EP2107331A1 - Torpedoabschussvorrichtung - Google Patents

Torpedoabschussvorrichtung Download PDF

Info

Publication number
EP2107331A1
EP2107331A1 EP08425224A EP08425224A EP2107331A1 EP 2107331 A1 EP2107331 A1 EP 2107331A1 EP 08425224 A EP08425224 A EP 08425224A EP 08425224 A EP08425224 A EP 08425224A EP 2107331 A1 EP2107331 A1 EP 2107331A1
Authority
EP
European Patent Office
Prior art keywords
torpedo
bag
launch
launch tube
thrust disk
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP08425224A
Other languages
English (en)
French (fr)
Other versions
EP2107331B1 (de
Inventor
Giorgio Giusti
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.)
Whitehead Sistemi Subacquei SpA
Original Assignee
Whitehead Alenia Sistemi Subacquei SpA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Whitehead Alenia Sistemi Subacquei SpA filed Critical Whitehead Alenia Sistemi Subacquei SpA
Priority to EP20080425224 priority Critical patent/EP2107331B1/de
Publication of EP2107331A1 publication Critical patent/EP2107331A1/de
Application granted granted Critical
Publication of EP2107331B1 publication Critical patent/EP2107331B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/08Rocket or torpedo launchers for marine torpedoes
    • F41F3/10Rocket or torpedo launchers for marine torpedoes from below the surface of the water

Definitions

  • the present invention relates to a torpedo launch device, in particular for launching torpedoes from a surface vessel.
  • Pneumatic torpedo launch devices which substantially comprise a launch tube, into which the torpedo is inserted; and a system for feeding compressed air into the rear of the launch tube to fire the torpedo.
  • the compressed air is contained in a highpressure cylinder.
  • compressed air must be made available on the launcher; maintaining the given compressed-air pressure may pose problems; and, finally, the pneumatic system calls for routine maintenance.
  • Number 1 in Figure 1 indicates as a whole a launch device for launching a torpedo 2.
  • Launch device 1 comprises a substantially cylindrical launch tube 3 having a front muzzle end 3a and a rear end 3b; and a expulsion assembly 4 housed inside launch tube 3, close to rear end 3b.
  • torpedo 2 is fitted at the rear with a shank 9 with a spherical end 9a.
  • Expulsion assembly 4 comprises a base disk 5 connected to rear end 3b of launch tube 3; a thrust disk 8 connectable releasably to shank 9 of torpedo 2 housed inside launch tube 3; and an explosive-actuated bag 7 interposed axially between base disk 5 and thrust disk 8.
  • Base disk 5 is preferably connected to rear end 3b of launch tube 3 by a fast-fit, e.g. bayonet, connecting device not shown.
  • Bag 7 is substantially cylindrical, and has a rear base wall 11 secured to base disk 5 by fast-fit, e.g. bayonet, connecting means not shown. At rest, as shown in Figure 1 , bag 7 is folded accordion-fashion and lashed in place by a calibrated-release binding not shown.
  • fast-fit e.g. bayonet
  • Bag 7 is fitted with and inflated by an explosive gas generator 10.
  • Bag 7 also comprises a relief valve 12 and a safety valve 13 housed in respective seats in base disk 5 to communicate with the outside of launch tube 3.
  • Thrust disk 8 is connected releasably to torpedo shank 9 by a lock device 14 shown in Figures 2 and 3 .
  • Lock device 14 substantially comprises a gripper 16 having a central body 18 housed in axially sliding manner inside a central cavity 17 of thrust disk 8, and to which are hinged two substantially L-shaped jaws 19, which cooperate with shank 9 of torpedo 2 and are held in the closed position gripping the shank by the walls of cavity 17.
  • Central body 18 has an axial push-rod 22 which cooperates with spherical end 9a of shank 9 of torpedo 2; and central body 18 is connected, by an actuating rod 20 fitted through thrust disk 8, to a pressure sensor plate 21 facing bag 7.
  • a first spring 48, externally coaxial with actuating rod 20, is compressed between plate 21 and thrust disk 8; and a second spring 49, externally coaxial with push-rod 22, is compressed between central body 18 and jaws 19 (when closed) of gripper 16, so as to push the jaws into the open position.
  • Lock device 14 also comprises a number of stop assemblies 24 housed in respective radial holes 23 formed in, and communicating with central cavity 17 of, thrust disk 8.
  • Each stop assembly 24 substantially comprises a rod 25 which interacts with central body 18 of gripper 16; and a push-rod 26 connected telescopically to rod 25, and which clicks inside a respective seat 27 in launch tube 3 to axially lock thrust disk 8.
  • rod 25 comprises a tubular portion 28 (partly removed in Figure 2 ) housing in sliding manner one end of push-rod 26 forming a plate 29.
  • Push-rod 26 is subjected to the action of two counteracting springs 30, 31 : spring 30 is compressed axially between rod 25 and plate 29 of push-rod 26 to push push-rod 26 outwards, i.e. towards the wall of launch tube 3, and rod 25 inwards, i.e. towards cavity 17; and spring 31 is compressed between an inner shoulder of hole 23 and plate 29 to hold push-rod 26 in the withdrawn position inside hole 23.
  • Rods 25 of stop assemblies 24 and central body 18 of gripper 16 have respective bevels 34, 35, which interact with one another, when central body 18 is inserted inside cavity 17, to push rods 25 outwards.
  • Thrust disk 8 and torpedo 2 are guided inside launch tube 3 by a number of inner longitudinal guides 40, 41 inside the tube ( Figure 4 ). More specifically, launch tube 3 has four grooves 40 spaced 90° apart and engaged in sliding manner by respective fins 42 on torpedo 2, and by respective guide fins 44 on thrust disk 8; and four grooves 41 spaced 45° from grooves 40 and engaged in sliding manner by respective outer radial projections 45 on thrust disk 8 ( Figure 5 ).
  • grooves 41 dead-end on the side facing end 3a of tube 3; and shock-absorbing stop devices 46 are provided at the end of grooves 41 to arrest thrust disk 8.
  • a bayonet system (not shown) conveniently permits extraction of thrust disk 8 from end 3a of launch tube 3.
  • Launch device 1 operates as follows.
  • torpedo 2 is configured for launching from the tube by fitting on interface shank 9.
  • Thrust disk 8 is then fixed onto shank 9 of torpedo 2 by means of lock device 14.
  • lock device 14 is shown in the deactivated position.
  • shank 9 pushes push-rod 22 of central body 18 axially to back up central body 18 inside cavity 17; jaws 19 close onto shank 9 by interaction with the walls of cavity 17; and bevels 34, 35 push stop assemblies 24 outwards.
  • Torpedo 2 and thrust disk 8 as a whole are then inserted inside launch tube 3 through rear end 3b, and are locked inside the tube by the ends of push-rods 26 clicking inside respective seats 27.
  • Base disk 5 already fitted with bag 7, is fitted inside rear end 3b of launch tube 3, as shown in Figure 1 .
  • launch tube 3 is ready for launching.
  • gas generator 10 is activated by a control signal.
  • Push-rods 26 are thus withdrawn by springs 31 to release thrust disk 8 from launch tube 3.
  • thrust disk 8 advances to expel torpedo 2 from launch tube 3, and comes to rest against shock-absorbing stop devices 46 at the end of launch tube 3.
  • launch device 1 is restored by :

Landscapes

  • Engineering & Computer Science (AREA)
  • Ocean & Marine Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Furnace Charging Or Discharging (AREA)
EP20080425224 2008-04-03 2008-04-03 Torpedoabschussvorrichtung Active EP2107331B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP20080425224 EP2107331B1 (de) 2008-04-03 2008-04-03 Torpedoabschussvorrichtung

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP20080425224 EP2107331B1 (de) 2008-04-03 2008-04-03 Torpedoabschussvorrichtung

Publications (2)

Publication Number Publication Date
EP2107331A1 true EP2107331A1 (de) 2009-10-07
EP2107331B1 EP2107331B1 (de) 2013-07-31

Family

ID=39776401

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20080425224 Active EP2107331B1 (de) 2008-04-03 2008-04-03 Torpedoabschussvorrichtung

Country Status (1)

Country Link
EP (1) EP2107331B1 (de)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2530423A1 (de) 2011-05-31 2012-12-05 Dcns Abschusssystem eines Unterwassergeräts
EP2657126A3 (de) * 2012-04-24 2013-12-18 ThyssenKrupp Marine Systems GmbH Unterseeboot
EP2476993A3 (de) * 2011-01-12 2015-04-22 ThyssenKrupp Marine Systems GmbH Waffenkupplung zum Festlegen einer Waffe in einer Waffen-Transport- und Staueinrichtung
WO2017021135A1 (de) * 2015-08-05 2017-02-09 Thyssenkrupp Marine Systems Gmbh Fernbedienbare waffenkupplung
WO2017144646A1 (fr) * 2016-02-25 2017-08-31 Dcns Structure de tube lance-arme et notamment de tube lance-torpille
DE102017212689A1 (de) * 2017-07-24 2018-07-05 Thyssenkrupp Ag Unterwasserstauvorrichtung
WO2020126502A1 (de) * 2018-12-20 2020-06-25 Atlas Elektronik Gmbh Vorrichtung und verfahren zum starten eines unterwasser-laufkörpers von einem wasserfahrzeug aus
CN113104177A (zh) * 2021-05-12 2021-07-13 南京佳乐船舶设备有限公司 信号弹发射装置以及应用于此发射装置的信号弹
US11946717B1 (en) * 2022-09-21 2024-04-02 The United States Of America As Represented By The Secretary Of The Navy Pressurized gas launcher

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110626525A (zh) * 2019-06-25 2019-12-31 北京机械设备研究所 一种适用于空间运行设备的释放装置及释放方法
CN112357025A (zh) * 2020-11-09 2021-02-12 西北工业大学 一种适用于不同口径水下航行器的发射管

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2462267A1 (de) * 1974-11-19 1977-03-03 Mak Maschinenbau Gmbh Ausstossvorrichtung fuer torpedos
US4944210A (en) * 1988-08-08 1990-07-31 Hughes Aircraft Company Missile launcher
WO2001092095A1 (en) * 2000-05-31 2001-12-06 Systems, Engineering Associates Corporation Improved torpedo launch mechanism and method
US20040031381A1 (en) * 2002-08-19 2004-02-19 Williams Michael W. Apparatus for launching an object in a fluid environment

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2462267A1 (de) * 1974-11-19 1977-03-03 Mak Maschinenbau Gmbh Ausstossvorrichtung fuer torpedos
US4944210A (en) * 1988-08-08 1990-07-31 Hughes Aircraft Company Missile launcher
WO2001092095A1 (en) * 2000-05-31 2001-12-06 Systems, Engineering Associates Corporation Improved torpedo launch mechanism and method
US20040031381A1 (en) * 2002-08-19 2004-02-19 Williams Michael W. Apparatus for launching an object in a fluid environment

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2476993A3 (de) * 2011-01-12 2015-04-22 ThyssenKrupp Marine Systems GmbH Waffenkupplung zum Festlegen einer Waffe in einer Waffen-Transport- und Staueinrichtung
EP2476993B1 (de) * 2011-01-12 2019-03-06 ThyssenKrupp Marine Systems GmbH Waffenkupplung zum Festlegen einer Waffe in einer Waffen-Transport- und Staueinrichtung
EP2530423A1 (de) 2011-05-31 2012-12-05 Dcns Abschusssystem eines Unterwassergeräts
EP2657126A3 (de) * 2012-04-24 2013-12-18 ThyssenKrupp Marine Systems GmbH Unterseeboot
DE102015214959A1 (de) * 2015-08-05 2017-02-09 Thyssenkrupp Ag Fernbedienbare Waffenkupplung
WO2017021135A1 (de) * 2015-08-05 2017-02-09 Thyssenkrupp Marine Systems Gmbh Fernbedienbare waffenkupplung
WO2017144646A1 (fr) * 2016-02-25 2017-08-31 Dcns Structure de tube lance-arme et notamment de tube lance-torpille
FR3048281A1 (fr) * 2016-02-25 2017-09-01 Dcns Structure de tube lance-arme et notamment de tube lance-torpille
US20190339041A1 (en) * 2016-02-25 2019-11-07 Naval Group Weapon tube and particularly torpedo tube structure
US11226172B2 (en) 2016-02-25 2022-01-18 Naval Group Weapon tube and particularly torpedo tube structure
DE102017212689A1 (de) * 2017-07-24 2018-07-05 Thyssenkrupp Ag Unterwasserstauvorrichtung
DE102017212689B4 (de) 2017-07-24 2020-06-18 Thyssenkrupp Ag Unterwasserstauvorrichtung
WO2020126502A1 (de) * 2018-12-20 2020-06-25 Atlas Elektronik Gmbh Vorrichtung und verfahren zum starten eines unterwasser-laufkörpers von einem wasserfahrzeug aus
DE102018222490A1 (de) * 2018-12-20 2020-06-25 Atlas Elektronik Gmbh Vorrichtung und Verfahren zum Starten eines Unterwasser-Laufkörpers von einem Wasserfahrzeug aus
US12017741B2 (en) 2018-12-20 2024-06-25 Atlas Elektronik Gmbh Device and method for launching an underwater projectile from a watercraft
CN113104177A (zh) * 2021-05-12 2021-07-13 南京佳乐船舶设备有限公司 信号弹发射装置以及应用于此发射装置的信号弹
US11946717B1 (en) * 2022-09-21 2024-04-02 The United States Of America As Represented By The Secretary Of The Navy Pressurized gas launcher

Also Published As

Publication number Publication date
EP2107331B1 (de) 2013-07-31

Similar Documents

Publication Publication Date Title
EP2107331A1 (de) Torpedoabschussvorrichtung
CA2493118C (en) Apparatus for delivering and deployment of an expandable stent within a blood vessel
CN102809325B (zh) 玩具枪用压缩空气射击弹壳
EP0499332A1 (de) Druckgaspatrone
US10036617B2 (en) Inflator with high flow rate
CN106064675A (zh) 用于撤离滑梯的软套释放机制
EP3505447B1 (de) Trennanordnung für eine luftlieferungsvorrichtung
US20140260945A1 (en) Grooved firearm chamber
ES2706698T3 (es) Sistema de extracción de granadas
CN107023706B (zh) 机械启动的充气阀致动设备
EP1647482A1 (de) Nutzlastauswurfsystem
EP1902938B1 (de) Schwimmer für ein in das Meer abgeworfene, luftfahrzeuggestützte Vorrichtung, insbesondere für eine Gegenmaßnahme
US4291809A (en) Pencil holder
US2594627A (en) Jet-propelled device
KR20160028746A (ko) 잠수함의 무장 발사 장치 및 방법
EP0070275B1 (de) Auswerfervorrichtung für ausrüstungen
JP7120522B2 (ja) 圧電素子によりトリガーされた蓄積エネルギーの開放
EP2746717B1 (de) Vorrichtung für Schnell-entkupplung von lasttragenden Strukturen
US5125319A (en) Transport safety system in a rocket launcher
EP3286522B1 (de) Projektil und gefechtskopf und abschusssystem dafür
US7182013B1 (en) Umbilical retraction assembly and method
US20230288169A1 (en) Projectile launcher
US9909837B2 (en) Rocket extraction device and method
EP2107335A1 (de) Torpedorückgewinnungsvorrichtung
EP2022716B1 (de) Vorrichtung zur Auslösung eines Gegenmassnahmeapparates

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

RTI1 Title (correction)

Free format text: TORPEDO LAUNCH DEVICE

17P Request for examination filed

Effective date: 20100407

AKX Designation fees paid

Designated state(s): DE FR GB IT

17Q First examination report despatched

Effective date: 20100614

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: WHITEHEAD SISTEMI SUBACQUEI S.P.A.

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602008026382

Country of ref document: DE

Effective date: 20130926

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20140502

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602008026382

Country of ref document: DE

Effective date: 20140502

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 9

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20230406

Year of fee payment: 16

Ref country code: FR

Payment date: 20230421

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20240423

Year of fee payment: 17

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20240429

Year of fee payment: 17