GB659795A - Improvements in or relating to combustion systems particularly applicable to high velocity gas streams - Google Patents

Improvements in or relating to combustion systems particularly applicable to high velocity gas streams

Info

Publication number
GB659795A
GB659795A GB261045A GB261045A GB659795A GB 659795 A GB659795 A GB 659795A GB 261045 A GB261045 A GB 261045A GB 261045 A GB261045 A GB 261045A GB 659795 A GB659795 A GB 659795A
Authority
GB
United Kingdom
Prior art keywords
relating
high velocity
gas streams
particularly applicable
velocity gas
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
GB261045A
Inventor
Daniel Norman Walker
Henry Cohen
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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 to NL68406D priority Critical patent/NL68406C/xx
Application filed by Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB261045A priority patent/GB659795A/en
Priority to CH266196D priority patent/CH266196A/en
Publication of GB659795A publication Critical patent/GB659795A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00—Subject-matter not provided for in other groups of this subclass
    • C—CHEMISTRY; METALLURGY
    • C10—PETROLEUM, GAS OR COKE INDUSTRIES; TECHNICAL GASES CONTAINING CARBON MONOXIDE; FUELS; LUBRICANTS; PEAT
    • C10L—FUELS NOT OTHERWISE PROVIDED FOR; NATURAL GAS; SYNTHETIC NATURAL GAS OBTAINED BY PROCESSES NOT COVERED BY SUBCLASSES C10G, C10K; LIQUEFIED PETROLEUM GAS; ADDING MATERIALS TO FUELS OR FIRES TO REDUCE SMOKE OR UNDESIRABLE DEPOSITS OR TO FACILITATE SOOT REMOVAL; FIRELIGHTERS
    • C10L1/00—Liquid carbonaceous fuels
    • C10L1/04—Liquid carbonaceous fuels essentially based on blends of hydrocarbons
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2700/00—Special arrangements for combustion apparatus using fluent fuel
    • F23C2700/02—Combustion apparatus using liquid fuel
    • F23C2700/023—Combustion apparatus using liquid fuel without pre-vaporising means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)

Abstract

A pilot fuel for starting the combustion of kerosene in a reheat combustion system for the exhaust gases of gas turbines consists of a lubricating oil containing 10.05 to 0.1 per cent of stearic acid and approximately 5 per cent of amyl nitrite. Alternatively the fuel may consist of colloidal magnesium or tertiary butyl peroxide.
GB261045A 1945-02-01 1945-02-01 Improvements in or relating to combustion systems particularly applicable to high velocity gas streams Expired GB659795A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
NL68406D NL68406C (en) 1945-02-01
GB261045A GB659795A (en) 1945-02-01 1945-02-01 Improvements in or relating to combustion systems particularly applicable to high velocity gas streams
CH266196D CH266196A (en) 1945-02-01 1946-01-29 Process for burning fuel in a hot gas stream at high velocity and apparatus for carrying out this process.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB261045A GB659795A (en) 1945-02-01 1945-02-01 Improvements in or relating to combustion systems particularly applicable to high velocity gas streams
GB951545 1945-04-16

Publications (1)

Publication Number Publication Date
GB659795A true GB659795A (en) 1951-10-31

Family

ID=26237615

Family Applications (1)

Application Number Title Priority Date Filing Date
GB261045A Expired GB659795A (en) 1945-02-01 1945-02-01 Improvements in or relating to combustion systems particularly applicable to high velocity gas streams

Country Status (3)

Country Link
CH (1) CH266196A (en)
GB (1) GB659795A (en)
NL (1) NL68406C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1051071B (en) * 1955-07-13 1959-02-19 Sud Aviation Combustion device for supersonic ramjet engines

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB667394A (en) * 1949-04-28 1952-02-27 Rolls Royce Improvements in or relating to combustion equipment for gas-turbine engines
US2828609A (en) * 1950-04-03 1958-04-01 Bristol Aero Engines Ltd Combustion chambers including suddenly enlarged chamber portions
US2697910A (en) * 1950-07-29 1954-12-28 Thermal Res And Engineering Co Fluid fuel burner with self-contained fuel vaporizing unit
US2651178A (en) * 1951-01-18 1953-09-08 A V Roe Canada Ltd Combination injector and stabilizer for gas turbine afterburners

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1051071B (en) * 1955-07-13 1959-02-19 Sud Aviation Combustion device for supersonic ramjet engines

Also Published As

Publication number Publication date
CH266196A (en) 1950-01-15
NL68406C (en)

Similar Documents

Publication Publication Date Title
CH284190A (en) Metal combustion chamber for generating hot gases, especially propellants for gas turbine systems.
GB680371A (en) Reheater for jet propulsion engines
FR951218A (en) Improvements to fuel systems for jet engines, gas turbines and similar power sources
GB659795A (en) Improvements in or relating to combustion systems particularly applicable to high velocity gas streams
ES262327A1 (en) Combustion equipment for a gas turbine engine
GB533330A (en) Generating combustion products for power purposes
GB637229A (en) Improvements relating to combustion chambers for liquid fuels
ES162326A1 (en) A GASOGEN FOR AUTOMOBILE VEHICLES
GB734190A (en) Method of reducing the corrosive attack of combustion gases on metal
CA607893A (en) Flame tubes for use in combustion systems of gas turbine engines
GB531430A (en) Apparatus for supplying an engine from a gas-producer applicable to explosion engines employing combustible liquids
GB428972A (en) Improvements in or relating to liquid fuels for internal combustion engines
GB564704A (en) Improvements in gas generators charged with solid combustible fuel
FR1144045A (en) Improvements to turbojets and gas turbines, particularly for the propulsion of air, land and marine vehicles
GB238621A (en) Improvements in and relating to the production of oxides of sulphur
ES154570A1 (en) SYSTEM OF APPLICATION OF FUEL TO VEHICLES OF ALL KINDS OPERATED BY INTERNAL COMBUSTION ENGINE IN WHICH THE COMPRESSED GAS IS USED, OR THE MIXTURE OF BOTH COMPRESSED
GB599974A (en) Installation for propulsion by reaction, notably for aircraft
GB802612A (en) Difficultly hydrolysable additives for diesel fuels
AU200301B2 (en) Low tension ignition system for jet engines, gas turbines, oil burner boilers and similar installations
FR953222A (en) Method and device for feeding heavy fuels (such as gas oil, petroleum, etc.) to internal combustion engines
ES167667A1 (en) A PRESSURE COOLING PROCEDURE COMBINED WITH A REHEATER INSTALLED IN THE EXHAUST DUCT FOR MIXED INTERNAL COMBUSTION AND VAPOR ENGINES
FR931213A (en) Improvements to fuel supply and power control systems for gas turbines, jet engines, etc.
AU41254A (en) Low tension ignition system for jet engines, gas turbines, oil burner boilers and similar installations
GB921621A (en) Improvements in or relating to gas turbine engines
ES220295A1 (en) A steam boiler for the heating of railway cars or similar. (Machine-translation by Google Translate, not legally binding)