BE692882A - - Google Patents

Info

Publication number
BE692882A
BE692882A BE692882DA BE692882A BE 692882 A BE692882 A BE 692882A BE 692882D A BE692882D A BE 692882DA BE 692882 A BE692882 A BE 692882A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE692882A publication Critical patent/BE692882A/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
    • 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
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Separation Using Semi-Permeable Membranes (AREA)
BE692882D 1966-02-01 1967-01-19 BE692882A (th)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US524101A US3338049A (en) 1966-02-01 1966-02-01 Gas turbine engine including separator for removing extraneous matter

Publications (1)

Publication Number Publication Date
BE692882A true BE692882A (th) 1967-07-03

Family

ID=24087767

Family Applications (1)

Application Number Title Priority Date Filing Date
BE692882D BE692882A (th) 1966-02-01 1967-01-19

Country Status (5)

Country Link
US (1) US3338049A (th)
BE (1) BE692882A (th)
DE (1) DE1601549A1 (th)
FR (1) FR1508698A (th)
GB (1) GB1139472A (th)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2554507A1 (fr) * 1983-11-03 1985-05-10 Gen Electric Admission d'air dans un moteur d'avion equipee d'un separateur de corps etrangers

Families Citing this family (51)

* Cited by examiner, † Cited by third party
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US3465950A (en) * 1968-01-22 1969-09-09 Gen Electric Separator
DE1751550C3 (de) * 1968-06-18 1975-04-17 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Dichtung zwischen dem Einlauf eines Strahltriebwerkes und einem zellenfesten Aufnahmering des Einlaufgehäuses
US3766719A (en) * 1971-11-26 1973-10-23 United Aircraft Corp Particle and moisture separator for engine inlet
US4004760A (en) * 1975-03-25 1977-01-25 Mitsubishi Jukogyo Kabushiki Kaisha Device for preventing foreign matters from being sucked into a gas turbine engine for an aircraft
US4185373A (en) * 1977-10-25 1980-01-29 General Dynamics Corporation Method of manufacturing an inflatable air inlet duct
US4250703A (en) * 1979-03-15 1981-02-17 Avco Corporation Swinging door particle separator and deicing system
GB2069053B (en) * 1980-02-09 1983-04-13 Rolls Royce Water separator in gas turbine inlet
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
US4617028A (en) * 1983-11-03 1986-10-14 General Electric Company Aircraft engine air intake including a foreign object separator
US4798047A (en) * 1983-12-19 1989-01-17 Elliott Turbomachinery Co., Inc. Particulate collection and cooling in a turbomachine
GB2196390B (en) * 1986-10-16 1991-06-26 Rolls Royce Plc Intake for turbopropeller gas turbine engine.
DE3742841A1 (de) * 1987-12-17 1989-07-13 Kloeckner Humboldt Deutz Ag Geblaese
US4928480A (en) * 1988-03-04 1990-05-29 General Electric Company Separator having multiple particle extraction passageways
US5033693A (en) * 1988-12-14 1991-07-23 The Boeing Company Single-piece, flexible inlet ramp
US4972672A (en) * 1989-09-28 1990-11-27 Pratt & Whitney Canada, Inc. Controlled bypass inlet duct
GB9018457D0 (en) * 1990-08-22 1990-10-03 Rolls Royce Plc Flow control means
DE4305688C2 (de) * 1993-02-25 1994-04-21 Voith Gmbh J M Vorrichtung und Verfahren zur Veränderung des Durchflußwiderstandes einer Drosselvorrichtung für fluide Strömungen
US6533541B1 (en) * 2001-12-04 2003-03-18 Honeywell International, Inc. High energy particle arrestor for air turbine starters
US6702873B2 (en) * 2002-04-23 2004-03-09 The Boeing Company High particle separation efficiency system
DE20207549U1 (de) * 2002-05-08 2002-08-29 Berbel Ablufttechnik GmbH, 48496 Hopsten Vorrichtung zum wirkungsvollen Abscheiden von Schwebteilchen aus einem Luftstrom
US7581397B2 (en) * 2005-08-26 2009-09-01 Honeywell International Inc. Diffuser particle separator
GB0617769D0 (en) * 2006-09-09 2006-10-18 Rolls Royce Plc An engine
US7802433B2 (en) * 2006-09-27 2010-09-28 General Electric Company Adaptive inertial particle separators and methods of use
US7927408B2 (en) * 2007-11-30 2011-04-19 Honeywell International Inc. Inlet particle separator systems and methods
US8986253B2 (en) 2008-01-25 2015-03-24 Tandem Diabetes Care, Inc. Two chamber pumps and related methods
FR2933443B1 (fr) * 2008-07-02 2013-10-11 Snecma Pointe d'un compresseur de turbomachine comprenant des moyens de degivrage
US8408421B2 (en) 2008-09-16 2013-04-02 Tandem Diabetes Care, Inc. Flow regulating stopcocks and related methods
AU2009293019A1 (en) 2008-09-19 2010-03-25 Tandem Diabetes Care Inc. Solute concentration measurement device and related methods
GB2466298A (en) * 2008-12-22 2010-06-23 Rolls Royce Plc Sealing method and apparatus
US7871455B1 (en) * 2009-06-19 2011-01-18 Vintage Capital Group, Llc Jet engine protection system
WO2011014704A2 (en) 2009-07-30 2011-02-03 Tandem Diabetes Care, Inc. Infusion pump system with disposable cartridge having pressure venting and pressure feedback
US8961111B2 (en) 2012-01-03 2015-02-24 General Electric Company Turbine and method for separating particulates from a fluid
US9180242B2 (en) 2012-05-17 2015-11-10 Tandem Diabetes Care, Inc. Methods and devices for multiple fluid transfer
US20140144123A1 (en) * 2012-11-29 2014-05-29 Honeywell International Inc. Inlet particle separator system with air injection
US9173998B2 (en) 2013-03-14 2015-11-03 Tandem Diabetes Care, Inc. System and method for detecting occlusions in an infusion pump
US9656760B2 (en) 2013-11-07 2017-05-23 Sikorsky Aircraft Corporation Variable geometry helicopter engine inlet
US9212606B2 (en) * 2013-12-24 2015-12-15 Khalid Hamad Mutleb ALNAFISAH Bird strike prevention device for jet engine, and airplane incorporating the same
US9869250B2 (en) 2014-05-20 2018-01-16 United Technologies Corporation Particle tolerant turboshaft engine
US10323573B2 (en) 2014-07-31 2019-06-18 United Technologies Corporation Air-driven particle pulverizer for gas turbine engine cooling fluid system
EP3001021B1 (en) 2014-09-25 2020-06-24 United Technologies Corporation Hail screen in the inlet of a conduit to a heat exhanger of an aircraft engine
EP3067532B1 (en) * 2015-03-11 2020-12-16 Rolls-Royce North American Technologies, Inc. Adaptable inertial particle separator for a gas turbine engine intake
FR3044357B1 (fr) * 2015-11-27 2020-06-05 Safran Aircraft Engines Turbomachine comprenant un piege de corps etrangers circulant dans un flux d'air
US10723474B2 (en) 2017-05-24 2020-07-28 Sikorsky Aircraft Corporation Variable geometry engine inlet for high speed aircraft
FR3069291B1 (fr) * 2017-07-24 2019-12-13 Safran Aircraft Engines Conduit d'alimentation d'un compresseur d'une turbomachine
US10738699B2 (en) * 2018-01-19 2020-08-11 Rolls-Royce North American Technologies Inc. Air-inlet particle separator having a bleed surface
US10767559B2 (en) * 2018-03-29 2020-09-08 Rolls-Royce North American Technologies Inc. Adaptive-area inertial particle separators
US11047305B2 (en) * 2018-04-12 2021-06-29 Stephanie Fraser-Beekman Debris deflector for a jet engine
US11261788B2 (en) 2019-03-15 2022-03-01 Honeywell International Inc. Systems and methods for dry fog inlet particle separator
US11834988B1 (en) 2022-06-15 2023-12-05 Rolls-Royce North American Technologies Inc. Turbine engine inertial particle separator with particle rebound suppression
US11964223B1 (en) * 2022-10-15 2024-04-23 Beta Air, Llc Methods and apparatus for an inertial separation of air in an electric aircraft

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2636666A (en) * 1947-08-20 1953-04-28 Rolls Royce Gas turbine engine with de-icing apparatus
US2966028A (en) * 1947-10-17 1960-12-27 Gen Electric Aerodynamic diffuser mechanisms
US2755044A (en) * 1950-05-25 1956-07-17 United Aircraft Corp De-icing arrangements for engine cooling systems
US2763426A (en) * 1952-05-22 1956-09-18 John R Erwin Means for varying the quantity characteristics of supersonic compressors
US2838227A (en) * 1953-12-23 1958-06-10 Armstrong Siddeley Motors Ltd Preventing or reducing stalling of the early rows of axial-flow compressor blades ofgas turbine engines
US2944731A (en) * 1956-05-17 1960-07-12 Lockheed Aircraft Corp Debris traps for engine-air inlets
US3148043A (en) * 1962-03-29 1964-09-08 Boeing Co Moisture and particle removing means for engines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2554507A1 (fr) * 1983-11-03 1985-05-10 Gen Electric Admission d'air dans un moteur d'avion equipee d'un separateur de corps etrangers

Also Published As

Publication number Publication date
US3338049A (en) 1967-08-29
DE1601549A1 (de) 1971-01-07
FR1508698A (fr) 1968-01-05
GB1139472A (en) 1969-01-08

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