EP2707279B1 - Schiff mit mindestens einem schaft zur aufnahme von mindestens einem raketenabschussbehälter - Google Patents

Schiff mit mindestens einem schaft zur aufnahme von mindestens einem raketenabschussbehälter Download PDF

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Publication number
EP2707279B1
EP2707279B1 EP12719722.6A EP12719722A EP2707279B1 EP 2707279 B1 EP2707279 B1 EP 2707279B1 EP 12719722 A EP12719722 A EP 12719722A EP 2707279 B1 EP2707279 B1 EP 2707279B1
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EP
European Patent Office
Prior art keywords
container
vessel according
strip
vessel
damping
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
Application number
EP12719722.6A
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English (en)
French (fr)
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EP2707279A1 (de
Inventor
Dominique Monteil
Didier SEGUINOT
Marie Anne ARMBRUST
Hervé Bruneau
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Naval Group SA
Original Assignee
DCNS SA
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Application filed by DCNS SA filed Critical DCNS SA
Priority to PL12719722T priority Critical patent/PL2707279T3/pl
Publication of EP2707279A1 publication Critical patent/EP2707279A1/de
Application granted granted Critical
Publication of EP2707279B1 publication Critical patent/EP2707279B1/de
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G3/00—Arrangements of ammunition stores or handlers; Vessels characterised thereby
    • B63G3/04—Arrangements of ammunition stores or handlers; Vessels characterised thereby for missiles

Definitions

  • the present invention relates to a vessel comprising at least one receiving well of at least one missile launching container.
  • vessels equipped with such containers for example chosen from the range of containers known under the trademark SYLVER® from the applicant, are already known.
  • the or each launching container is received in one or more corresponding wells of the ship so that their upper part is flush with the deck of the ship and their lower part is fixed rigidly to the bottom of the well and thus to the structure of the ship.
  • Such a support comprises a U-shaped support element of resilient material, one of whose branches is attached to the supporting structure such as the ship and the other branch supports the device or material, the two branches being stiffened. by a spacer extending between them, formed by a fracturable rod in a plane substantially parallel to the branches of the U and connected to the two branches, the connection with at least one of said branches being provided by a second fracturable element in the direction of the stem.
  • the object of the invention is therefore to solve the problems mentioned above.
  • the subject of the invention is a ship of the type comprising at least one missile launching container and at least one receiving well thereof, characterized in that the launching container is received with an axial and lateral displacement.
  • controlled in the well in that the side wall of this container is provided with its upper part, means for centering / guiding in the well and in that its lower end comprises a container-carrying sole associated with a support plate of the ship through damping means with a shock filter threshold comprising at least one minus a damper assembly with metal turns associated with break-off bars mounted under prestressing between the two flanges.
  • the container and the well have vertical axes, the upper part of the container flush for example the deck of the vessel and being provided with a closure door designated by the general reference 4, retractable when firing. of a missile.
  • these missiles are for example received in the container 1 with their cells or protective caps, one of which is for example designated by the general reference 5.
  • the launch container 1 is received with a controlled axial and lateral displacement in the well and the side wall of this container is provided, in its upper part, with centering / guiding means in the well, formed for example by abutments of damping material, one of which is visible in these figures and designated by the general reference 6.
  • abutments in damping material are then for example disposed between the container and the corresponding wall of the well to center and guide for example the upper part of this container in the well.
  • the container In its lower part the container is associated and rests on damping means designated by the general reference 7 on the figure 1 , having a sole Container carrier designated by the general reference 8 associated with a bearing plate of the ship designated by the general reference 9, through damping means with shock filtration threshold designated by the general reference 10.
  • damping means will be described in more detail on the figures 4 , 5 and 6 .
  • damping means comprise at least one damping assembly with metal turns and in the illustrated example at least two damping assemblies with metal turns, arranged symmetrically on either side of the container and designated by the general references 11 and 12 in these figures.
  • the coil damping assemblies are, for example, in the form of at least one helical spring member disposed in an extended position between the soles and whose opposite edges are engaged in holes for the passage of the corresponding connecting ties of the soles.
  • the crosspieces 13, 14, 15 and 16 illustrated in these figures such as for example the crosspieces 13, 14, 15 and 16 illustrated in these figures.
  • damping means also comprise break-off bars mounted under prestressing between the two flanges of which two respectively 17 and 18 are illustrated in these figures.
  • This rupture bar then comprises two bar portions respectively 19 and 20 connected by a breakable pin 21 and each end of which is associated with a sole.
  • each bar has a male bar portion designated by the general reference 20, one end of which is adapted to engage in a clevis 22 of one end of a corresponding female bar portion 19, the breakable pin 21 extending transversely in the yoke 22 of the female bar portion 19 and through the male bar portion 20.
  • each bar 18 is threaded and is engaged in a through hole 23, 24 respectively of a fastening tab 25, 26 on the corresponding sole 8, 9 and cooperates with a corresponding nut 27, 28 to allow the fitting under prestressing of this bar between the soles.
  • each bar is threaded and each of these is adapted to be engaged in a hole of a fixing lug and to cooperate with a corresponding nut.
  • each nut has a spherical bearing surface 29 and 30, respectively, adapted to cooperate with a complementary bearing surface of the corresponding tab 25, 26.
  • the threshold damping means may comprise several bars with associated break point.
  • At least two strips with associated breaking threshold and mounted head to tail between the flanges can be envisaged.
  • the damping means may comprise two sets of two bars arranged symmetrically on either side of the container.
  • the container has a rectangular section and two metal coil damping assemblies are arranged symmetrically on two sides thereof, while two sets of two bars are arranged symmetrically on the other two sides. of it.
  • Such a structure makes it possible, for example, from an input shock of 30 g vertically or 15 g transversely, to absorb shock energy to obtain a maximum of 10 g on the onboard munition, with a loading ammunition variable from 1 to 4 ammunition that is to say an evolution of the ammunition mass from 150 to 600 kilos, a loading of asymmetric ammunition or taking into account the effort related to the departure of a missile (35 KN dissymmetrical to the launcher) knowing that under normal conditions of use (missile firing, platform movements, etc ...), the axes of the launching cells must respect a position fidelity of the order 1.5 mrad.
  • the launcher Under normal conditions of use, the launcher retains its stiffness characteristics to meet the missile alignment requirements and in the event of shocks related for example to underwater explosions, the shocks are triggered at the calibration values.
  • the bars are mounted with a prestressing at the damping means.
  • the bars are in extension and resist the forces generated by the crashing of the dampers.
  • shock absorbers then take over to filter the accelerations and preserve the ammunition.
  • This principle makes it possible to halve the accelerations of the vertical shock, ie 15 g.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Vibration Dampers (AREA)

Claims (14)

  1. Schiff vom Typ, der mindestens einen Behälter (1) für den Abschuss von Flugkörpern und mindestens einen Schacht (2) zur Aufnahme desselben aufweist, dadurch gekennzeichnet, dass der Abschussbehälter (1) mit einer axial und lateral gesteuerten Auslenkung in dem Schacht (2) aufgenommen ist, dass die Seitenwand dieses Behälters (1) in ihrem oberen Bereich mit Mitteln (6) zur Zentrierung/Führung in dem Schacht (2) ausgerüstet ist, und dass sein unteres Ende eine Behälterträgerplatte (8) aufweist, die einer Abstützplatte (2) des Schiffs (3) über Mittel (10) zur Stoßdämpfung mit einer Schwelle zur Filtration von Stößen zugeordnet ist, die mindestens eine Metallwindungen aufweisende Dämpferanordnung (11, 12) umfassen, die Stäben (17, 18) mit Bruchschwelle zugeordnet ist, die mit Vorspannung zwischen den zwei Platten (8, 9) montiert sind.
  2. Schiff nach Anspruch 1, dadurch gekennzeichnet, dass der Schacht (2) und der Behälter (1) vertikale Achsen aufweisen.
  3. Schiff nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass die Mittel zur Führung/Zentrierung Anschläge (6) aus dämpfendem Material (6) umfassen.
  4. Schiff nach einem beliebigen der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Dämpfungsmittel (10) mindestens zwei Metallwindungen aufweisende Dämpfungsanordnungen (11, 12) umfassen, die beidseitig des Behälters (1) symmetrisch angeordnet sind.
  5. Schiff nach einem beliebigen der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Metallwindungen in Form mindestens eines Spiralfederelements (11, 12) ausgebildet sind, das in langgezogener Position zwischen den Platten (8, 9) angeordnet ist und dessen gegenüberliegende Ränder mit Durchgangsöffnungen von korrespondierenden Verbindungstraversen (13, 14, 15, 16) der Platten (8, 9) in Eingriff sind.
  6. Schiff nach einem beliebigen der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass jeder Bruchstab (17, 18) zwei Stabteile (19, 20) aufweist, die durch einen brechbaren Stift (21) verbunden sind und von denen jedes Ende einer Platte (8, 9) zugeordnet ist.
  7. Schiff nach Anspruch 6, dadurch gekennzeichnet, dass die Stabteile ein Einsteckstabteil (20) aufweisen, dessen eines Ende angepasst ist, in einen Kopf (22) eines Endes eines korrespondierenden Aufnahmestabteils (19) einzugreifen und dass der brechbare Stift (21) sich quer in dem Kopf (22) des Aufnahmestabteils (19) und dem Einsteckstabteil (20) erstreckt.
  8. Schiff nach einem beliebigen der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass mindestens ein Ende jedes Bruchstabs (17, 18) mit einem Gewinde versehen ist und ein Durchgangsloch (23, 24) eines Befestigungsansatzes (25, 26) an der korrespondierenden Platte (8, 9) durchgreift und mit einer korrespondierenden Mutter (27, 28) zusammenarbeitet, um die Montage des Stabs (17, 18) unter Vorspannung zwischen den Platten zu gestatten.
  9. Schiff nach Anspruch 8, dadurch gekennzeichnet, dass die zwei Enden jedes Stabes (17, 18) mit einem Gewinde versehen sind, und dass jedes dieser Gewinde angepasst ist, ein Loch (23, 24) eines Befestigungsansatzes (25, 26) zu durchgreifen und mit einer korrespondierenden Mutter (27, 28) zusammenzuarbeiten.
  10. Schiff nach Anspruch 8 oder 9, dadurch gekennzeichnet, dass jede Mutter (27, 28) eine kugelförmige Auflagefläche (29, 30) aufweist, die ausgebildet ist, mit einer komplementären Stützfläche des korrespondierenden Ansatzes (25, 26) zusammenzuarbeiten.
  11. Schiff nach einem beliebigen der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Dämpfungsmittel mit Schwelle mindestens zwei zugeordnete Stäbe (17, 18) mit Bruchschwelle umfassen, die entgegengesetzt liegend zwischen den Platten (8, 9) montiert sind.
  12. Schiff nach einem beliebigen der vorhergehenden Ansprüche, dadurch gekennzeichnet, dass die Stäbe (17, 18) mit Bruchschwelle in Richtung der Achse des Behälters geneigt sind.
  13. Schiff nach Anspruch 11 oder 12, dadurch gekennzeichnet, dass die Dämpfungsmittel (10) mit Schwelle mindestens zwei Sätze von mindestens zwei Stäben (17, 18) aufweisen, die beidseitig des Behälters (11) symmetrisch angeordnet sind.
  14. Schiff nach Anspruch 13, dadurch gekennzeichnet, dass der Behälter (1) einen rechteckigen Querschnitt aufweist, und dass die zwei Metallwindungen aufweisenden Dämpfungsanordnungen (11, 12) symmetrisch an zwei Seiten desselben angeordnet sind, während die zwei Sätze von zwei Stäben (17, 18) symmetrisch an den zwei anderen Seiten desselben angeordnet sind.
EP12719722.6A 2011-05-11 2012-05-09 Schiff mit mindestens einem schaft zur aufnahme von mindestens einem raketenabschussbehälter Active EP2707279B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL12719722T PL2707279T3 (pl) 2011-05-11 2012-05-09 Okręt zawierający co najmniej jeden szyb mieszczący co najmniej jeden kontener wyrzutni rakietowej

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1154061A FR2975074B1 (fr) 2011-05-11 2011-05-11 Navire du type comportant au moins un puits de reception d'au moins un conteneur de lancement de missile
PCT/EP2012/058529 WO2012152826A1 (fr) 2011-05-11 2012-05-09 Navire du type comportant au moins un puits de réception d'au moins un conteneur de lancement de missile

Publications (2)

Publication Number Publication Date
EP2707279A1 EP2707279A1 (de) 2014-03-19
EP2707279B1 true EP2707279B1 (de) 2017-10-04

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EP12719722.6A Active EP2707279B1 (de) 2011-05-11 2012-05-09 Schiff mit mindestens einem schaft zur aufnahme von mindestens einem raketenabschussbehälter

Country Status (8)

Country Link
US (1) US9200868B2 (de)
EP (1) EP2707279B1 (de)
ES (1) ES2646715T3 (de)
FR (1) FR2975074B1 (de)
NO (1) NO2707279T3 (de)
PL (1) PL2707279T3 (de)
PT (1) PT2707279T (de)
WO (1) WO2012152826A1 (de)

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EP2889877B1 (de) * 2013-12-06 2021-03-10 ITT Manufacturing Enterprises LLC Anordnung zur seismischen Isolation
US20150345900A1 (en) * 2014-05-28 2015-12-03 Chief Of Naval Research, Office Of Counsel Missile Launcher System
US20170307045A1 (en) 2014-09-24 2017-10-26 Itt Manufacturing Enterprises Llc Damping and support device for electrical equipments
JP6787643B2 (ja) * 2015-08-21 2020-11-18 Thk株式会社 上下免震装置
ITUB20161198A1 (it) * 2016-03-01 2017-09-01 Cometto Ind Veicolo per il supporto, il trasporto ed il comando di un carico balistico
CN109996417B (zh) * 2019-02-20 2023-10-20 和信精密科技（吴江）有限公司 一种可拆式server
WO2021126031A1 (en) * 2019-12-19 2021-06-24 Saab Ab A suspension assembly for supporting a vibration sensitive device

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Also Published As

Publication number Publication date
EP2707279A1 (de) 2014-03-19
FR2975074B1 (fr) 2013-06-21
FR2975074A1 (fr) 2012-11-16
PL2707279T3 (pl) 2018-03-30
WO2012152826A1 (fr) 2012-11-15
NO2707279T3 (de) 2018-03-03
US9200868B2 (en) 2015-12-01
US20140060296A1 (en) 2014-03-06
ES2646715T3 (es) 2017-12-15
PT2707279T (pt) 2017-12-14

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