 et le circuit d'affichage 22, sont pilotés
par le séquenceur 19 qui, tel un microprocesseur, assure le
séquencement des différentes opérations.The
La figure 3a est un chronogramme qui représente l'enchaínement temporel des opérations lorsque la première voie de mesure est choisie.Figure 3a is a timing diagram which represents the temporal sequence of operations when the first measurement channel is chosen.
L'utilisateur qui a mis la munition en place peut tout d'abord vérifier que le circuit électrique du véhicule détecte bien la présence de la munition de test (allumage d'un voyant "présence munition" sur son pupitre de commande).The user who installed the ammunition can first check that the vehicle's electrical system correctly detects the presence of the test ammunition (ignition an ammunition presence indicator on its control console).
Il a choisi la position du commutateur manuel 10 qui
correspond au test du courant de mise à feu.He chose the position of
Il appuie sur le bouton de mise à feu pendant une durée d'au moins 1 seconde (ce qui correspond au créneau 26).It presses the firing button for a duration at least 1 second (which corresponds to time slot 26).
Cette action assure la présence du courant du réseau de
bord du véhicule aux contacts du dispositif pendant une durée
suffisante pour assurer la charge du condensateur 15.This action ensures the presence of current from the
vehicle edge in contact with the device for a period
sufficient to charge the
Au bout d'environ 550 millisecondes (temps nécessaire à
la stabilisation des fonctions internes), le circuit de test
16, commandé par le séquenceur 19, réalise la mesure (créneau
27).After approximately 550 milliseconds (time required to
stabilization of internal functions), the
A l'issue de la durée Tm (15 ms) de ce créneau, l'affichage du voyant rouge ou vert est commandé par le séquenceur 19 (créneau 28).At the end of the duration Tm (15 ms) of this slot, the display of the red or green indicator is controlled by the sequencer 19 (slot 28).
Cet affichage persiste pendant 1 à 2 secondes après le
relâchement du bouton de mise à feu. Cette durée correspond à
la décharge du condensateur 15 dans les organes de
visualisation (Led 11a ou 11b). This display persists for 1 to 2 seconds after
release of the firing button. This duration corresponds to
the discharge of the
La figure 3b est un chronogramme qui représente l'enchaínement temporel des opérations lorsque la deuxième voie de mesure est choisie.Figure 3b is a timing diagram which represents the temporal sequence of operations when the second measurement channel is chosen.
L'utilisateur a positionné le commutateur manuel 10 sur
la position correspondant à la mesure du courant de sécurité.The user has set the
Il appuie sur le bouton de mise à feu pendant une durée de l'ordre de 1 sec (créneau 29).It presses the firing button for a duration of the order of 1 sec (slot 29).
Le dispositif utilise alors l'énergie fournie par le tube
de lancement pour charger la capacité 15.The device then uses the energy supplied by the tube
launch to load
Lorsque l'utilisateur relâche le bouton de mise à feu, le
circuit de test 17, commandé par le séquenceur 19, effectue
la mesure du courant de sécurité (créneau 30), et cela
pendant une durée de mesure Tm.When the user releases the fire button, the
La détection du relâchement du bouton est effectuée par un autre circuit comparateur (non représenté sur le schéma de la figure 2) et qui détecte la disparition de l'énergie fournie par le tube de lancement.Button release detection is performed by another comparator circuit (not shown in the diagram of Figure 2) and which detects the disappearance of the energy supplied by the launch tube.
A l'issue de la durée Tm (15 ms) du créneau 30,
l'affichage du voyant rouge ou vert est commandé par le
séquenceur 19 (créneau 31). L'affichage persiste pendant une
certaine durée correspondant à la décharge du condensateur 15
dans les organes de visualisation (LED 11a ou 11b).At the end of the duration Tm (15 ms) of the
On voit que le dispositif de test selon l'invention permet de réaliser d'une façon extrêmement simple toutes les opérations de test du lanceur.It can be seen that the test device according to the invention allows to carry out in an extremely simple way all the launcher test operations.
La seule action demandée à l'opérateur est d'appuyer sur le bouton de mise à feu et cela aussi bien pour le test du courant de mise à feu que pour celui du courant de sécurité.The only action requested of the operator is to press the firing button and this as well for testing the firing current as for that of the safety current.
Le résultat de la mesure lui est présenté de façon simple par les deux voyants.The measurement result is presented to him in a simple way by the two LEDs.
Le dispositif de test est mis en oeuvre comme une munition normale et n'est pas plus encombrant que celle ci, ce qui autorise son emport dans tous les véhicules.The test device is implemented as a normal ammunition and is not more bulky than this one, which allows it to be carried in all vehicles.
Il ne contient aucune source d'énergie et peut donc être stocké indéfiniment sans perte de performances.It contains no energy sources and can therefore be stored indefinitely without loss of performance.
A titre de variante, il est possible de définir un dispositif de test ne comportant qu'une seule voie de mesure (par exemple le courant de mise à feu).As a variant, it is possible to define a test device with only one measurement channel (e.g. firing current).
Claims (9)
- A device (1) to test the functionability of a launcher formed of a tube able to receive a munition and inside which electrical power supply means (5) are arranged for the munition intended in particular to allow it to be fired, said device being constituted by a substantially munition-shaped body (6, 7, 8) incorporating electrical power receiving means (9) co-operating with the electrical supply means (5) of the launcher tube, said receiving means being connected to test electronics (12) placed inside the body, device characterised in that the test electronics (12) are supplied with power by the launcher tube via the power receiving means (9).
- A test device according to Claim 1, characterised in that the test electronics (12) incorporate at least one capacitor (15) that is powered by the launcher, said capacitor providing the electrical power for the test device.
- A test device according to one of Claims 1 or 2, characterised in that the test electronics (12) incorporate at least a first measurement channel (16) to verify that the intensity of the current received by the launcher tube during firing is greater than a minimal intensity during a minimal duration (Tm).
- A test device according to one of Claims 1 to 3, characterised in that the test electronics (12) incorporate at least a second measurement channel (17) to verify that the intensity received by the launcher tube constantly excluding during firing is less than a maximal intensity (iM).
- A test device according to one of Claims 3 or 4, characterised in that the test electronics (12) comprise an electronic power switch (18) to switch the power supplied by the electrical power receiving means (9) towards one or other of the measurement channels (16, 17).
- A test device according to Claim 5, characterised in that the power switch closure time (18) is at least equal to the minimal duration (Tm).
- A test device according to one of Claims 5 or 6, characterised in that it incorporates a manual switch (10), carried on the device's body, enabling one or other of the measurement channels (16, 17) to be selected.
- A test device according to one of Claims 1 to 7, characterised in that the measurement result is given by a display (11a, 11b) integral with the body.
- A test device according to one of Claim 3 to 8, characterised in that it incorporates a sequencer (19) ensuring the sequencing of the switching, measurement and measurement result display operations.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9604115A FR2746911B1 (en) | 1996-04-02 | 1996-04-02 | DEVICE FOR TESTING THE OPERATION OF AN AMMUNITION LAUNCHER |
FR9604115 | 1996-04-02 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0800053A1 EP0800053A1 (en) | 1997-10-08 |
EP0800053B1 true EP0800053B1 (en) | 2001-11-07 |
Family
ID=9490815
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97400518A Expired - Lifetime EP0800053B1 (en) | 1996-04-02 | 1997-03-07 | Functioning testing device for an ammunition launcher |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0800053B1 (en) |
AT (1) | ATE208487T1 (en) |
DE (1) | DE69707953T2 (en) |
FR (1) | FR2746911B1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2758161C1 (en) * | 2021-03-22 | 2021-10-26 | Федеральное государственное бюджетное образовательное учреждение высшего образования «Амурский государственный университет» | Universal simulator of transport and launch container for conducting vibrodynamic tests of cubesat standard satellites |
RU211274U1 (en) * | 2021-12-29 | 2022-05-30 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Амурский государственный университет" | Simulator of the transport and launch container for the behavior of vibration-dynamic tests of satellites of the CubeSat 1U-3U standard |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
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RU2279030C1 (en) * | 2005-01-11 | 2006-06-27 | Открытое акционерное общество специального машиностроения и металлургии "Мотовилихинские заводы" | Method and device for test of multibarreled launcher |
CA2831189A1 (en) | 2011-03-29 | 2012-10-04 | Dynaenergetics Gmbh & Co. Kg | Packing for hollow charges |
RU2519615C1 (en) * | 2013-02-12 | 2014-06-20 | Сергей Михайлович Мужичек | Method for determining characteristics of fragmentation field of ammunition, and device for its implementation |
RU2519608C1 (en) * | 2013-02-13 | 2014-06-20 | Сергей Михайлович Мужичек | Method for determining characteristics of fragmentation field of ammunition, and device for its implementation |
RU2519618C1 (en) * | 2013-02-19 | 2014-06-20 | Сергей Михайлович Мужичек | Method for determining characteristics of fragmentation field of ammunition, and device for its implementation |
RU2519611C1 (en) * | 2013-02-26 | 2014-06-20 | Сергей Михайлович Мужичек | Method for determining characteristics of fragmentation field of ammunition, and device for its implementation |
RU2519617C1 (en) * | 2013-03-12 | 2014-06-20 | Сергей Михайлович Мужичек | Method for determining characteristics of fragmentation field of ammunition, and device for its implementation |
RU2518678C1 (en) * | 2013-03-26 | 2014-06-10 | Сергей Михайлович Мужичек | Method of determining characteristics of fragmentation field of ammunition and device for its implementation |
RU2521932C1 (en) * | 2013-04-05 | 2014-07-10 | Сергей Михайлович Мужичек | Method of remote ammunition piercing effect estimation and device to this end |
RU2521460C1 (en) * | 2013-04-18 | 2014-06-27 | Сергей Михайлович Мужичек | Method of remote ammunition incendiary effect estimation and device to this end |
CN103357138A (en) * | 2013-07-25 | 2013-10-23 | 成都陵川特种工业有限责任公司 | Detection seat of fire extinguishing launcher |
CN103357137A (en) * | 2013-07-25 | 2013-10-23 | 成都陵川特种工业有限责任公司 | Apparatus for detecting fire extinguishing launcher |
CN110749253B (en) * | 2019-10-24 | 2021-11-30 | 中国人民解放军32181部队 | Missile performance test unit for missile test system |
DE102021107186A1 (en) | 2021-03-23 | 2022-09-29 | Krauss-Maffei Wegmann Gmbh & Co. Kg | throwing body replica |
CN116379846B (en) * | 2023-06-06 | 2023-09-05 | 北京星河动力装备科技有限公司 | Rocket flight time sequence verification device and system |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3374429A (en) * | 1964-05-15 | 1968-03-19 | Navy Usa | Bridge circuit for determining the thermal parameters of bridgewires used in electro-explosive devices |
US3562640A (en) * | 1969-01-15 | 1971-02-09 | Us Army | Apparatus for testing exploding bridgewire ordnance devices for continuity and shorts |
DE3940595A1 (en) * | 1989-12-08 | 1991-06-13 | Rheinmetall Gmbh | ARM PISTON FOR GOOD TEST AND ACCEPTANCE SHOTS OF A GRENADE |
US5050501A (en) * | 1991-01-07 | 1991-09-24 | The United States Of America As Represented By The Secretary Of The Army | Projected grenade simulator |
-
1996
- 1996-04-02 FR FR9604115A patent/FR2746911B1/en not_active Expired - Fee Related
-
1997
- 1997-03-07 AT AT97400518T patent/ATE208487T1/en not_active IP Right Cessation
- 1997-03-07 DE DE69707953T patent/DE69707953T2/en not_active Expired - Fee Related
- 1997-03-07 EP EP97400518A patent/EP0800053B1/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2758161C1 (en) * | 2021-03-22 | 2021-10-26 | Федеральное государственное бюджетное образовательное учреждение высшего образования «Амурский государственный университет» | Universal simulator of transport and launch container for conducting vibrodynamic tests of cubesat standard satellites |
RU211274U1 (en) * | 2021-12-29 | 2022-05-30 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Амурский государственный университет" | Simulator of the transport and launch container for the behavior of vibration-dynamic tests of satellites of the CubeSat 1U-3U standard |
Also Published As
Publication number | Publication date |
---|---|
FR2746911A1 (en) | 1997-10-03 |
ATE208487T1 (en) | 2001-11-15 |
DE69707953T2 (en) | 2002-05-29 |
DE69707953D1 (en) | 2001-12-13 |
EP0800053A1 (en) | 1997-10-08 |
FR2746911B1 (en) | 1998-05-22 |
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