IT1006315B - Sistema di controllo di portata refrigerante per camicia di po tenziatore di turbomotore a gas - Google Patents

Sistema di controllo di portata refrigerante per camicia di po tenziatore di turbomotore a gas

Info

Publication number
IT1006315B
IT1006315B IT20314/74A IT2031474A IT1006315B IT 1006315 B IT1006315 B IT 1006315B IT 20314/74 A IT20314/74 A IT 20314/74A IT 2031474 A IT2031474 A IT 2031474A IT 1006315 B IT1006315 B IT 1006315B
Authority
IT
Italy
Prior art keywords
turbomotor
gas
control system
flow control
refrigerant flow
Prior art date
Application number
IT20314/74A
Other languages
English (en)
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
Application filed by Gen Electric filed Critical Gen Electric
Application granted granted Critical
Publication of IT1006315B publication Critical patent/IT1006315B/it

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)
IT20314/74A 1973-02-09 1974-02-08 Sistema di controllo di portata refrigerante per camicia di po tenziatore di turbomotore a gas IT1006315B (it)

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
IT1006315B true IT1006315B (it) 1976-09-30

Family

ID=23292537

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20314/74A IT1006315B (it) 1973-02-09 1974-02-08 Sistema di controllo di portata refrigerante per camicia di po tenziatore di turbomotore a gas

Country Status (8)

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

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
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
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
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 (it) * 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
FR2217547A1 (it) 1974-09-06
US3866417A (en) 1975-02-18
BE810794A (fr) 1974-05-29
GB1458054A (en) 1976-12-08
JPS49112017A (it) 1974-10-25
CA995472A (en) 1976-08-24

Similar Documents

Publication Publication Date Title
IT1006315B (it) Sistema di controllo di portata refrigerante per camicia di po tenziatore di turbomotore a gas
BR7407715D0 (pt) Sistema de refrigeracao
IT1022361B (it) Sistema di protezione contro lostallo per un turbomotore a gas
IT1022228B (it) Sistema di controllo della temperatura e servomotore multifunzionale per lo stesso
IT993054B (it) Sistema di raffreddamento per elementi di turbomotori a gas
BR7500064A (pt) Sistema de refrigeracao
IT1003729B (it) Sistema automatizzato di controllo di volume
IT1011781B (it) Sistema di comando per motori a impulsi
IT1019984B (it) Sistema di comando a distanza per un apparecchio elettric
DK143380C (da) Elektrodekedel med automatisk styring til luftkonditioneringsanlaeg
IT1014878B (it) Mezzo di azionamento per valvola
IT1060804B (it) Sistema di controllo per ferrovie
SE407268B (sv) Styrventilsystem for fluidmanovrerade anordningar
IT1124840B (it) Sistema di comando forzato per valvole per compressore alternativo
IT1022482B (it) Sistema di valvola
IT1024568B (it) Sistema per il controllo di bruciatori
BR7508526A (pt) Sistema de refrigeracao
ZA747333B (en) Control valve for water conditioners
DK141041B (da) Væskestyreorgan til et kraftstyreanlæg til et køretøj.
IT1088478B (it) Sistema di controllo della valvola di spillamento per turboreattori
IT1004726B (it) Sistema di controllo di posizione a trasduttore
IT1014464B (it) Sistema di irrigazione
ZA731367B (en) Local conditioning induction-type apparatus employing primary inlet air as a power means for controlling temperature
SE408585B (sv) Reglerdon for en luftkonditioneringsapparat
IT1049142B (it) Sistema di comando a fluido per doppio impianto di servosterzo