EP2141444B1 - Câble électrique, étanche au gaz dans un projectile - Google Patents
Câble électrique, étanche au gaz dans un projectile Download PDFInfo
- Publication number
- EP2141444B1 EP2141444B1 EP09006364.5A EP09006364A EP2141444B1 EP 2141444 B1 EP2141444 B1 EP 2141444B1 EP 09006364 A EP09006364 A EP 09006364A EP 2141444 B1 EP2141444 B1 EP 2141444B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- basic body
- projectile
- signal line
- connection
- bore
- 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.)
- Active
Links
- 239000012777 electrically insulating material Substances 0.000 claims description 6
- 238000000034 method Methods 0.000 claims description 6
- 239000004020 conductor Substances 0.000 claims description 4
- 239000000853 adhesive Substances 0.000 claims description 3
- 230000001070 adhesive effect Effects 0.000 claims description 3
- 239000011248 coating agent Substances 0.000 claims description 3
- 238000000576 coating method Methods 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 3
- 229910000838 Al alloy Inorganic materials 0.000 claims description 2
- 229910052782 aluminium Inorganic materials 0.000 claims description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims description 2
- 239000000463 material Substances 0.000 claims description 2
- 239000004411 aluminium Substances 0.000 claims 1
- 239000003380 propellant Substances 0.000 description 15
- 239000007789 gas Substances 0.000 description 4
- 238000007743 anodising Methods 0.000 description 3
- 239000010410 layer Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 239000002360 explosive Substances 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 239000012790 adhesive layer Substances 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000010292 electrical insulation Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 239000000700 radioactive tracer Substances 0.000 description 1
- 230000008054 signal transmission Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
- F42C19/06—Electric contact parts specially adapted for use with electric fuzes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
Definitions
- the invention relates to a projectile with a propellant charge igniter and an electrical, gastight bushing, which is an electrically conductive connection in a rear part of the projectile, and a method for implementing this implementation.
- Projectiles with a settable detonator typically include an isolated electrical signal line and a grounded line (hereinafter also referred to as a ground line) for programming the ignition timing of the detonator.
- the signal line and the ground line are passed axially in known Leittechnikstabilinstrumentes floors in the area of the projectile tail in the form of a cable containing both lines through this.
- the interface between the high-pressure and high-temperature hot room and the inside of the projectile receiver eg an igniter
- complex components since no gas may penetrate into the projectile.
- complex gas-tight bushings must be provided in the tail boom for the corresponding cable.
- the WO 00/17598 A2 discloses a plasma generating device by which a drive system can be electrothermally-chemically ignited. Also the US 5,830,377 A deals with such a plasma injection device (ETC).
- ETC plasma injection device
- a rocket device which indicates a safe power implementation in the rocket.
- a rear end of the missile head of the missile is integrated with a combustible sleeve with a metal bottom in which the ignition mechanism with the time-limiting function is located.
- the signal transmission is via ring-shaped signal electrodes on the front surface of the device, which are electrically connected to signal cable terminals of the metal bottom.
- the invention is based on the object, a simple, gas-tight implementation of mentioned type to be implemented, which preferably implements a galvanic electrical line in a floor.
- the invention is based essentially on the idea to realize the electrical, gas-tight implementation by an insulated outer body and a metallic, electrically conductive inner conductor. It is provided that a base body is formed by a rear part of a projectile and this function of the ground / signal line takes over. The metallic main body forms the ground line and only the signal line is isolated within the body passed through a corresponding bore of the body, the signal line should fill the bore substantially.
- the main body is preferably machined and is provided on all sides, including within all holes to be insulated and over all threads, with a non-conductive coating.
- the insulation of the signal line is not by means of an insulating jacket, which is wound around the cable, but by the prior to introduction of the signal line into the bore on the base body applied coating of an electrically insulating material.
- the ends of the signal line are provided with terminal contacts, which are preferably at least partially screwed into the body and isolated from the main body are fixed to this.
- the front and back of the body are provided with coating-free holes.
- the threaded portions of the terminal contacts preferably before screwing into the recesses of the Main body, wetted with an electrically insulating liquid adhesive.
- connection contacts for connection to the electrical conductor with axially arranged bores into which the ends of the conductor can be inserted.
- an aluminum alloy is used as the material for the base body, preferably anodising may be used as the electrically insulating material.
- the basic body according to the invention is therefore particularly suitable for providing a gas-tight transmission of electrical signals and can be used in a projectile-stabilized projectile, for example. It is only necessary with such projectiles to introduce an axially continuous bore for the signal line and preferably provided with threads areas for the connection contacts in the tail boom before the known per se application of an anodizing the Leittechnikitati and the inner walls of the bore and the areas for the Co-mount terminal contacts with anodising. Then then the holes for the connections of the ground line can be introduced into the tail boom.
- the rear-side terminal contact on its side facing away from the base body has an axially extending blind hole into which the end of a with the propellant charge connected plug contact, for example, against the pressure of a located in the blind hole return spring is inserted.
- a mass conductive throw can be provided, which can intervene on the one hand in the coating-free bore of the front of the body, if such is present, and on the other hand, for example via a grinding system, the ground line of the propellant charge contacted.
- the propellant charge igniter can in principle be connected to the projectile by means of threads, bolts, springs, fits or the like and thereby a contacting of the conduits It is important that the lighter is connected directly to the floor of the building. The thus resulting interface provides a secure contact between bullet tail and propellant charge.
- the advantage of this design is therefore also that the propellant charge igniter is connected directly to the rear of the bullet and thus something like an interface for secure contact between bullet tail and propellant charge igniter results.
- the propellant lighter can be screwed from the rear, causing a simplification of the laboratory of a cartridge.
- the construction is fireproof because the attachment components are accelerated by the large areas to the rear so as to enforce gas tightness. In addition to good EMC resistance, it has easy mounting.
- Fig. 1 1 is a projectile, here a large-caliber wing-stabilized sabot projectile, which comprises a projectile body 3 filled with an explosive 2 and a segmentable sabot 4.
- the projectile body 3 comprises on the front side a tempable detonator 5 and has on the rear side an existing example of an aluminum base body 6, here the rear part of the projectile 1, which carries the tail 7 of the sabot projectile 1.
- the heatable igniter 5 is connected via an electrical connection 8 (in Fig. 1 indicated as a dashed line) connected to a rear side arranged first terminal contact 9.
- a plug contact 11 can be introduced, for example, in cartridged ammunition ( Fig. 4 ), which is connected via extending within a propellant charge igniter 10 electrical lines with on the sleeve bottom (not shown) of the corresponding ammunition arranged electrodes.
- second terminal contact 12 is first in the main body 6 a the front 13 and the back 14 of the base 6 connecting Bore 15 for the signal line 16 of the electrical connection 8 and for receiving the connection contacts 9, 12 for the electrical connection 8 in the front and back 13, 14 corresponding, provided with female threads receiving areas 17, 18 introduced ( Fig. 2 ).
- coating-free blind holes 20, 21 are introduced into the base body 6 ( Fig. 3 ), so that the main body 6 can be contacted later with the subsequent ground lines of the adjacent components (propellant charge, bow-sided projectile part) and the base body 6 itself forms the ground line 22 for a coaxially extending signal line 16.
- connection contacts 9, 12 are then inserted into the bore 15 and the connection contacts 9, 12 provided with corresponding external threads are screwed into the receiving regions 17, 18, so that the two ends 23, 24 of the signal line 16 are inserted into corresponding recesses 25, 26 of the connection contacts 9, 12 are inserted and the connection contacts 9, 12 are electrically connected to each other via the signal line 16.
- the terminal contacts 9, 12 preferably with a liquid adhesive (for example Kleiberit) wetted.
- a liquid adhesive for example Kleiberit
- the first terminal 9 on its side facing away from the base 6 an axially extending blind hole 100, in which the end of a with the Propellant charge igniter (not shown in detail) connectable plug contact 11 is inserted ( Fig. 4 ).
- a mass conductive cap 27 is provided which can intervene in the presence of a coating-free blind hole 20 of the front side 13 of the body 6.
- the first terminal contact 9 two or more eccentrically arranged recesses 30, for example, for receiving tracer sets on.
- the invention can be applied to all floors, which are, for example tempered and must have an electrical, gas-tight implementation or should.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Elimination Of Static Electricity (AREA)
- Air Bags (AREA)
- Structure Of Receivers (AREA)
Claims (10)
- Projectile (1) comprenant un allumeur de charge propulsive (10) et une ligne de transit électrique hermétique aux gaz de signaux électriques d'une zone à haute pression vers une zone à basse pression présentant un corps de base (6), composé d'un corps externe isolé et d'un conducteur interne métallique électriquement conducteur, le corps de base métallique formant la ligne de masse et seule la ligne de signal à l'intérieur du corps de base passant à travers un alésage correspondant du corps de base en étant isolée, et la ligne de signal devant essentiellement remplir l'alésage, le corps de base (6) étant formé par la partie arrière, l'allumeur de charge propulsive (10) étant relié directement avec la partie arrière (6) du projectile (1) au moyen d'un filet, d'un boulon, de ressorts ou d'ajustements ou similaires, de sorte que celui-ci est monté par l'arrière sur la partie arrière (6) et une mise en contact directe est réalisée entre l'allumeur de charge propulsive (10) et la partie arrière (6).
- Projectile (1) selon la revendication 1, caractérisé en ce que la partie intérieure conduisant le signal est une partie qui s'étend dans le sens axial.
- Projectile (1) selon la revendication 2, caractérisé en ce qu'une ligne de signal (16) passe le long de l'axe central à travers le corps de base (6) faisant office de ligne de masse.
- Projectile (1) selon l'une des revendications 1 à 3, caractérisé en ce qu'un premier contact de raccordement (9) de la ligne de signal (16) sur un côté à l'opposé du corps de base (6) présente un alésage à fond plein (100) qui s'étend dans le sens axial, dans lequel peut être insérée l'extrémité d'un contact mâle (11) qui peut être relié avec l'allumeur de charge propulsive.
- Projectile (1) selon l'une des revendications 1 à 4, caractérisé en ce que la partie arrière (6) est de forme conique.
- Procédé de fabrication d'une ligne de transit électrique hermétique aux gaz pour un projectile selon l'une des revendications 1 à 5, possédant les caractéristiques suivantes :a) dans le corps de base (6) sont aménagés un alésage (15) qui relie le côté avant (13) et le côté arrière (14) du corps de base (6) ainsi que des zones d'accueil (17, 18) correspondantes dans les côtés avant et arrière (13,14) destinées à accueillir des contacts de raccordement (9, 12) pour la liaison (8) électriquement conductrice ;b) l'ensemble du corps de base (6) est ensuite recouvert d'un matériau (19) électriquement isolant ;c) pour établir le contact avec le corps de base (6) utilisé en tant que ligne de masse (22), des alésages à fond plein (20, 21) dépourvus de revêtement sont aménagés dans celui-ci depuis le côté avant (13) et/ou le côté arrière (14) ;d) une ligne de signal (16) électriquement conductrice qui remplit pour l'essentiel l'alésage (15) est insérée dans l'alésage (15) et ensuite reliée électriquement avec les contacts de raccordement (9, 12) introduits dans les zones d'accueil (17, 18).
- Procédé selon la revendication 6, caractérisé en ce que les zones d'accueil (17, 18), avant le revêtement du corps de base (6) avec le matériau (19) électriquement isolant, sont respectivement munies d'un filet femelle dans lequel sont vissés les contacts de raccordement (9, 12) munis d'un filet mâle correspondant.
- Procédé selon la revendication 6 ou 7, caractérisé en ce que les zones filetées des contacts de raccordement (9, 12) sont enduites d'un agent adhésif liquide électriquement isolant avant le vissage dans les zones d'accueil (17, 18) du corps de base (6).
- Procédé selon l'une des revendications 6 à 8, caractérisé en ce que les contacts de raccordement (9, 12), pour la liaison avec la ligne de signal (16), sont munis d'évïdements (25, 26) disposés dans le sens axial, dans lesquels peuvent être introduites les extrémités (23, 24) de la ligne de signal (16).
- Procédé selon l'une des revendications 6 à 9, caractérisé en ce que le matériau utilisé pour le corps de base (6) est un alliage d'aluminium et de l'anodisation est utilisée comme matériau électriquement isolant.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102008030663A DE102008030663A1 (de) | 2008-07-01 | 2008-07-01 | Elektrische, gasdichte Durchführung sowie Verwendung in einem Geschoss |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2141444A2 EP2141444A2 (fr) | 2010-01-06 |
EP2141444A3 EP2141444A3 (fr) | 2013-06-05 |
EP2141444B1 true EP2141444B1 (fr) | 2014-08-06 |
Family
ID=40707749
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09006364.5A Active EP2141444B1 (fr) | 2008-07-01 | 2009-05-12 | Câble électrique, étanche au gaz dans un projectile |
Country Status (4)
Country | Link |
---|---|
US (1) | US8336458B2 (fr) |
EP (1) | EP2141444B1 (fr) |
DE (1) | DE102008030663A1 (fr) |
ES (1) | ES2514519T3 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008030663A1 (de) * | 2008-07-01 | 2010-01-07 | Rheinmetall Waffe Munition Gmbh | Elektrische, gasdichte Durchführung sowie Verwendung in einem Geschoss |
DE102013013602A1 (de) * | 2013-08-19 | 2015-02-19 | Trützschler GmbH + Co KG Textilmaschinenfabrik | Vorrichtung an einer Karde oder Krempel für Baumwolle, Chemiefasern u. dgl. mit einer drehbaren Abstreifwalze |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE526010A (fr) * | 1953-01-27 | |||
US4015531A (en) * | 1975-01-31 | 1977-04-05 | General Electric Company | Electrical fuze with selectable modes of operation |
US5353710A (en) * | 1991-02-11 | 1994-10-11 | Giat Industries | Container fitted with electrical connecting means |
FR2672674B1 (fr) * | 1991-02-11 | 1995-01-13 | Giat Ind Sa | Conteneur muni de moyens de liaison electrique. |
US5485787A (en) * | 1994-06-21 | 1996-01-23 | Rockwell International Corporation | Gas gun launched scramjet test projectile |
US5830377A (en) * | 1997-06-04 | 1998-11-03 | United Defense, Lp | Method and apparatus for providing a stabilized plasma arc |
US6119599A (en) * | 1998-08-19 | 2000-09-19 | United Defense, L.P. | Sequential arc surface injector |
JP3660991B2 (ja) * | 2002-06-24 | 2005-06-15 | 防衛庁技術研究本部長 | 時限起爆機構への信号伝達可能な可燃性薬包付き飛しょう体装置 |
DE102008030663A1 (de) * | 2008-07-01 | 2010-01-07 | Rheinmetall Waffe Munition Gmbh | Elektrische, gasdichte Durchführung sowie Verwendung in einem Geschoss |
-
2008
- 2008-07-01 DE DE102008030663A patent/DE102008030663A1/de not_active Withdrawn
-
2009
- 2009-05-12 EP EP09006364.5A patent/EP2141444B1/fr active Active
- 2009-05-12 ES ES09006364.5T patent/ES2514519T3/es active Active
- 2009-07-01 US US12/495,912 patent/US8336458B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US8336458B2 (en) | 2012-12-25 |
US20100132579A1 (en) | 2010-06-03 |
EP2141444A3 (fr) | 2013-06-05 |
ES2514519T3 (es) | 2014-10-28 |
EP2141444A2 (fr) | 2010-01-06 |
DE102008030663A1 (de) | 2010-01-07 |
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