CH365910A - Afterburner on a jet engine - Google Patents

Afterburner on a jet engine

Info

Publication number
CH365910A
CH365910A CH6213358A CH6213358A CH365910A CH 365910 A CH365910 A CH 365910A CH 6213358 A CH6213358 A CH 6213358A CH 6213358 A CH6213358 A CH 6213358A CH 365910 A CH365910 A CH 365910A
Authority
CH
Switzerland
Prior art keywords
afterburner
jet engine
jet
engine
Prior art date
Application number
CH6213358A
Other languages
German (de)
Inventor
Howard Shackelford Milton
Mccardle Arthur Jr
Original Assignee
Gen Electric
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 GB1514458A priority Critical patent/GB842197A/en
Priority to DEG24595A priority patent/DE1123163B/en
Application filed by Gen Electric filed Critical Gen Electric
Priority to CH6213358A priority patent/CH365910A/en
Publication of CH365910A publication Critical patent/CH365910A/en

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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
CH6213358A 1958-05-23 1958-07-23 Afterburner on a jet engine CH365910A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB1514458A GB842197A (en) 1958-07-23 1958-05-12 Improvements in afterburner combustion equipment of a gas turbine jet propulsion engine
DEG24595A DE1123163B (en) 1958-05-23 1958-05-23 Recoil engine with afterburners
CH6213358A CH365910A (en) 1958-07-23 1958-07-23 Afterburner on a jet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH6213358A CH365910A (en) 1958-07-23 1958-07-23 Afterburner on a jet engine

Publications (1)

Publication Number Publication Date
CH365910A true CH365910A (en) 1962-11-30

Family

ID=4524103

Family Applications (1)

Application Number Title Priority Date Filing Date
CH6213358A CH365910A (en) 1958-05-23 1958-07-23 Afterburner on a jet engine

Country Status (2)

Country Link
CH (1) CH365910A (en)
GB (1) GB842197A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2873168B1 (en) * 2004-07-16 2008-10-31 Snecma Moteurs Sa TURBOREACTOR COMPRISING A SECURED IGNITION POST-COMBUSTION CHAMBER
GB201907834D0 (en) 2019-06-03 2019-07-17 Rolls Royce Plc A fuel sparay nozzle arrangement

Also Published As

Publication number Publication date
GB842197A (en) 1960-07-20

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