ES2054016T3 - Manorregulador de choque. - Google Patents

Manorregulador de choque.

Info

Publication number
ES2054016T3
ES2054016T3 ES89309222T ES89309222T ES2054016T3 ES 2054016 T3 ES2054016 T3 ES 2054016T3 ES 89309222 T ES89309222 T ES 89309222T ES 89309222 T ES89309222 T ES 89309222T ES 2054016 T3 ES2054016 T3 ES 2054016T3
Authority
ES
Spain
Prior art keywords
projectile
gauges
shock
nozzle
chamber
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
Application number
ES89309222T
Other languages
English (en)
Inventor
Lee D Miller
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Application granted granted Critical
Publication of ES2054016T3 publication Critical patent/ES2054016T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F41A21/00Barrels; Gun tubes; Muzzle attachments; Barrel mounting means
    • F41A21/28Gas-expansion chambers; Barrels provided with gas-relieving ports
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Toys (AREA)
  • Vending Machines For Individual Products (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Circuit Arrangements For Discharge Lamps (AREA)
  • Pens And Brushes (AREA)
  • Devices For Indicating Variable Information By Combining Individual Elements (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Valve Device For Special Equipments (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

APARATO PARA LANZAMIENTO DE UN PROYECTIL QUE TIENE UNA TOBERA PARA EMISION DEL GAS DURANTE EL LANZAMIENTO, DICHO APARATO QUE COMPRENDE EL INSTRUMENTO PARA SOPORTE DE UN PROYECTIL Y UN CAMARA QUE TIENE UN ORIFICIO SITUADO PARA RECIBIR PARTE O TODA EL CHORRO DE LA TOBERA DEL PROYECTILEN EL SE CONFIGURA LA CAMARA PARA QUE LA PRESION SE DESARROLLE EN ELLA PARA PROPORSIONAR UN IMPULSO ADICIONAL AL PROYECTIL DURANTE EL LANZAMIENTO.
ES89309222T 1988-10-27 1989-09-12 Manorregulador de choque. Expired - Lifetime ES2054016T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB888825195A GB8825195D0 (en) 1988-10-27 1988-10-27 Impingement pressure regulator

Publications (1)

Publication Number Publication Date
ES2054016T3 true ES2054016T3 (es) 1994-08-01

Family

ID=10645894

Family Applications (1)

Application Number Title Priority Date Filing Date
ES89309222T Expired - Lifetime ES2054016T3 (es) 1988-10-27 1989-09-12 Manorregulador de choque.

Country Status (8)

Country Link
US (1) US5012718A (es)
EP (1) EP0366247B1 (es)
AT (1) ATE106545T1 (es)
DE (1) DE68915687T2 (es)
DK (1) DK172767B1 (es)
ES (1) ES2054016T3 (es)
GB (1) GB8825195D0 (es)
NO (1) NO179650C (es)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2668254B1 (fr) * 1990-10-18 1993-07-23 France Etat Armement Dispositif de fermeture et de protection d'un systeme d'evacuation de gaz d'un module de lancement vertical.
US7040212B1 (en) * 1996-08-09 2006-05-09 Mbda Uk Limited Launching missiles
US6079310A (en) * 1996-12-05 2000-06-27 The United States Of America As Represented By The Secretary Of The Navy Portable launcher
US5837919A (en) * 1996-12-05 1998-11-17 The United States Of America As Represented By The Secretary Of The Navy Portable launcher
US6283005B1 (en) 1998-07-29 2001-09-04 The United States Of America As Represented By The Secretary Of The Navy Integral ship-weapon module
US6318229B1 (en) * 1999-11-22 2001-11-20 Joel P. Nevels System for boosting velocity of a rocket
US6971300B2 (en) * 2003-11-25 2005-12-06 The United States Of America As Represented By The Secretary Of The Navy Reloadable concentric canister launcher
KR100629930B1 (ko) * 2004-07-30 2006-09-29 국방과학연구소 유도탄 사출 발사 장치
US8468923B2 (en) * 2007-02-16 2013-06-25 Lockheed Martin Corporation Apparatus and method for selectively affecting a launch trajectory of a projectile
US8353239B1 (en) * 2008-05-29 2013-01-15 Lockheed Martin Corporation Apparatus and method for directing the launch of a projectile
US8960067B2 (en) * 2012-01-12 2015-02-24 Lockheed Martin Corporation Method and apparatus for launch recoil abatement
KR101536991B1 (ko) * 2013-09-23 2015-07-15 국방과학연구소 화염 역류 방지판을 가진 발사관
KR101478120B1 (ko) * 2013-10-25 2014-12-31 국방과학연구소 부가 추력 조절이 가능한 능동형 추력 부가 장치
KR101405261B1 (ko) * 2014-02-24 2014-06-10 국방과학연구소 화염 역류 방지 발사관
US11041692B1 (en) * 2020-05-12 2021-06-22 Michael Chromych System and method for launching and acceleration of objects

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4185538A (en) * 1960-08-30 1980-01-29 The United States Of America As Represented By The Secretary Of The Navy Simplified air system for underwater rocket launching
US3279319A (en) * 1964-06-19 1966-10-18 Joseph W Semonian Floatable rocket launcher
US3298278A (en) * 1965-04-15 1967-01-17 Edward J Barakauskas Standpipe for underwater launching system
US4203347A (en) * 1978-04-10 1980-05-20 The Boeing Company Shock suppressing apparatus and method for a rocket launcher
US4186647A (en) * 1978-08-09 1980-02-05 General Dynamics Corporation, Pomona Division Multiple area rear launch tube cover
US4436016A (en) * 1981-08-11 1984-03-13 Westinghouse Electric Corp. Variable energy missile eject system
US4426909A (en) * 1981-10-20 1984-01-24 The Boeing Company Noise, flash and smoke suppressor apparatus and method for rocket launcher
US4686884A (en) * 1985-12-27 1987-08-18 General Dynamics, Pomona Division Gas management deflector
US4683798A (en) * 1985-12-27 1987-08-04 General Dynamics, Pomona Division Gas management transition device
US4796510A (en) * 1987-11-09 1989-01-10 General Dynamics, Pomona Division Rocket exhaust recirculation obturator for missile launch tube

Also Published As

Publication number Publication date
EP0366247A3 (en) 1991-07-31
GB8825195D0 (en) 1989-04-19
NO894297L (no) 1990-04-30
DK172767B1 (da) 1999-07-05
DE68915687T2 (de) 1994-09-15
ATE106545T1 (de) 1994-06-15
US5012718A (en) 1991-05-07
NO894297D0 (no) 1989-10-27
DK529589A (da) 1990-04-28
DK529589D0 (da) 1989-10-25
NO179650B (no) 1996-08-12
NO179650C (no) 1996-11-20
EP0366247A2 (en) 1990-05-02
DE68915687D1 (de) 1994-07-07
EP0366247B1 (en) 1994-06-01

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