EP0800053B1 - Dispositif de test de fonctionnement d'un lanceur de munitions - Google Patents
Dispositif de test de fonctionnement d'un lanceur de munitions 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
- Authority
- 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
Links
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).
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Maintenance And Inspection Apparatuses For Elevators (AREA)
- Eye Examination Apparatus (AREA)
- Testing Electric Properties And Detecting Electric Faults (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
- 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.
Claims (9)
- Dispositif (1) 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 (5) de fourniture d'énergie électrique à la munition destinés en particulier à permettre sa mise à feu, dispositif constitué par un corps (6,7,8) ayant sensiblement la forme d'une munition et comportant des moyens (9) récepteurs d'énergie électrique coopérant avec les moyens (5) de fourniture d'énergie du tube lanceur, moyens récepteurs reliés à une électronique de test (12) disposée à l'intérieur du corps, dispositif caractérisé en ce que l'électronique de test (12) est alimentée en énergie par le tube lanceur au travers des moyens récepteurs d'énergie (9).
- Dispositif de test suivant la revendication 1, caractérisé en ce que l'électronique de test (12) comporte au moins une capacité (15) qui est chargée en énergie par le lanceur, capacité assurant l'alimentation électrique du dispositif de test.
- Dispositif de test suivant une des revendications 1 ou 2, caractérisé en ce que l'électronique de test (12) comporte au moins une première voie de mesure (16) permettant de vérifier que l'intensité du courant reçu du tube lanceur lors de la mise à feu est supérieure à une intensité minimale (Im) pendant une durée minimale (Tm).
- Dispositif de test suivant une des revendications 1 à 3, caractérisé en ce que l'électronique de test (12) comporte au moins une deuxième voie de mesure (17) 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 (iM).
- Dispositif de test suivant une des revendications 3 ou 4, caractérisé en ce que l'électronique de test (12) comprend un commutateur électronique de puissance (18) permettant de commuter le courant fourni par les moyens (9) récepteurs d'énergie électrique vers l'une ou l'autre des voies de mesure (16,17).
- Dispositif de test suivant la revendication 5, caractérisé en ce que le temps de fermeture du commutateur de puissance (18) est au moins égal à la durée minimale (Tm).
- Dispositif de test suivant une des revendications 5 ou 6, caractérisé en ce qu'il comporte un commutateur manuel (10) porté par le corps du dispositif et permettant de sélectionner l'une ou l'autre des voies de mesures (16,17).
- Dispositif de test selon une des revendications 1 à 7, caractérisé en ce que le résultat des mesures est donné par un afficheur (11a,11b) solidaire du corps.
- Dispositif de test selon une des revendications 3 à 8, caractérisé en ce qu'il comporte un séquenceur (19) assurant le séquencement des opérations de commutation, de mesure et d'affichage du résultat de la mesure.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9604115 | 1996-04-02 | ||
FR9604115A FR2746911B1 (fr) | 1996-04-02 | 1996-04-02 | Dispositif de test de fonctionnement d'un lanceur de munitions |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0800053A1 EP0800053A1 (fr) | 1997-10-08 |
EP0800053B1 true EP0800053B1 (fr) | 2001-11-07 |
Family
ID=9490815
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97400518A Expired - Lifetime EP0800053B1 (fr) | 1996-04-02 | 1997-03-07 | Dispositif de test de fonctionnement d'un lanceur de munitions |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0800053B1 (fr) |
AT (1) | ATE208487T1 (fr) |
DE (1) | DE69707953T2 (fr) |
FR (1) | FR2746911B1 (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2758161C1 (ru) * | 2021-03-22 | 2021-10-26 | Федеральное государственное бюджетное образовательное учреждение высшего образования «Амурский государственный университет» | Универсальный имитатор транспортно-пускового контейнера для поведения вибродинамических испытаний спутников стандарта CubeSat |
RU211274U1 (ru) * | 2021-12-29 | 2022-05-30 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Амурский государственный университет" | Имитатор транспортно-пускового контейнера для поведения вибродинамических испытаний спутников стандарта CubeSat 1U-3U |
Families Citing this family (14)
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CA2831189A1 (fr) | 2011-03-29 | 2012-10-04 | Dynaenergetics Gmbh & Co. Kg | Emballage pour charges creuses |
RU2519615C1 (ru) * | 2013-02-12 | 2014-06-20 | Сергей Михайлович Мужичек | Способ определения характеристик осколочного поля боеприпаса и устройство для его осуществления |
RU2519608C1 (ru) * | 2013-02-13 | 2014-06-20 | Сергей Михайлович Мужичек | Способ определения характеристик осколочного поля боеприпаса и устройство для его осуществления |
RU2519618C1 (ru) * | 2013-02-19 | 2014-06-20 | Сергей Михайлович Мужичек | Способ определения характеристик осколочного поля боеприпаса и устройство для его осуществления |
RU2519611C1 (ru) * | 2013-02-26 | 2014-06-20 | Сергей Михайлович Мужичек | Способ определения характеристик осколочного поля боеприпасов и устройство для его осуществления |
RU2519617C1 (ru) * | 2013-03-12 | 2014-06-20 | Сергей Михайлович Мужичек | Способ определения характеристик осколочного поля боеприпасов и устройство для его осуществления |
RU2518678C1 (ru) * | 2013-03-26 | 2014-06-10 | Сергей Михайлович Мужичек | Способ определения характеристик осколочного поля боеприпасов и устройство для его осуществления |
RU2521932C1 (ru) * | 2013-04-05 | 2014-07-10 | Сергей Михайлович Мужичек | Способ определения пробивного действия осколков боеприпасов и устройство для его осуществления |
RU2521460C1 (ru) * | 2013-04-18 | 2014-06-27 | Сергей Михайлович Мужичек | Способ определения зажигательной способности боеприпаса дистанционного действия и устройство для его осуществления |
CN103357137A (zh) * | 2013-07-25 | 2013-10-23 | 成都陵川特种工业有限责任公司 | 用于检测灭火发射器的装置 |
CN103357138A (zh) * | 2013-07-25 | 2013-10-23 | 成都陵川特种工业有限责任公司 | 一种灭火发射器的检测座 |
CN110749253B (zh) * | 2019-10-24 | 2021-11-30 | 中国人民解放军32181部队 | 导弹测试系统用导弹性能测试单元 |
DE102021107186A1 (de) | 2021-03-23 | 2022-09-29 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Wurfkörpernachbildung |
CN116379846B (zh) * | 2023-06-06 | 2023-09-05 | 北京星河动力装备科技有限公司 | 火箭的飞行时序验证设备以及系统 |
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 (de) * | 1989-12-08 | 1991-06-13 | Rheinmetall Gmbh | Waffenrohr fuer guetepruef- und abnahmebeschuesse einer granate |
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/fr not_active Expired - Fee Related
-
1997
- 1997-03-07 EP EP97400518A patent/EP0800053B1/fr not_active Expired - Lifetime
- 1997-03-07 DE DE69707953T patent/DE69707953T2/de not_active Expired - Fee Related
- 1997-03-07 AT AT97400518T patent/ATE208487T1/de not_active IP Right Cessation
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2758161C1 (ru) * | 2021-03-22 | 2021-10-26 | Федеральное государственное бюджетное образовательное учреждение высшего образования «Амурский государственный университет» | Универсальный имитатор транспортно-пускового контейнера для поведения вибродинамических испытаний спутников стандарта CubeSat |
RU211274U1 (ru) * | 2021-12-29 | 2022-05-30 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Амурский государственный университет" | Имитатор транспортно-пускового контейнера для поведения вибродинамических испытаний спутников стандарта CubeSat 1U-3U |
Also Published As
Publication number | Publication date |
---|---|
DE69707953T2 (de) | 2002-05-29 |
ATE208487T1 (de) | 2001-11-15 |
FR2746911B1 (fr) | 1998-05-22 |
EP0800053A1 (fr) | 1997-10-08 |
DE69707953D1 (de) | 2001-12-13 |
FR2746911A1 (fr) | 1997-10-03 |
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