GB822645A - Improvements in or relating to devices for regulating the fuel flow delivered to supersonic ram jets - Google Patents

Improvements in or relating to devices for regulating the fuel flow delivered to supersonic ram jets

Info

Publication number
GB822645A
GB822645A GB30180/56A GB3018056A GB822645A GB 822645 A GB822645 A GB 822645A GB 30180/56 A GB30180/56 A GB 30180/56A GB 3018056 A GB3018056 A GB 3018056A GB 822645 A GB822645 A GB 822645A
Authority
GB
United Kingdom
Prior art keywords
fuel
supply
missile
aircraft
oct
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
GB30180/56A
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.)
Sud Aviation Societe Nationale de Constructions Aerdnaettiques
Original Assignee
Sud Aviation Societe Nationale de Constructions Aerdnaettiques
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 Sud Aviation Societe Nationale de Constructions Aerdnaettiques filed Critical Sud Aviation Societe Nationale de Constructions Aerdnaettiques
Publication of GB822645A publication Critical patent/GB822645A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

822,645. Jet propulsion plant. SUD-AVIATION SOC. NATIONALE DE CONSTRUCTIONS AERONAUTIQUES. Oct. 3, 1956 [Oct. 12, 1955], No. 30180/56. Class 110 (3). [Also in Groups XII and XXXV] In Fig. 1 the supply to a pilot fuel injection manifold 60 and main fuel injection manifolds 61, 62 of an aircraft or missile ram jet engine 1 is regulated by a rotary sleeve valve 9 driven by an electric servomotor 91 under the control (see Group XXXV) of Mach meters 14 and 17 responsive to internal and external airflow respectively. The aircraft or missile is launched by auxiliary means and the fuel supply is initiated soon after launching by raising fuel pressure to burst a diaphragm (not shown). Fuel is then supplied to manifolds 60, 61 and somewhat later to manifold 62. Regulation of by-pass fuel instead of the main fuel supply is referred to. Specification 810,843, [Group XII], is referred to.
GB30180/56A 1955-10-12 1956-10-03 Improvements in or relating to devices for regulating the fuel flow delivered to supersonic ram jets Expired GB822645A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR822645X 1955-10-12

Publications (1)

Publication Number Publication Date
GB822645A true GB822645A (en) 1959-10-28

Family

ID=9281006

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30180/56A Expired GB822645A (en) 1955-10-12 1956-10-03 Improvements in or relating to devices for regulating the fuel flow delivered to supersonic ram jets

Country Status (1)

Country Link
GB (1) GB822645A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3067577A (en) * 1960-01-25 1962-12-11 North American Aviation Inc Method and control system for sensing temperatured differentials of flowing gases

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3067577A (en) * 1960-01-25 1962-12-11 North American Aviation Inc Method and control system for sensing temperatured differentials of flowing gases

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