BE810794A - GAS TURBINE ENGINE WITH POST-COMBUSTION DEVICE - Google Patents

GAS TURBINE ENGINE WITH POST-COMBUSTION DEVICE

Info

Publication number
BE810794A
BE810794A BE140711A BE140711A BE810794A BE 810794 A BE810794 A BE 810794A BE 140711 A BE140711 A BE 140711A BE 140711 A BE140711 A BE 140711A BE 810794 A BE810794 A BE 810794A
Authority
BE
Belgium
Prior art keywords
post
gas turbine
turbine engine
combustion device
combustion
Prior art date
Application number
BE140711A
Other languages
French (fr)
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 filed Critical
Publication of BE810794A publication Critical patent/BE810794A/en

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Exhaust Silencers (AREA)
BE140711A 1973-02-09 1974-02-08 GAS TURBINE ENGINE WITH POST-COMBUSTION DEVICE BE810794A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US331078A US3866417A (en) 1973-02-09 1973-02-09 Gas turbine engine augmenter liner coolant flow control system

Publications (1)

Publication Number Publication Date
BE810794A true BE810794A (en) 1974-05-29

Family

ID=23292537

Family Applications (1)

Application Number Title Priority Date Filing Date
BE140711A BE810794A (en) 1973-02-09 1974-02-08 GAS TURBINE ENGINE WITH POST-COMBUSTION DEVICE

Country Status (8)

Country Link
US (1) US3866417A (en)
JP (1) JPS49112017A (en)
BE (1) BE810794A (en)
CA (1) CA995472A (en)
DE (1) DE2405840A1 (en)
FR (1) FR2217547A1 (en)
GB (1) GB1458054A (en)
IT (1) IT1006315B (en)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4072008A (en) * 1976-05-04 1978-02-07 General Electric Company Variable area bypass injector system
US4461146A (en) * 1982-10-22 1984-07-24 The United States Of America As Represented By The Secretary Of The Navy Mixed flow swirl augmentor for turbofan engine
US4833881A (en) * 1984-12-17 1989-05-30 General Electric Company Gas turbine engine augmentor
DE3606286A1 (en) * 1985-03-04 1986-09-04 General Electric Co., Schenectady, N.Y. METHOD AND DEVICE FOR CONTROLLING THE COOLANT FLOW FLOW IN AN AFTERBURN LINING
US4961312A (en) * 1985-03-04 1990-10-09 General Electric Company Method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine
US4958489A (en) * 1985-03-04 1990-09-25 General Electric Company Means for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas turbine engine
US4813229A (en) * 1985-03-04 1989-03-21 General Electric Company Method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas
US4718230A (en) * 1986-11-10 1988-01-12 United Technologies Corporation Augmentor liner construction
US4706453A (en) * 1986-11-12 1987-11-17 General Motors Corporation Support and seal assembly
US4773593A (en) * 1987-05-04 1988-09-27 United Technologies Corporation Coolable thin metal sheet
US4920742A (en) * 1988-05-31 1990-05-01 General Electric Company Heat shield for gas turbine engine frame
GB9127505D0 (en) * 1991-03-11 2013-12-25 Gen Electric Multi-hole film cooled afterburner combustor liner
US5157917A (en) * 1991-05-20 1992-10-27 United Technologies Corporation Gas turbine engine cooling air flow
US5720434A (en) * 1991-11-05 1998-02-24 General Electric Company Cooling apparatus for aircraft gas turbine engine exhaust nozzles
US5201887A (en) * 1991-11-26 1993-04-13 United Technologies Corporation Damper for augmentor liners
DE4338745B4 (en) * 1993-11-12 2005-05-19 Alstom Device for heat shielding the rotor in gas turbines
US5704208A (en) * 1995-12-05 1998-01-06 Brewer; Keith S. Serviceable liner for gas turbine engine
US7966823B2 (en) * 2006-01-06 2011-06-28 General Electric Company Exhaust dust flow splitter system
FR2900444B1 (en) * 2006-04-28 2008-06-13 Snecma Sa TURBOREACTOR COMPRISING A POST COMBUSTION CHANNEL COOLED BY A VARIABLE FLOW VENTILATION FLOW
GB2449477B (en) * 2007-05-24 2009-05-13 Rolls Royce Plc A duct installation
GB0904973D0 (en) * 2009-03-24 2009-05-06 Rolls Royce Plc A casing arrangement
US10253651B2 (en) * 2012-06-14 2019-04-09 United Technologies Corporation Turbomachine flow control device
US10054080B2 (en) * 2012-10-22 2018-08-21 United Technologies Corporation Coil spring hanger for exhaust duct liner
FR3004494B1 (en) * 2013-04-15 2018-01-19 Safran Nacelles TUYERE FOR AIRCRAFT TURBOPROPULSER WITH NON-CARBONATED BLOWER
US10385868B2 (en) * 2016-07-05 2019-08-20 General Electric Company Strut assembly for an aircraft engine
FR3100284B1 (en) * 2019-08-30 2021-12-03 Safran Aircraft Engines COUPLE CONVERGENT-DIVERGENT FLAP FOR VARIABLE GEOMETRY TURBOREACTOR NOZZLE WHOSE SHUTTERS EACH INCLUDE A COOLING AIR CIRCULATION DUCT
US11905843B2 (en) * 2020-04-01 2024-02-20 General Electric Company Liner support system

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR962862A (en) * 1946-10-26 1950-06-22
US2974486A (en) * 1958-03-27 1961-03-14 United Aircraft Corp Afterburner mixture and flame control baffle
US3031844A (en) * 1960-08-12 1962-05-01 William A Tomolonius Split combustion liner
FR1525092A (en) * 1967-01-23 1968-05-17 Snecma Hot gas flow and cold air flow turbo-reactor
US3712062A (en) * 1968-04-17 1973-01-23 Gen Electric Cooled augmentor liner
GB1180706A (en) * 1968-08-02 1970-02-11 Rolls Royce Flame Tube

Also Published As

Publication number Publication date
JPS49112017A (en) 1974-10-25
CA995472A (en) 1976-08-24
IT1006315B (en) 1976-09-30
DE2405840A1 (en) 1974-08-15
FR2217547A1 (en) 1974-09-06
GB1458054A (en) 1976-12-08
US3866417A (en) 1975-02-18

Similar Documents

Publication Publication Date Title
BE810491A (en) GAS TURBINE ENGINE WITH POST-COMBUSTION DEVICE
BE810794A (en) GAS TURBINE ENGINE WITH POST-COMBUSTION DEVICE
BE810901A (en) GAS TURBINE ENGINE
FR2290350A1 (en) NACELLE FOR GAS TURBINE ENGINE
FR2333954A1 (en) GAS TURBINE ENGINE MECHANISM
FR2313566A1 (en) VARIABLE CYCLE GAS TURBINE ENGINE
BE861363A (en) PERFECTED DIFFUSER FOR GAS TURBINE ENGINE
NL7502782A (en) COMBUSTION ENGINE (A).
IT7821288A0 (en) GAS TURBINE ENGINE.
FR2284754A1 (en) GAS TURBINE ENGINE STATOR ELEMENT
SE428387B (en) FUEL, INCLUDING A COMBUSTION ENGINE
FR2315612A1 (en) GAS TURBINE ENGINE
FR2315611A1 (en) GAS TURBINE ENGINE
BE818151A (en) COMPRESSED GAS ENGINE
NO147889C (en) SPEED LIMITS FOR A COMBUSTION ENGINE.
FR2333126A1 (en) GAS TURBINE ENGINE COMBUSTION CHAMBER REFRIGERATION DEVICE
FR2316434A1 (en) AUTOMATIC START GAS ENGINE
SE391222B (en) CONTROL DEVICE FOR A GAS TURBINE ENGINE
IT1034600B (en) GAS TURBINE ENGINE
BE805378A (en) IGNITION DEVICE FOR GAS TURBINE ENGINE
JPS5211315A (en) Gas turbine engine exhaust device
BE763178A (en) GAS TURBINE ENGINE WITH ADVANCED AFTER-COMBUSTION DEVICE
BE837177A (en) IGNITION DEVICE FOR GAS TURBINE ENGINE
FR2314361A1 (en) GAS TURBINE ENGINE
BE795004A (en) REGULATION DEVICE FOR GAS TURBINE ENGINE UNIT, IN PARTICULAR FOR TURBOREACTOR