GB659794A - Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams - Google Patents

Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams

Info

Publication number
GB659794A
GB659794A GB25261/44A GB2526144A GB659794A GB 659794 A GB659794 A GB 659794A GB 25261/44 A GB25261/44 A GB 25261/44A GB 2526144 A GB2526144 A GB 2526144A GB 659794 A GB659794 A GB 659794A
Authority
GB
United Kingdom
Prior art keywords
fuel
jets
bullet
pot
apex
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
GB25261/44A
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
Application filed by Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB25261/44A priority Critical patent/GB659794A/en
Priority to CH272676D priority patent/CH272676A/en
Priority to FR922032D priority patent/FR922032A/en
Priority to BE463180D priority patent/BE463180A/xx
Priority to NL125040A priority patent/NL68602C/xx
Publication of GB659794A publication Critical patent/GB659794A/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
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers

Abstract

659,794. Jet propulsion engines. POWER JETS (RESEARCH & DEVELOPMENT) Ltd., COHEN, H., and DARTH, J. H. H. Dec. 15, 1944, No. 25261. [Class 110(iii)] [Also in Group XII] Means for reheating the exhaust gases of a gas turbine jet propulsion engine comprises a cylindrical pot 12, having an open end 13 facing downstream around which there is a fuel pipe 14 pierced with holes 15, attached to the truncated apex of the turbine exhaust fairing 8. Within the pot is an igniter 16. The presence and form of the pot 12 produces turbulence in the main gas stream and causes part of it together with entrained fuel to enter the pot where it is ignited. The resulting flame ignites the fuel sprayed radially outwards by the jets 15. The operation of the ignition may be effected by a single lever connected to the fuel control means and to the control of a variable area propelling nozzle as described in Specification 659,793. In the Provisional Specification an arrangement is described in which a series of fuel jets is arranged at a short distance upstream from the apex of the bullet in recesses within the profile of the bullet. These recesses have miniature trap doors to cover them when the fuel jets are not in use. In another arrangement the fuel jets are arranged upstream of the apex of the bullet in or near a part of the bullet which is of such material and design that it has a large heat capacity so that it will re-ignite the flame if it is extinguished. In both of these arrangements, means may be provided to drain the fuel supply piping where it is liable to get hot. and to blow cold air through the piping when the fuel is shut off.
GB25261/44A 1944-12-15 1944-12-15 Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams Expired GB659794A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB25261/44A GB659794A (en) 1944-12-15 1944-12-15 Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams
CH272676D CH272676A (en) 1944-12-15 1946-01-22 Device for the combustion of liquid fuel in a gas stream at high speed.
FR922032D FR922032A (en) 1944-12-15 1946-02-12 Improvements to devices for obtaining stable combustion of fuel in high velocity gas streams
BE463180D BE463180A (en) 1944-12-15 1946-02-18
NL125040A NL68602C (en) 1944-12-15 1946-04-30

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB25261/44A GB659794A (en) 1944-12-15 1944-12-15 Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams

Publications (1)

Publication Number Publication Date
GB659794A true GB659794A (en) 1951-10-31

Family

ID=10256807

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25261/44A Expired GB659794A (en) 1944-12-15 1944-12-15 Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams

Country Status (5)

Country Link
BE (1) BE463180A (en)
CH (1) CH272676A (en)
FR (1) FR922032A (en)
GB (1) GB659794A (en)
NL (1) NL68602C (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2707372A (en) * 1947-06-11 1955-05-03 Lockheed Aircraft Corp Afterburner apparatus for turbo jet engines having movable flame holder means
US2724238A (en) * 1950-10-25 1955-11-22 Tresham D Gregg Jet propulsive devices
US2771740A (en) * 1950-11-16 1956-11-27 Lockheed Aircraft Corp Afterburning means for turbo-jet engines
US2768498A (en) * 1950-12-15 1956-10-30 Gen Motors Corp Retractable afterburner
US2729937A (en) * 1951-03-20 1956-01-10 United Aircraft Corp Retractable flameholders for afterburners
US2835108A (en) * 1951-07-17 1958-05-20 Solar Aircraft Co Variable area flametholder for afterburner
US2866314A (en) * 1953-01-02 1958-12-30 United Aircraft Corp Flame holding device movable between a flameholding position and a streamlined position
DE1074920B (en) * 1955-07-07 1960-02-04 Ing habil Fritz A F Schmidt Murnau Dr (Obb) Method and device for regulating gas turbine combustion chambers with subdivided combustion and several pressure levels

Also Published As

Publication number Publication date
FR922032A (en) 1947-05-27
CH272676A (en) 1950-12-31
BE463180A (en) 1946-03-30
NL68602C (en) 1951-09-15

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