GB1458054A - Gas turbine engines including exhaust reheat combustion equipment - Google Patents

Gas turbine engines including exhaust reheat combustion equipment

Info

Publication number
GB1458054A
GB1458054A GB448374A GB448374A GB1458054A GB 1458054 A GB1458054 A GB 1458054A GB 448374 A GB448374 A GB 448374A GB 448374 A GB448374 A GB 448374A GB 1458054 A GB1458054 A GB 1458054A
Authority
GB
United Kingdom
Prior art keywords
liner
openings
jet pipe
gas turbine
engine
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
GB448374A
Other languages
English (en)
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB1458054A publication Critical patent/GB1458054A/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
    • 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)
GB448374A 1973-02-09 1974-01-31 Gas turbine engines including exhaust reheat combustion equipment Expired GB1458054A (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
GB1458054A true GB1458054A (en) 1976-12-08

Family

ID=23292537

Family Applications (1)

Application Number Title Priority Date Filing Date
GB448374A Expired GB1458054A (en) 1973-02-09 1974-01-31 Gas turbine engines including exhaust reheat combustion equipment

Country Status (8)

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

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
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
DE3606286A1 (de) * 1985-03-04 1986-09-04 General Electric Co., Schenectady, N.Y. Verfahren und einrichtung zum steuern des kuehlmittelstroemungsflusses in einer nachbrennerauskleidung
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
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 (de) * 1993-11-12 2005-05-19 Alstom Vorrichtung zur Wärmeabschirmung des Rotors in Gasturbinen
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 (fr) * 2006-04-28 2008-06-13 Snecma Sa Turboreacteur comprenant un canal de post combustion refroidi par un flux de ventilation a debit variable
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 (fr) * 2013-04-15 2018-01-19 Safran Nacelles Tuyere pour turbopropulseur d’aeronef a soufflante non carenee
US10385868B2 (en) * 2016-07-05 2019-08-20 General Electric Company Strut assembly for an aircraft engine
FR3100284B1 (fr) * 2019-08-30 2021-12-03 Safran Aircraft Engines Couple volet convergent-volet divergent pour tuyère de turboréacteur à géométrie variable dont les volets comprennent chacun un conduit de circulation d’air de refroidissement
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 (enrdf_load_stackoverflow) * 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 (fr) * 1967-01-23 1968-05-17 Snecma Turbo-réacteur à flux de gaz chaud et à flux d'air froid
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
DE2405840A1 (de) 1974-08-15
US3866417A (en) 1975-02-18
CA995472A (en) 1976-08-24
BE810794A (fr) 1974-05-29
FR2217547A1 (enrdf_load_stackoverflow) 1974-09-06
JPS49112017A (enrdf_load_stackoverflow) 1974-10-25
IT1006315B (it) 1976-09-30

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee