GB1407869A - Apparatus for burning normally non-fluid fuel - Google Patents

Apparatus for burning normally non-fluid fuel

Info

Publication number
GB1407869A
GB1407869A GB381173A GB381173A GB1407869A GB 1407869 A GB1407869 A GB 1407869A GB 381173 A GB381173 A GB 381173A GB 381173 A GB381173 A GB 381173A GB 1407869 A GB1407869 A GB 1407869A
Authority
GB
United Kingdom
Prior art keywords
fluid fuel
normally non
burning normally
burning
fuel
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
GB381173A
Other languages
English (en)
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.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 JP47012047A external-priority patent/JPS5138004B2/ja
Priority claimed from JP1793372A external-priority patent/JPS506606B2/ja
Application filed by Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Publication of GB1407869A publication Critical patent/GB1407869A/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
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
    • 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
    • F02K9/70—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using semi- solid or pulverulent propellants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G7/00—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
    • F23G7/12—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of plastics, e.g. rubber
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L2900/00—Special arrangements for supplying or treating air or oxidant for combustion; Injecting inert gas, water or steam into the combustion chamber
    • F23L2900/07004—Injecting liquid or solid materials releasing oxygen, e.g. perchlorate, nitrate, peroxide, and chlorate compounds, or appropriate mixtures thereof
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Environmental & Geological Engineering (AREA)
GB381173A 1972-02-02 1973-01-25 Apparatus for burning normally non-fluid fuel Expired GB1407869A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP47012047A JPS5138004B2 (enExample) 1972-02-02 1972-02-02
JP1793372A JPS506606B2 (enExample) 1972-02-21 1972-02-21

Publications (1)

Publication Number Publication Date
GB1407869A true GB1407869A (en) 1975-09-24

Family

ID=26347592

Family Applications (1)

Application Number Title Priority Date Filing Date
GB381173A Expired GB1407869A (en) 1972-02-02 1973-01-25 Apparatus for burning normally non-fluid fuel

Country Status (4)

Country Link
US (1) US3792669A (enExample)
DE (1) DE2304970A1 (enExample)
FR (1) FR2170153B1 (enExample)
GB (1) GB1407869A (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH585874A5 (enExample) * 1975-07-04 1977-03-15 Demoiseau Bernard
US6367244B1 (en) * 1997-05-09 2002-04-09 Hy Pat Corporation Propulsion system containing a mixed-phase propellant and a method for propelling an object with the same
GB9917404D0 (en) * 1999-07-26 2000-08-23 Secr Defence Hydrogen peroxide based propulsion system
CA2367197A1 (en) * 2001-01-10 2002-07-10 Cesaroni Technology Incorporated Liquid/solid fuel hybrid propellant system for a rocket
CA2504993A1 (en) * 2004-04-28 2005-10-28 Anthony Joseph Cesaroni Injector system for rocket motors
US10920714B2 (en) * 2013-03-15 2021-02-16 Exquadrum, Inc. Stable hybrid rocket technology
DE112019005545B4 (de) * 2018-11-06 2025-02-06 Cummins Emission Solutions Inc. Systeme und Verfahren zum Reduzieren einer Bildung von Reduktionsmittelablagerungen in einem Zersetzungsreaktor eines Abgasnachbehandlungssystems für einen Verbrennungsmotor
US11952965B2 (en) 2019-01-30 2024-04-09 Laboratoire Reaction Dynamics Inc. Rocket engine's thrust chamber assembly

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3085393A (en) * 1958-06-03 1963-04-16 North American Aviation Inc Rocket engine starting method
US3106059A (en) * 1961-03-30 1963-10-08 United Aircraft Corp Oxidizer inlet and igniter for a rocket
US3120738A (en) * 1962-03-03 1964-02-11 James E Webb Ignition system for monopropellant combustion devices
US3518828A (en) * 1968-09-27 1970-07-07 Us Air Force Hybrid rocket motor ignition system

Also Published As

Publication number Publication date
FR2170153A1 (enExample) 1973-09-14
US3792669A (en) 1974-02-19
DE2304970A1 (de) 1973-08-30
FR2170153B1 (enExample) 1976-05-14

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
746 Register noted 'licences of right' (sect. 46/1977)
PCNP Patent ceased through non-payment of renewal fee