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CH335303A - Afterburner for aircraft jet engines - Google Patents

Afterburner for aircraft jet engines

Info

Publication number
CH335303A
CH335303A CH335303DA CH335303A CH 335303 A CH335303 A CH 335303A CH 335303D A CH335303D A CH 335303DA CH 335303 A CH335303 A CH 335303A
Authority
CH
Switzerland
Prior art keywords
afterburner
jet engines
aircraft jet
aircraft
engines
Prior art date
Application number
Other languages
German (de)
Inventor
Edward Ledbetter Robert
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 claimed from US417192A external-priority patent/US2874536A/en
Application filed by Gen Electric filed Critical Gen Electric
Publication of CH335303A publication Critical patent/CH335303A/en

Links

Classifications

    • 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
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Exhaust Silencers (AREA)
  • Spray-Type Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH335303D 1954-02-23 1955-02-22 Afterburner for aircraft jet engines CH335303A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US803813XA 1954-02-23 1954-02-23
US417192A US2874536A (en) 1954-03-18 1954-03-18 Cooling means for tailpipe

Publications (1)

Publication Number Publication Date
CH335303A true CH335303A (en) 1958-12-31

Family

ID=26763440

Family Applications (2)

Application Number Title Priority Date Filing Date
CH335303D CH335303A (en) 1954-02-23 1955-02-22 Afterburner for aircraft jet engines
CH331332D CH331332A (en) 1954-02-23 1955-03-17 Afterburner on an aircraft jet engine

Family Applications After (1)

Application Number Title Priority Date Filing Date
CH331332D CH331332A (en) 1954-02-23 1955-03-17 Afterburner on an aircraft jet engine

Country Status (4)

Country Link
BE (1) BE535906A (en)
CH (2) CH335303A (en)
DE (2) DE1021208B (en)
GB (2) GB803813A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3307354A (en) * 1965-10-01 1967-03-07 Gen Electric Cooling structure for overlapped panels

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3085401A (en) * 1959-01-22 1963-04-16 Rolls Royce Reheat combustion equipment of gas-turbine engines
DE1221053B (en) * 1960-06-11 1966-07-14 Rolls Royce Turbine jet engine
DE1210628B (en) * 1962-02-08 1966-02-10 Rolls Royce Jet pipe for recoil engines, for example for the gas turbine jet engine of an aircraft
GB1102572A (en) * 1964-06-06 1968-02-07 Bristol Siddeley Engines Ltd Jet propulsion engines
GB1157930A (en) * 1966-12-28 1969-07-09 Rolls Royce Gas Turbine Jet Propulsion Engine
US4833881A (en) * 1984-12-17 1989-05-30 General Electric Company Gas turbine engine augmentor
US20060137352A1 (en) * 2004-12-29 2006-06-29 United Technologies Corporation Augmentor liner

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH214477A (en) * 1939-01-30 1941-04-30 Bbc Brown Boveri & Cie Cooling device on pipes, containers, housings or the like through which hot gases flow or which include them.
US2458497A (en) * 1945-05-05 1949-01-11 Babcock & Wilcox Co Combustion chamber
FR962862A (en) * 1946-10-26 1950-06-22
CH255541A (en) * 1947-05-12 1948-06-30 Bbc Brown Boveri & Cie Cooled metal combustion chamber for generating heating and propellant gases.
NL72931C (en) * 1948-02-21
US2508420A (en) * 1948-09-21 1950-05-23 Westinghouse Electric Corp Combustion apparatus
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner
US2632299A (en) * 1949-06-17 1953-03-24 United Aircraft Corp Precombustion chamber
DE825777C (en) * 1949-08-19 1951-12-20 Canadian Patents Dev Flame tube of combustion chambers, especially for gas turbines
GB700004A (en) * 1949-12-12 1953-11-25 Babcock & Wilcox Ltd Improvements in or relating to combustion apparatus
DE889240C (en) * 1950-10-17 1953-09-10 Canadian Patents Dev Flame tube of combustion chambers, especially for gas turbine engines
US2651912A (en) * 1950-10-31 1953-09-15 Gen Electric Combustor and cooling means therefor
FR1002312A (en) * 1951-04-01 1952-03-05 Combustion chamber for thermo-propellants, turbo-engines or the like

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3307354A (en) * 1965-10-01 1967-03-07 Gen Electric Cooling structure for overlapped panels

Also Published As

Publication number Publication date
GB802370A (en) 1958-10-01
DE1045180B (en) 1958-11-27
DE1021208B (en) 1957-12-19
CH331332A (en) 1958-07-15
BE535906A (en)
GB803813A (en) 1958-11-05

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