IL61028A0 - Foreign particle separator system for use in a gas turbine - Google Patents

Foreign particle separator system for use in a gas turbine

Info

Publication number
IL61028A0
IL61028A0 IL61028A IL6102880A IL61028A0 IL 61028 A0 IL61028 A0 IL 61028A0 IL 61028 A IL61028 A IL 61028A IL 6102880 A IL6102880 A IL 6102880A IL 61028 A0 IL61028 A0 IL 61028A0
Authority
IL
Israel
Prior art keywords
gas turbine
particle separator
separator system
foreign particle
foreign
Prior art date
Application number
IL61028A
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
Publication of IL61028A0 publication Critical patent/IL61028A0/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
    • F02C7/052—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with dust-separation devices
    • 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)
  • Jet Pumps And Other Pumps (AREA)
  • Cyclones (AREA)
  • Separating Particles In Gases By Inertia (AREA)
IL61028A 1979-10-01 1980-09-10 Foreign particle separator system for use in a gas turbine IL61028A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/080,854 US4265646A (en) 1979-10-01 1979-10-01 Foreign particle separator system

Publications (1)

Publication Number Publication Date
IL61028A0 true IL61028A0 (en) 1980-11-30

Family

ID=22160062

Family Applications (1)

Application Number Title Priority Date Filing Date
IL61028A IL61028A0 (en) 1979-10-01 1980-09-10 Foreign particle separator system for use in a gas turbine

Country Status (8)

Country Link
US (1) US4265646A (fr)
JP (1) JPS5664122A (fr)
CA (1) CA1136866A (fr)
DE (1) DE3036525A1 (fr)
FR (1) FR2466617A1 (fr)
GB (1) GB2058929A (fr)
IL (1) IL61028A0 (fr)
IT (1) IT1133141B (fr)

Families Citing this family (78)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2095335B (en) 1981-03-20 1984-05-31 Rolls Royce Gas turbine engine air intake system
US4456458A (en) * 1982-09-20 1984-06-26 The De Havilland Aircraft Of Canada, Limited Air intake system for engine
US4527387A (en) * 1982-11-26 1985-07-09 General Electric Company Particle separator scroll vanes
US4685942A (en) * 1982-12-27 1987-08-11 General Electric Company Axial flow inlet particle separator
CH663254A5 (de) * 1983-06-06 1987-11-30 Jakob Huber Gasturbinen-triebwerk mit kohlenstaubfeuerung.
US4509962A (en) * 1983-10-06 1985-04-09 Pratt & Whitney Canada Inc. Inertial particle separator
GB2196390B (en) * 1986-10-16 1991-06-26 Rolls Royce Plc Intake for turbopropeller gas turbine engine.
US4896510A (en) * 1987-02-06 1990-01-30 General Electric Company Combustor liner cooling arrangement
GB2203801B (en) * 1987-04-14 1991-11-27 Rolls Royce Plc A gas turbine engine
GB2509886B (en) * 1992-09-22 2015-03-18 Rolls Royce Plc Improvements in or relating to engine intake protection and supression of engine infra-red emissions
DE4413202C2 (de) * 1994-04-13 2000-08-17 Ver Energiewerke Ag Verfahren und Anordnung zur Vermeidung des Anhaftens von in einem Heißgas geführten Partikeln an einem vom Heißgas beaufschlagten Anlagenteil, insbesondere an den Schaufeln einer Gasturbine
DE19632038A1 (de) * 1996-08-08 1998-02-12 Asea Brown Boveri Vorrichtung zur Abscheidung von Staubpartikeln
RU2169851C2 (ru) * 1999-06-03 2001-06-27 Открытое акционерное общество "Рыбинские моторы" Газотурбинный двигатель
EP1237641B1 (fr) * 1999-11-23 2015-09-09 Marina Ellen Marinella Pavlatos Moteur avec capot a contre courant fixe de façon rotative
US8876930B2 (en) * 1999-11-23 2014-11-04 Marina Ellen Marinella Pavlatos Single/multiple guard(s)/cap(s) and/or screen(s) with engine attached chamber/manifold particle collector
RU2198311C2 (ru) * 2001-01-03 2003-02-10 Открытое акционерное общество "Авиадвигатель" Газотурбинная установка
DE10162238A1 (de) 2001-12-18 2003-07-10 Rolls Royce Deutschland Lufteinlasssystem eines PTL-Antriebs
US7976273B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Tip turbine engine support structure
US8641367B2 (en) 2004-12-01 2014-02-04 United Technologies Corporation Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
EP1831520B1 (fr) * 2004-12-01 2009-02-25 United Technologies Corporation Moteur à turbine d'extremité et procédé d'opération associé
WO2006059980A2 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Aspiration par diffuseur pour moteur a turbine d'extremite
US7882695B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Turbine blow down starter for turbine engine
DE602004016065D1 (de) 2004-12-01 2008-10-02 United Technologies Corp Variable gebläseeinlassleitschaufelanordnung, turbinenmotor mit solch einer anordnung und entsprechendes steuerverfahren
US8365511B2 (en) 2004-12-01 2013-02-05 United Technologies Corporation Tip turbine engine integral case, vane, mount and mixer
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
EP1825117B1 (fr) 2004-12-01 2012-06-13 United Technologies Corporation Moteur à turbine équipé d'une soufflante et d'un compresseur entraînés par un engrenage différentiel
WO2006059971A2 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Logement de moteur a turbine integrant un ventilateur, un combustor, et une turbine
DE602004027766D1 (de) 2004-12-01 2010-07-29 United Technologies Corp Hydraulische dichtung für ein getriebe eines spitzenturbinenmotors
US7874802B2 (en) 2004-12-01 2011-01-25 United Technologies Corporation Tip turbine engine comprising turbine blade clusters and method of assembly
EP1828591B1 (fr) * 2004-12-01 2010-07-21 United Technologies Corporation Foyer peripherique pour moteur a turbine de bout
WO2006060010A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Pale de guidage d’entree de compresseur pour moteur de turbine a pression d’entree et procede de commande correspondant
US7959406B2 (en) 2004-12-01 2011-06-14 United Technologies Corporation Close coupled gearbox assembly for a tip turbine engine
EP1825111B1 (fr) 2004-12-01 2011-08-31 United Technologies Corporation Carter de compresseur à rotation inverse pour un moteur à turbine en bout
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
WO2006060001A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Rotor de ventilateur pour moteur a turbine de bout
EP1819907A2 (fr) 2004-12-01 2007-08-22 United Technologies Corporation Pale de ventilateur comprenant une section de diffuseur integrale et une section de pale de turbine a aube destine a une moteur a turbine a aube
EP1828683B1 (fr) 2004-12-01 2013-04-10 United Technologies Corporation Dispositif de combustion pour moteur de turbine
WO2006059988A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine de bout modulaire
WO2006059995A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Systeme de lubrification de boite de vitesses pour moteur a turbine d'extremite
WO2006060006A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Cone arriere non metallique de moteur a turbine de bout
US7878762B2 (en) 2004-12-01 2011-02-01 United Technologies Corporation Tip turbine engine comprising turbine clusters and radial attachment lock arrangement therefor
EP1828545A2 (fr) 2004-12-01 2007-09-05 United Technologies Corporation Elements annulaires de rotor de turbine
WO2006060013A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Ensemble de joint de rotor de ventilateur de moteur de turbine a pression d’entree
EP1825116A2 (fr) * 2004-12-01 2007-08-29 United Technologies Corporation Refroidissement par ejecteur de l'enveloppe exterieure d'un moteur a turbine de bout
DE602004031470D1 (de) * 2004-12-01 2011-03-31 United Technologies Corp Übergangskanal mit mitteln zur strömungsvektorbeeinflussung bei einer gasturbine
US8104257B2 (en) * 2004-12-01 2012-01-31 United Technologies Corporation Tip turbine engine with multiple fan and turbine stages
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
US7607286B2 (en) 2004-12-01 2009-10-27 United Technologies Corporation Regenerative turbine blade and vane cooling for a tip turbine engine
WO2006110125A2 (fr) * 2004-12-01 2006-10-19 United Technologies Corporation Elements annulaires empiles pour moteurs a turbine
WO2006059986A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine de bout et procede de fonctionnement avec inversion de la circulation d'air du noyau du ventilateur
WO2006060014A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Systeme de generateur-demarreur pour moteur de turbine a pression d’entree
WO2006059978A1 (fr) 2004-12-01 2006-06-08 United Technologies Corporation Moteur a turbine de bout en porte-a-faux
US7883314B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
EP1825113B1 (fr) * 2004-12-01 2012-10-24 United Technologies Corporation Boîte de vitesses contre-rotative pour moteur à turbine en bout
EP1825114B1 (fr) 2004-12-01 2008-08-20 United Technologies Corporation Moteur de turbine a aube comprenant un echangeur thermique
US8807936B2 (en) 2004-12-01 2014-08-19 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
US7934902B2 (en) 2004-12-01 2011-05-03 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
US8757959B2 (en) 2004-12-01 2014-06-24 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
US9109537B2 (en) 2004-12-04 2015-08-18 United Technologies Corporation Tip turbine single plane mount
RU2293195C2 (ru) * 2005-01-17 2007-02-10 Ирина Федоровна Алавердова Газотурбинная энергоустановка
WO2007120161A2 (fr) * 2005-06-20 2007-10-25 Rolls-Royce North American Technologies, Inc. Séparateurs de particules pour des turbines à gaz
EP2466097A1 (fr) 2005-06-20 2012-06-20 Rolls-Royce North American Technologies, Inc. Sélecteur de particules avec entrée regroupée
EP1896157B1 (fr) * 2005-06-20 2012-05-02 Rolls-Royce North American Technologies, Inc. Séparateur de particules pour une turbine à gaz
US7581397B2 (en) * 2005-08-26 2009-09-01 Honeywell International Inc. Diffuser particle separator
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
EP2382026B1 (fr) * 2008-12-26 2017-08-23 Rolls-Royce North American Technologies, Inc. Système à filtre séparateur de particules pour turbine à gaz
CN101915164B (zh) * 2010-09-03 2012-09-05 中国航空动力机械研究所 一种燃气轮机进气粒子分离装置
US20120131900A1 (en) * 2010-11-30 2012-05-31 General Electric Company Inlet particle separator system
US8945254B2 (en) 2011-12-21 2015-02-03 General Electric Company Gas turbine engine particle separator
US20140144123A1 (en) * 2012-11-29 2014-05-29 Honeywell International Inc. Inlet particle separator system with air injection
US9541003B2 (en) 2013-02-23 2017-01-10 Rolls-Royce Corporation Air particle separator
US10100705B2 (en) * 2014-08-27 2018-10-16 Sikorsky Aircraft Corporation Exhaust mixer and method of making same
EP3067531B1 (fr) 2015-03-10 2020-05-06 Rolls-Royce North American Technologies, Inc. Séparateur de particules inertiel et contrôle de rebond particulaire
BR112018004079B1 (pt) * 2015-08-31 2023-03-07 Hitachi Energy Switzerland Ag Aparelho de extração de partícula
US10695704B2 (en) * 2016-07-20 2020-06-30 General Electric Company Multi-station debris separation system
US10393021B2 (en) 2016-09-01 2019-08-27 Rolls-Royce North American Technologies Inc. Particle separator
US10794402B2 (en) 2017-10-31 2020-10-06 General Electric Company Ejector and a turbo-machine having an ejector
US10738699B2 (en) 2018-01-19 2020-08-11 Rolls-Royce North American Technologies Inc. Air-inlet particle separator having a bleed surface

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE854879C (de) * 1947-10-11 1952-11-06 Jacques Bolsey Photographische Kamera
US3348379A (en) * 1963-09-25 1967-10-24 Rolls Royce Turbojet engine with compressor bypass and aft fan
GB1070458A (en) * 1964-06-12 1967-06-01 Boeing Co Separator for removing foreign matter from a gas stream
US3362155A (en) * 1965-03-29 1968-01-09 Gen Electric Axial flow separator
GB1195973A (en) * 1966-06-22 1970-06-24 Rolls Royce Air Intakes.
BE710709A (fr) * 1968-02-13 1968-06-17
US3832086A (en) * 1971-11-23 1974-08-27 Gen Electric Particle separator with scroll scavenging means
US3766719A (en) * 1971-11-26 1973-10-23 United Aircraft Corp Particle and moisture separator for engine inlet
US3811254A (en) * 1972-05-08 1974-05-21 United Aircraft Corp Engine air particle separator with fluid scavenge pump
US3979903A (en) * 1974-08-01 1976-09-14 General Electric Company Gas turbine engine with booster stage
US4002024A (en) * 1974-12-02 1977-01-11 General Electric Company Infrared suppression system for a gas turbine engine
GB1504793A (en) * 1975-02-14 1978-03-22 Rolls Royce Ducted fan gas turbine engine gas flow ducts
US4175384A (en) * 1977-08-02 1979-11-27 General Electric Company Individual bypass injector valves for a double bypass variable cycle turbofan engine
GB2007303B (en) * 1977-11-04 1982-04-07 Rolls Royce By-pass gas turbine engines
GB2044359B (en) * 1979-03-16 1982-10-27 Rolls Royce Gas turbine engine air intakes

Also Published As

Publication number Publication date
CA1136866A (fr) 1982-12-07
JPS5664122A (en) 1981-06-01
IT8024868A0 (it) 1980-09-24
US4265646A (en) 1981-05-05
FR2466617A1 (fr) 1981-04-10
GB2058929A (en) 1981-04-15
IT1133141B (it) 1986-07-09
DE3036525A1 (de) 1981-04-16

Similar Documents

Publication Publication Date Title
IL61028A0 (en) Foreign particle separator system for use in a gas turbine
GB2074655B (en) Particle separator for the inlet of a gas turbine engine
GB2152147B (en) Improvements in gas turbines
GB2049818B (en) Foreign particle separator
GB2177162B (en) Inlet particle separator for gas turbine engine
GB2050592B (en) Gas turbine
GB2100412B (en) Gas turbine fuel system
GB2043868B (en) Gas turbine
EP0081996A3 (en) Regenerative gas turbine cycle
DE3365942D1 (en) Exhaust duct for gas turbines
GB8313516D0 (en) Gas turbine engine
IL69290A0 (en) Improvements in gas turbine engines
EG14810A (en) Improved engine air particle separator for use with gas turbine engine
DE3462169D1 (en) Axial turbine for a turbo charger
GB2046843B (en) Gas turbine engines-de-icing-icing
DE3360573D1 (en) Combustor for gas turbine
GB2127105B (en) Improvements in cooled gas turbine engine aerofoils
GB2097865B (en) Power gas turbine
EP0081995A3 (en) Regenerative gas turbine cycle
GB8312111D0 (en) Prediffuser for gas turbine engine
JPS55160127A (en) Gas turbine
GB2015899B (en) Conditioning a particle-laden gas
ZA828482B (en) Combined gas and steam turbine process
GB2069053B (en) Water separator in gas turbine inlet
GB2044431B (en) Gas turbine