[go: up one dir, main page]

IT8321994A0 - Sistema di scarico di turboventilatore a flusso mescolato. - Google Patents

Sistema di scarico di turboventilatore a flusso mescolato.

Info

Publication number
IT8321994A0
IT8321994A0 IT8321994A IT2199483A IT8321994A0 IT 8321994 A0 IT8321994 A0 IT 8321994A0 IT 8321994 A IT8321994 A IT 8321994A IT 2199483 A IT2199483 A IT 2199483A IT 8321994 A0 IT8321994 A0 IT 8321994A0
Authority
IT
Italy
Prior art keywords
exhaust system
mixed flow
turbo fan
fan exhaust
flow turbo
Prior art date
Application number
IT8321994A
Other languages
English (en)
Other versions
IT1168268B (it
Inventor
Donald John Dusa
Andrew Paul Kuchar
Guy Kemp Faust
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
Publication of IT8321994A0 publication Critical patent/IT8321994A0/it
Application granted granted Critical
Publication of IT1168268B publication Critical patent/IT1168268B/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
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
  • Control Of Motors That Do Not Use Commutators (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
IT21994/83A 1982-07-12 1983-07-08 Sistema di scarico di turboventilatore a flusso mescolato IT1168268B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US39732182A 1982-07-12 1982-07-12

Publications (2)

Publication Number Publication Date
IT8321994A0 true IT8321994A0 (it) 1983-07-08
IT1168268B IT1168268B (it) 1987-05-20

Family

ID=23570739

Family Applications (1)

Application Number Title Priority Date Filing Date
IT21994/83A IT1168268B (it) 1982-07-12 1983-07-08 Sistema di scarico di turboventilatore a flusso mescolato

Country Status (6)

Country Link
JP (1) JPS5932655A (it)
CA (1) CA1209353A (it)
DE (1) DE3324347A1 (it)
FR (1) FR2529956B1 (it)
GB (1) GB2123486B (it)
IT (1) IT1168268B (it)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5117628A (en) * 1990-01-25 1992-06-02 General Electric Company Mixed flow augmentor pre-mixer
US5758488A (en) * 1993-05-11 1998-06-02 Roderick Thomson Core flow expansion chamber device system for reduction of jet turbine engine noise
DE19740228A1 (de) 1997-09-12 1999-03-18 Bmw Rolls Royce Gmbh Turbofan-Flugtriebwerk
WO2000074831A1 (en) * 1999-06-09 2000-12-14 Aeroflo (Proprietary) Limited Method and device for mixing gases
US7017331B2 (en) 2002-12-07 2006-03-28 Anderson Jack H Jet nozzle mixer
WO2003050403A1 (en) 2001-12-07 2003-06-19 Anderson Jack H Jet nozzle mixer
FR2855558B1 (fr) 2003-05-28 2005-07-15 Snecma Moteurs Tuyere de turbomachine a reduction de bruit
FR2858999B1 (fr) * 2003-08-18 2005-11-11 Snecma Moteurs Turbomachine pour aeronef a emissions de bruit reduites
RU2263220C1 (ru) * 2004-01-28 2005-10-27 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Устройство для соединения смесителя с корпусом наружного контура двухконтурного газотурбинного двигателя
FR2911922B1 (fr) * 2007-01-26 2009-04-24 Snecma Sa Melangeur de flux a section variable pour turboreacteur a double flux d'avion supersonique
FR2919899B1 (fr) * 2007-08-06 2014-02-14 Snecma Melangeur a lobes muni de bras redresseurs d'ecoulement pour tuyere a flux confluents de turbomachine
FR3025255B1 (fr) * 2014-09-03 2016-11-04 Turbomeca Tuyere d'echappement de gaz de turbomoteur

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641104A (en) * 1950-04-18 1953-06-09 United Aircraft Corp Tail cone having radially adjustable wall
FR1104644A (fr) * 1954-02-15 1955-11-22 Thomson Houston Comp Francaise Perfectionnements aux systèmes de commande de l'écoulement d'un fluide
US2978865A (en) * 1956-02-06 1961-04-11 Curtiss Wright Corp Turbo fan exhaust mixing device
GB874496A (en) * 1957-08-30 1961-08-10 Robert Westley Jet propulsion nozzle noise suppression means and thrust reverser
US3048376A (en) * 1958-04-09 1962-08-07 Curtiss Wright Corp Fluid mixing apparatus
NL249340A (it) * 1959-03-13
FR1515198A (fr) * 1967-01-18 1968-03-01 Snecma Silencieux à jets fluides pour systèmes d'éjection
US3793865A (en) * 1972-07-05 1974-02-26 Gen Electric Mixer fabrication
US4045957A (en) * 1976-02-20 1977-09-06 United Technologies Corporation Combined guide vane and mixer for a gas turbine engine
US4165609A (en) * 1977-03-02 1979-08-28 The Boeing Company Gas turbine mixer apparatus
US4240252A (en) * 1978-01-19 1980-12-23 General Electric Company Acoustically-treated mixer for a mixed flow gas turbine engine
US4214441A (en) * 1978-09-12 1980-07-29 The United States Of America As Represented By The Secretary Of The Navy Infrared suppressor device
GB2031070B (en) * 1978-10-02 1982-11-17 Boeing Co Suppression of noise from a ducted-fan turbojet engine
FR2438168A1 (fr) * 1978-10-03 1980-04-30 Boeing Co Melangeur d'echappement anti-bruit pour turboreacteur a double flux

Also Published As

Publication number Publication date
GB2123486B (en) 1986-01-02
JPH0344220B2 (it) 1991-07-05
IT1168268B (it) 1987-05-20
DE3324347C2 (it) 1993-04-01
CA1209353A (en) 1986-08-12
DE3324347A1 (de) 1984-01-12
FR2529956A1 (fr) 1984-01-13
GB2123486A (en) 1984-02-01
FR2529956B1 (fr) 1987-01-16
JPS5932655A (ja) 1984-02-22
GB8316375D0 (en) 1983-07-20

Similar Documents

Publication Publication Date Title
IT8119944A0 (it) Sistema ausiliario di ventilazione per turbomotori a gas.
IT8424116A0 (it) Sistema di raffreddamento di componenti di turbomotore a gas.
IT8122555A0 (it) Sistema di controllo di gioco per turbomotori a gas.
IT1208034B (it) Distributore a vortice per un sistema di raffreddamento di turbomotori a gas.
IT8022083A0 (it) Sistema di controllo per turbomotore a gas.
FR2513324B1 (fr) Ventilateur a flux radial
NO158555C (no) Luftkondisjoneringssystem.
IT8321994A0 (it) Sistema di scarico di turboventilatore a flusso mescolato.
IT8220226A0 (it) Motore a turbina a gas e suo sistema di presa d'aria associato.
NO883600D0 (no) Ventilator for transversalstroemming.
IT8224980A0 (it) Sistema di raffreddamento di palette di turbina a gas.
IT8521319A0 (it) Sistema di controllo di turbomotore a gas.
IT8320849A0 (it) Sistema di controllo di pale variabili di statore di turbomotori a gas.
DE3668374D1 (de) Luftdurchflussmengenmesser.
ES271608Y (es) Impulsor de aire, perfeccionado.
IT8223141V0 (it) Bocchetta di ventilazione per abitacolo di autoveicolo.
IT8220265A0 (it) Sistema di turbina a gas.
IT8423838A0 (it) Sistema compatto di entrata del gas fresco, per motori con sovralimentazione combinata.
DK116983A (da) Ventilator
IT8324209A0 (it) Sistema di controllo per turbomotori a gas di aereo.
IT8421174A0 (it) Gas di scarico. sistema di comando per inserire e disinserire un turbocompressore a
IT1178575B (it) Sistema di controllo di aria particolarmente per turbomotore a gas
DE3380900D1 (de) Radialventilator.
IT8223925A0 (it) Dispositivo condizionatore.
IT8221464A0 (it) Sistema di azionamento da impiegare su un turbomotore a gas.

Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19950726