IL74354A - Temperature sensitive ducted rocket motor fuel nozzle and method for thrust regulation - Google Patents

Temperature sensitive ducted rocket motor fuel nozzle and method for thrust regulation

Info

Publication number
IL74354A
IL74354A IL74354A IL7435485A IL74354A IL 74354 A IL74354 A IL 74354A IL 74354 A IL74354 A IL 74354A IL 7435485 A IL7435485 A IL 7435485A IL 74354 A IL74354 A IL 74354A
Authority
IL
Israel
Prior art keywords
fuel nozzle
temperature sensitive
rocket motor
motor fuel
ducted rocket
Prior art date
Application number
IL74354A
Other languages
English (en)
Original Assignee
Hercules Inc
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 Hercules Inc filed Critical Hercules Inc
Publication of IL74354A publication Critical patent/IL74354A/xx

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
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • F02K9/58—Propellant feed valves
    • 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
    • F02K9/805—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control servo-mechanisms or control devices therefor
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/1842—Ambient condition change responsive
    • Y10T137/1939—Atmospheric
    • Y10T137/1963—Temperature
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7737—Thermal responsive

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Temperature-Responsive Valves (AREA)
  • Diaphragms And Bellows (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Testing Of Engines (AREA)
  • Jet Pumps And Other Pumps (AREA)
IL74354A 1984-02-16 1985-02-15 Temperature sensitive ducted rocket motor fuel nozzle and method for thrust regulation IL74354A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/580,580 US4574586A (en) 1984-02-16 1984-02-16 Self compensating ducted rocket motor fuel nozzle and method for regulating fuel generation

Publications (1)

Publication Number Publication Date
IL74354A true IL74354A (en) 1991-06-10

Family

ID=24321672

Family Applications (1)

Application Number Title Priority Date Filing Date
IL74354A IL74354A (en) 1984-02-16 1985-02-15 Temperature sensitive ducted rocket motor fuel nozzle and method for thrust regulation

Country Status (6)

Country Link
US (1) US4574586A (xx)
EP (1) EP0153153B1 (xx)
JP (1) JPS60243353A (xx)
DE (1) DE3562288D1 (xx)
IL (1) IL74354A (xx)
NO (1) NO850606L (xx)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4821510A (en) * 1987-04-22 1989-04-18 Morton Thiokol, Inc. Multiple-stage rocket motor nozzle throat
US5817968A (en) * 1987-08-03 1998-10-06 The United States Of America As Represented By The Secretary Of The Air Force Gas generation with high pressure sensitivity exponent propellant
CA1304335C (en) * 1987-10-22 1992-06-30 Charles F. Stearns Metering valve temperature compensation
US5172547A (en) * 1991-04-30 1992-12-22 The United States Of America As Represented By The Secretary Of The Air Force Electronic valve control for gas generator outflow
US5341639A (en) * 1993-01-19 1994-08-30 The United States Of America As Represented By The Secretary Of The Army Fullerene rocket fuels
US6895991B2 (en) * 2002-08-09 2005-05-24 Honeywell International, Inc. Missile thrust system and valve with refractory piston cylinder
US6837479B2 (en) * 2002-08-26 2005-01-04 Honeywell International Inc. Fluid drain assembly
WO2007008766A1 (en) * 2005-07-08 2007-01-18 Cdm Optics, Inc. Ray correction apparatus and method
US7600737B2 (en) * 2007-04-13 2009-10-13 Honeywell International Inc. Cutback poppet valve
RU2484281C1 (ru) * 2011-11-09 2013-06-10 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Регулятор расхода твердого топлива
KR101305256B1 (ko) * 2012-12-18 2013-09-06 포항공과대학교 산학협력단 초고속 균일 나노 입자 생성 노즐, 생성 장치 및 생성 방법
US10081091B2 (en) * 2015-06-12 2018-09-25 Postech Academy-Industry Foundation Nozzle, device, and method for high-speed generation of uniform nanoparticles

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2990119A (en) * 1961-06-27 willson
US1231164A (en) * 1913-02-24 1917-06-26 William H Jahns Valve-lock.
US2379124A (en) * 1943-07-15 1945-06-26 Milwaukee Gas Specialty Co Thermal expansion responsive control
US2573522A (en) * 1947-09-08 1951-10-30 Gen Motors Corp Valve with vibration damper
US2829492A (en) * 1955-02-28 1958-04-08 Reaction Motors Inc Temperature compensated regulator for fluid supply lines
US2968919A (en) * 1957-03-25 1961-01-24 Hughes Aircraft Co Variable area nozzle
BE609711A (xx) * 1960-10-29
DE1189819B (de) * 1962-06-26 1965-03-25 Danfoss As Thermostatisches Ventil fuer eine Warmwasser-Heizungsanlage
US3332237A (en) * 1964-10-27 1967-07-25 Fiego Louis Lo Mechanical valve
FR1558482A (xx) * 1967-12-22 1969-02-28
US3648967A (en) * 1970-11-10 1972-03-14 Physics Int Co Temperature compensated hydraulic valve
FR2147500A5 (xx) * 1971-07-29 1973-03-09 Denisselle Jean
SE7713106L (sv) * 1977-11-21 1979-05-22 Tour & Andersson Ab Anordning for temperaturreglering av radiatorer och samrorsanleggningar
DE2828249C2 (de) * 1978-06-28 1982-05-19 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum Steuern oder Regeln der Durchflußmenge von Heißgas in einem Strömungskanal, insbesondere von brennstoffreichen Gasen für die Brennkammer von Raketentriebwerken
US4355663A (en) * 1980-03-11 1982-10-26 Hercules Incorporated Nozzle/valve device for a ducted rocket motor
DE3101560C2 (de) * 1981-01-20 1986-06-19 Afriso-Euro-Index GmbH, 7129 Güglingen Temperaturgesteuertes Sicherheitsventil
US4444006A (en) * 1981-02-04 1984-04-24 Hercules Incorporated Nozzle/valve device for a ducted rocket motor
US4442669A (en) * 1981-02-12 1984-04-17 Hercules Incorporated Nozzle/valve device for a ducted rocket motor

Also Published As

Publication number Publication date
EP0153153A1 (en) 1985-08-28
JPH0534508B2 (xx) 1993-05-24
JPS60243353A (ja) 1985-12-03
DE3562288D1 (en) 1988-05-26
EP0153153B1 (en) 1988-04-20
NO850606L (no) 1985-08-19
US4574586A (en) 1986-03-11

Similar Documents

Publication Publication Date Title
DE3170269D1 (en) Thrust reverser for an aircraft jet engine
EP0152019A3 (en) Method for controlling fuel injection for engine
GB2182724B (en) Gas turbine engine thrust reverser
GB2055333B (en) Vectorable thrust nozzle
GB2230240B (en) Thrust vectoring nozzle
EP0286572A3 (en) Thrust vectoring exhaust nozzle arrangement
JPS5759029A (en) Position-lock detector for thrust reverser of turbo jet engine
IL74354A (en) Temperature sensitive ducted rocket motor fuel nozzle and method for thrust regulation
GB2183030B (en) An in-flight engine control optical pyrometer
DE3368753D1 (en) Thermal oxidizer and method for operating same
DE3566014D1 (en) Thermally actuated rocket motor safety system
GB8811126D0 (en) Bipropellant rocket engines
DE3666967D1 (en) Fuel injection control apparatus with forced fuel injection during engine startup period
DE3463821D1 (en) Device for increasing and deflecting thrust of jet-propulsion engine of v/stol aircraft
GB2026407B (en) Hydraulic control system for jet engine thrust reversers
GB8713612D0 (en) Aircraft thrust control
GB1545089A (en) Jet engine thrust reverser and cowl structure
DE3566095D1 (en) Heater system associated with an engine
DE3560960D1 (en) Method for continuous fuel injection and device for carrying out the method
DE3663061D1 (en) Regulating system for the fuel supply of an aircraft engine
GB8713798D0 (en) Aircraft thrust control
GB2165338B (en) Integral rocket and ramjet engine
GB2168298B (en) Thrust reverser
GB2188886B (en) Thrust deflectors for turbomachine propulsion nozzles
EP0278068A3 (en) Thrust vectoring control system for aircraft

Legal Events

Date Code Title Description
EXP Patent expired