IT8024868A0 - Sistema separatore di particelle estranee. - Google Patents

Sistema separatore di particelle estranee.

Info

Publication number
IT8024868A0
IT8024868A0 IT8024868A IT2486880A IT8024868A0 IT 8024868 A0 IT8024868 A0 IT 8024868A0 IT 8024868 A IT8024868 A IT 8024868A IT 2486880 A IT2486880 A IT 2486880A IT 8024868 A0 IT8024868 A0 IT 8024868A0
Authority
IT
Italy
Prior art keywords
particle separator
separator system
foreign particle
foreign
separator
Prior art date
Application number
IT8024868A
Other languages
English (en)
Other versions
IT1133141B (it
Inventor
Barry Weinstein
William Steyer
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 IT8024868A0 publication Critical patent/IT8024868A0/it
Application granted granted Critical
Publication of IT1133141B publication Critical patent/IT1133141B/it

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)
  • Separating Particles In Gases By Inertia (AREA)
  • Cyclones (AREA)
IT24868/80A 1979-10-01 1980-09-24 Sistema separatore di particelle estranee IT1133141B (it)

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 (2)

Publication Number Publication Date
IT8024868A0 true IT8024868A0 (it) 1980-09-24
IT1133141B IT1133141B (it) 1986-07-09

Family

ID=22160062

Family Applications (1)

Application Number Title Priority Date Filing Date
IT24868/80A IT1133141B (it) 1979-10-01 1980-09-24 Sistema separatore di particelle estranee

Country Status (8)

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

Families Citing this family (74)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
AU3434401A (en) * 1999-11-23 2001-06-04 Marina Ellen Marinella Pavlatos Engine with upstream and rotationally attached guard
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
DE10162238A1 (de) * 2001-12-18 2003-07-10 Rolls Royce Deutschland Lufteinlasssystem eines PTL-Antriebs
US9003759B2 (en) 2004-12-01 2015-04-14 United Technologies Corporation Particle separator for tip turbine engine
WO2006059974A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Close coupled gearbox assembly for a tip turbine engine
WO2006110125A2 (en) * 2004-12-01 2006-10-19 United Technologies Corporation Stacked annular components for turbine engines
EP1825112B1 (en) 2004-12-01 2013-10-23 United Technologies Corporation Cantilevered tip turbine engine
WO2006060001A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Fan rotor assembly for a tip turbine engine
WO2006059977A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and corresponding orepating method
US20090148273A1 (en) * 2004-12-01 2009-06-11 Suciu Gabriel L Compressor inlet guide vane for tip turbine engine and corresponding control method
EP1831530B1 (en) 2004-12-01 2009-02-25 United Technologies Corporation Compressor variable stage remote actuation for turbine engine
WO2006060013A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Seal assembly for a fan rotor of a tip turbine engine
WO2006059980A2 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Diffuser aspiration for a tip turbine engine
US7845157B2 (en) 2004-12-01 2010-12-07 United Technologies Corporation Axial compressor for tip turbine engine
US7631485B2 (en) 2004-12-01 2009-12-15 United Technologies Corporation Tip turbine engine with a heat exchanger
EP1825116A2 (en) * 2004-12-01 2007-08-29 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
WO2006059969A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Counter-rotating compressor case and assembly method for tip turbine engine
US7976273B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Tip turbine engine support structure
US7937927B2 (en) 2004-12-01 2011-05-10 United Technologies Corporation Counter-rotating gearbox for tip turbine engine
WO2006059971A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine integral fan, combustor, and turbine case
WO2006059970A2 (en) 2004-12-01 2006-06-08 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
EP1834076B1 (en) 2004-12-01 2011-04-06 United Technologies Corporation Turbine blade cluster for a fan-turbine rotor assembly and method of mounting such a cluster
US8104257B2 (en) * 2004-12-01 2012-01-31 United Technologies Corporation Tip turbine engine with multiple fan and turbine stages
EP2333287A1 (en) * 2004-12-01 2011-06-15 United Technologies Corporation Vectoring transition duct for turbine engine
WO2006112807A2 (en) 2004-12-01 2006-10-26 United Technologies Corporation Turbine engine and method for starting a turbine engine
US8365511B2 (en) 2004-12-01 2013-02-05 United Technologies Corporation Tip turbine engine integral case, vane, mount and mixer
WO2006060006A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine non-metallic tailcone
DE602004031679D1 (de) 2004-12-01 2011-04-14 United Technologies Corp Regenerative Kühlung einer Leit- und Laufschaufel für ein Tipturbinentriebwerk
EP1831521B1 (en) 2004-12-01 2008-08-20 United Technologies Corporation Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
WO2006060004A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Combustor for turbine engine
US8807936B2 (en) 2004-12-01 2014-08-19 United Technologies Corporation Balanced turbine rotor fan blade for a tip turbine engine
DE602004027766D1 (de) 2004-12-01 2010-07-29 United Technologies Corp Hydraulische dichtung für ein getriebe eines spitzenturbinenmotors
EP1825170B1 (en) 2004-12-01 2009-03-18 United Technologies Corporation Gearbox lubrication supply system for a tip turbine engine
US7976272B2 (en) 2004-12-01 2011-07-12 United Technologies Corporation Inflatable bleed valve for a turbine engine
WO2006060011A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine comprising a nonrotable compartment
WO2006059986A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine and operating method with reverse core airflow
US7887296B2 (en) 2004-12-01 2011-02-15 United Technologies Corporation Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
EP1828545A2 (en) 2004-12-01 2007-09-05 United Technologies Corporation Annular turbine ring rotor
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
US7631480B2 (en) 2004-12-01 2009-12-15 United Technologies Corporation Modular tip turbine engine
EP1834067B1 (en) 2004-12-01 2008-11-26 United Technologies Corporation Fan blade assembly for a tip turbine engine and method of assembly
WO2006060014A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Starter generator system for a tip turbine engine
EP1828591B1 (en) * 2004-12-01 2010-07-21 United Technologies Corporation Peripheral combustor for tip turbine engine
US7883314B2 (en) 2004-12-01 2011-02-08 United Technologies Corporation Seal assembly for a fan-turbine rotor of a tip turbine engine
US9109537B2 (en) 2004-12-04 2015-08-18 United Technologies Corporation Tip turbine single plane mount
EP1896157B1 (en) * 2005-06-20 2012-05-02 Rolls-Royce North American Technologies, Inc. Particle separator for a gas turbine engine
EP1893862B1 (en) * 2005-06-20 2014-05-21 Rolls-Royce North American Technologies, Inc. Particle separators for gas turbine engines
WO2007002021A2 (en) 2005-06-20 2007-01-04 Rolls-Royce North American Technologies, Inc. Clustered inlet particle separator
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
US9046056B2 (en) * 2008-12-26 2015-06-02 Rolls-Royce North American Technologies, Inc. Inlet particle separator system for a gas turbine engine
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 (en) 2015-03-10 2020-05-06 Rolls-Royce North American Technologies, Inc. Inertial particle separator and particle bounce control
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 (it) * 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
FR2466617A1 (fr) 1981-04-10
IL61028A0 (en) 1980-11-30
DE3036525A1 (de) 1981-04-16
JPS5664122A (en) 1981-06-01
IT1133141B (it) 1986-07-09
CA1136866A (en) 1982-12-07
US4265646A (en) 1981-05-05
GB2058929A (en) 1981-04-15

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