EP2090859A3 - Launcher with at least one start tube for rocket-propelled missiles - Google Patents

Launcher with at least one start tube for rocket-propelled missiles Download PDF

Info

Publication number
EP2090859A3
EP2090859A3 EP20090002082 EP09002082A EP2090859A3 EP 2090859 A3 EP2090859 A3 EP 2090859A3 EP 20090002082 EP20090002082 EP 20090002082 EP 09002082 A EP09002082 A EP 09002082A EP 2090859 A3 EP2090859 A3 EP 2090859A3
Authority
EP
European Patent Office
Prior art keywords
gas generator
launcher
rocket
pipe
serving
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
EP20090002082
Other languages
German (de)
French (fr)
Other versions
EP2090859A2 (en
EP2090859B1 (en
Inventor
Thomas Klaffert
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.)
MBDA Deutschland GmbH
Original Assignee
MBDA Deutschland GmbH
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 MBDA Deutschland GmbH filed Critical MBDA Deutschland GmbH
Publication of EP2090859A2 publication Critical patent/EP2090859A2/en
Publication of EP2090859A3 publication Critical patent/EP2090859A3/en
Application granted granted Critical
Publication of EP2090859B1 publication Critical patent/EP2090859B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/0413Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A1/00Missile propulsion characterised by the use of explosive or combustible propellant charges
    • F41A1/08Recoilless guns, i.e. guns having propulsion means producing no recoil
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A25/00Gun mountings permitting recoil or return to battery, e.g. gun cradles; Barrel buffers or brakes
    • F41A25/06Friction-operated systems
    • 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
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/042Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

Werfer mit mindestens einem Startrohr (12) für raketenbetriebene Flugkörper, die ihre Startbeschleunigung und einen Anfangsdrall mittels eines im axial gefesselten Startrohr (12) befindlichen Gasgenerator (15)(Booster) erhalten, mit einer am abgewandtem Ende des Startrohres (12) dem Austritt des Gasvolumenstromes des Gasgenerators dienenden Lavaldüse (13) mit nachgeordneter Lavaldüsen-Anordnung (30) und mit einem dem Gasgenerator zugeordneten der Rückstoßkompensation des Startrohres (12) dienenden gestellfesten Schockabsorbers (17) aus zwei koaxialen Führungshülsen (18, 19), von denen die eine (18) gestellfest und die zweite, relativ dazu beweglich gelagert ist, zwischen denen ein Rücklaufweg und -zeit bestimmende Reibungs-Ringfeder (20)sich befindet.

Figure imgaf001
Launcher with at least one launch tube (12) for rocket - propelled missiles, which receive their start acceleration and an initial twist by means of a gas generator (15) (booster) located in the axially bounded start pipe (12), with one at the opposite end of the start pipe (12) the exit of the Gas volume flow of the gas generator serving Laval nozzle (13) with downstream Laval nozzle arrangement (30) and with a gas generator associated the recoil compensation of the starting pipe (12) serving frame-fixed shock absorber (17) of two coaxial guide sleeves (18, 19), of which the one ( 18) fixed to the frame and the second, is movably mounted relative thereto, between which a return path and time-determining friction ring spring (20) is located.
Figure imgaf001

EP09002082.7A 2008-02-18 2009-02-14 Launcher with at least one start tube for rocket-propelled missiles Active EP2090859B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200810009638 DE102008009638B3 (en) 2008-02-18 2008-02-18 Launcher with at least one launch tube for rocket-propelled missiles

Publications (3)

Publication Number Publication Date
EP2090859A2 EP2090859A2 (en) 2009-08-19
EP2090859A3 true EP2090859A3 (en) 2013-05-29
EP2090859B1 EP2090859B1 (en) 2015-06-03

Family

ID=40578863

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09002082.7A Active EP2090859B1 (en) 2008-02-18 2009-02-14 Launcher with at least one start tube for rocket-propelled missiles

Country Status (2)

Country Link
EP (1) EP2090859B1 (en)
DE (1) DE102008009638B3 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010006493B4 (en) * 2010-02-02 2012-04-26 Diehl Bgt Defence Gmbh & Co. Kg Container for a jet-propelled missile
CN112644801A (en) * 2020-09-21 2021-04-13 中山市哈工朗德智能科技有限公司 Novel horizontal sealing guide device
CN116006360B (en) * 2022-12-03 2024-04-09 中国科学院力学研究所 Special-shaped Laval micro-spray pipe

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE695584C (en) * 1933-11-05 1940-08-28 Mauser Werke Ag Machine gun with movable barrel
DE716385C (en) * 1939-03-04 1942-01-19 Mauser Werke Ag Friction ring spring with enlarged work destruction, especially for the weapon industry
DE1428637C1 (en) * 1964-02-26 1975-02-20 Messerschmitt Boelkow Blohm Tubular launcher for projectiles, especially for missiles
US4106389A (en) * 1976-05-14 1978-08-15 British Aircraft Corporation Aircraft weapon mountings
GB2121149A (en) * 1982-05-27 1983-12-14 British Aerospace Missile housing and launch arrangement

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH450228A (en) * 1965-10-22 1968-01-15 Transurvey Holding Company Inc Device for launching a projectile
US6352030B1 (en) * 1998-11-12 2002-03-05 Cordant Technologies Inc. Gas generating eject motor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE695584C (en) * 1933-11-05 1940-08-28 Mauser Werke Ag Machine gun with movable barrel
DE716385C (en) * 1939-03-04 1942-01-19 Mauser Werke Ag Friction ring spring with enlarged work destruction, especially for the weapon industry
DE1428637C1 (en) * 1964-02-26 1975-02-20 Messerschmitt Boelkow Blohm Tubular launcher for projectiles, especially for missiles
US4106389A (en) * 1976-05-14 1978-08-15 British Aircraft Corporation Aircraft weapon mountings
GB2121149A (en) * 1982-05-27 1983-12-14 British Aerospace Missile housing and launch arrangement

Also Published As

Publication number Publication date
EP2090859A2 (en) 2009-08-19
DE102008009638B3 (en) 2009-09-03
EP2090859B1 (en) 2015-06-03

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