GB1028465A - Method of deflecting a hot gas jet passing through a nozzle for carrying out the method - Google Patents

Method of deflecting a hot gas jet passing through a nozzle for carrying out the method

Info

Publication number
GB1028465A
GB1028465A GB519163A GB519163A GB1028465A GB 1028465 A GB1028465 A GB 1028465A GB 519163 A GB519163 A GB 519163A GB 519163 A GB519163 A GB 519163A GB 1028465 A GB1028465 A GB 1028465A
Authority
GB
United Kingdom
Prior art keywords
nozzle
liquid
injected
injection
insert
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
Application number
GB519163A
Other languages
English (en)
Inventor
Jean Henrl Bertin
Cyrille Francois Pavlin
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.)
Bertin Technologies SAS
Original Assignee
Bertin et Cie SA
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
Priority claimed from FR887391A external-priority patent/FR1322872A/fr
Priority claimed from FR921523A external-priority patent/FR82940E/fr
Application filed by Bertin et Cie SA filed Critical Bertin et Cie SA
Publication of GB1028465A publication Critical patent/GB1028465A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/668—Injection of a fluid, e.g. a propellant, into the gas shear in a nozzle or in the boundary layer at the outer surface of a missile, e.g. to create a shock wave in a supersonic flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Nozzles (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
GB519163A 1962-02-08 1963-02-08 Method of deflecting a hot gas jet passing through a nozzle for carrying out the method Expired GB1028465A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR887391A FR1322872A (fr) 1962-02-08 1962-02-08 Procédé et dispositif de déviation du jet d'une fusée
FR921523A FR82940E (fr) 1963-01-15 1963-01-15 Procédé et dispositif de déviation du jet d'une fusée

Publications (1)

Publication Number Publication Date
GB1028465A true GB1028465A (en) 1966-05-04

Family

ID=26194288

Family Applications (1)

Application Number Title Priority Date Filing Date
GB519163A Expired GB1028465A (en) 1962-02-08 1963-02-08 Method of deflecting a hot gas jet passing through a nozzle for carrying out the method

Country Status (2)

Country Link
DE (1) DE1240747C2 (enExample)
GB (1) GB1028465A (enExample)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1158156A3 (en) * 2000-05-26 2003-10-29 General Electric Company Fluidic nozzle control system
GB2398046A (en) * 2003-01-15 2004-08-11 S & C Thermofluids Ltd Porous nozzle arrangement
GB2428413A (en) * 2005-02-24 2007-01-31 Rolls Royce Plc Fluid vectoring nozzle
US7658337B2 (en) 2005-02-24 2010-02-09 Rolls-Royce Plc Fluid vectoring nozzle
CN104712460A (zh) * 2015-01-14 2015-06-17 北京理工大学 一种推力可控的固体火箭发动机
US11629669B1 (en) * 2019-05-31 2023-04-18 Exquadrum, Inc. Liquid monopropellant controlled solid rocket motor with aft end injection deflector

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2922576C2 (de) * 1979-06-02 1982-02-18 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Strahltriebwerk mit Schubvektorsteuerung

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2916873A (en) * 1958-10-22 1959-12-15 Advanced Res Associates Inc Jet deflecting apparatus

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1158156A3 (en) * 2000-05-26 2003-10-29 General Electric Company Fluidic nozzle control system
GB2398046A (en) * 2003-01-15 2004-08-11 S & C Thermofluids Ltd Porous nozzle arrangement
GB2398046B (en) * 2003-01-15 2006-07-12 S & C Thermofluids Ltd The use of porous surfaces with coanda effect
GB2428413A (en) * 2005-02-24 2007-01-31 Rolls Royce Plc Fluid vectoring nozzle
GB2428413B (en) * 2005-02-24 2008-02-20 Rolls Royce Plc Fluid vectoring nozzle
US7658337B2 (en) 2005-02-24 2010-02-09 Rolls-Royce Plc Fluid vectoring nozzle
EP1696116A3 (en) * 2005-02-24 2012-12-12 Rolls-Royce plc Thrust vectoring using fluid jets
CN104712460A (zh) * 2015-01-14 2015-06-17 北京理工大学 一种推力可控的固体火箭发动机
US11629669B1 (en) * 2019-05-31 2023-04-18 Exquadrum, Inc. Liquid monopropellant controlled solid rocket motor with aft end injection deflector

Also Published As

Publication number Publication date
DE1240747C2 (de) 1975-07-10
DE1240747B (enExample) 1975-07-10

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