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USB535928I5 - - Google Patents

Info

Publication number
USB535928I5
USB535928I5 US53592874A USB535928I5 US B535928 I5 USB535928 I5 US B535928I5 US 53592874 A US53592874 A US 53592874A US B535928 I5 USB535928 I5 US B535928I5
Authority
US
United States
Legal status (The legal status 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 status listed.)
Pending
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
Priority to US05/535,928 priority Critical patent/US3981466A/en
Publication of USB535928I5 publication Critical patent/USB535928I5/en
Application granted granted Critical
Publication of US3981466A publication Critical patent/US3981466A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F02C7/047—Heating to prevent icing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
US05/535,928 1974-12-23 1974-12-23 Integrated thermal anti-icing and environmental control system Expired - Lifetime US3981466A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US05/535,928 US3981466A (en) 1974-12-23 1974-12-23 Integrated thermal anti-icing and environmental control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/535,928 US3981466A (en) 1974-12-23 1974-12-23 Integrated thermal anti-icing and environmental control system

Publications (2)

Publication Number Publication Date
USB535928I5 true USB535928I5 (en) 1976-01-13
US3981466A US3981466A (en) 1976-09-21

Family

ID=24136386

Family Applications (1)

Application Number Title Priority Date Filing Date
US05/535,928 Expired - Lifetime US3981466A (en) 1974-12-23 1974-12-23 Integrated thermal anti-icing and environmental control system

Country Status (1)

Country Link
US (1) US3981466A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2552816A1 (en) * 1983-10-03 1985-04-05 Nuovo Pignone Spa ANTI-ICING SYSTEM FOR A GAS TURBINE
CN103628984A (en) * 2013-12-06 2014-03-12 中国电力工程顾问集团西南电力设计院 Loop heating system for gas turbine anti-freezing device and working method of loop heating system
EP2842872A1 (en) * 2013-09-03 2015-03-04 Hamilton Sundstrand Corporation Bleed air system
EP2990335A1 (en) * 2014-08-26 2016-03-02 Rolls-Royce plc Gas turbine engine anti-icing system
EP2900957A4 (en) * 2012-09-27 2016-04-27 United Technologies Corp Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
EP3115298A1 (en) * 2015-07-07 2017-01-11 United Technologies Corporation Nacelle anti-ice system and method with equalized flow
EP2685065A3 (en) * 2012-07-12 2018-03-07 Rolls-Royce plc A gas turbine engine

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US4240250A (en) * 1977-12-27 1980-12-23 The Boeing Company Noise reducing air inlet for gas turbine engines
US4482114A (en) * 1981-01-26 1984-11-13 The Boeing Company Integrated thermal anti-icing and environmental control system
US4406431A (en) * 1981-11-23 1983-09-27 Omac, Inc. Air scoop lip warmer de-icing system
DE3212575C1 (en) * 1982-04-03 1983-08-11 Dornier System Gmbh, 7990 Friedrichshafen Method and device for the temperature control of the bleed air leaving the high pressure outlet of a compressor stage of a jet engine
US4738416A (en) * 1986-09-26 1988-04-19 Quiet Nacelle Corporation Nacelle anti-icing system
US4782658A (en) * 1987-05-07 1988-11-08 Rolls-Royce Plc Deicing of a geared gas turbine engine
US4783026A (en) * 1987-05-22 1988-11-08 Avco Corporation Anti-icing management system
US4831819A (en) * 1987-07-02 1989-05-23 Avco Corporation Anti-icing valve
US5088277A (en) * 1988-10-03 1992-02-18 General Electric Company Aircraft engine inlet cowl anti-icing system
US5014933A (en) * 1989-04-27 1991-05-14 The Boeing Company Translating lip aircraft cowling structure adapted for noise reduction
US5050109A (en) * 1989-12-19 1991-09-17 The Boeing Company Method and apparatus for measuring the humidity of ambient air surrounding an aircraft in flight
US5114100A (en) * 1989-12-29 1992-05-19 The Boeing Company Anti-icing system for aircraft
US5161364A (en) * 1991-04-01 1992-11-10 United Technologies Corporation Control of aircraft bleed air stage mixing
FR2705996B1 (en) * 1993-06-03 1995-07-07 Snecma Defrosting system for the front parts of a turbomachine.
US5558303A (en) * 1994-12-27 1996-09-24 Koethe; Terence L. Method and apparatus for using hot fuels to de-ice aircraft
US5779196A (en) * 1995-12-08 1998-07-14 The Boeing Company Ram air drive laminar flow control system
FR2757823B1 (en) * 1996-12-26 1999-03-12 Aerospatiale LAMINARY FLOW TURBOREACTOR BASKET
US6179251B1 (en) * 1998-02-06 2001-01-30 Northrop Grumman Corporation Thin inlet lip design for low drag and reduced nacelle size
US6442944B1 (en) * 2000-10-26 2002-09-03 Lockheet Martin Corporation Bleed air heat exchanger integral to a jet engine
US20020172858A1 (en) * 2001-05-15 2002-11-21 Daniel Ashikian Thermo-dynamic battery storage unit
US6481210B1 (en) 2001-05-16 2002-11-19 Honeywell International, Inc. Smart surge bleed valve system and method
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GB0311663D0 (en) * 2003-05-21 2003-06-25 Rolls Royce Plc Aeroengine intake
US6990797B2 (en) * 2003-09-05 2006-01-31 General Electric Company Methods and apparatus for operating gas turbine engines
DE10361655B4 (en) * 2003-12-30 2007-10-04 Airbus Deutschland Gmbh Device and method for underfloor heating in an aircraft
US7784739B2 (en) * 2004-05-26 2010-08-31 The Boeing Company Detection system and method for ice and other debris
FR2875542B1 (en) * 2004-09-21 2009-02-13 Airbus France Sas DEVICE FOR PROTECTING AGAINST AIRCRAFT ENGINES AND METHODS OF DEFROSTING THE SAME
US7171819B2 (en) * 2005-01-21 2007-02-06 Honeywell International, Inc. Indirect regenerative air cycle for integrated power and cooling machines
US8366047B2 (en) * 2005-05-31 2013-02-05 United Technologies Corporation Electrothermal inlet ice protection system
US20070022732A1 (en) * 2005-06-22 2007-02-01 General Electric Company Methods and apparatus for operating gas turbine engines
ES2308384T3 (en) * 2005-07-01 2008-12-01 Saab Ab DEVICE AND ANTI-ICE SYSTEM FOR AIRCRAFT UNDERSTANDING SUCH DEVICE.
RU2455510C2 (en) * 2007-02-20 2012-07-10 Эрбюс Операсьон(Сас) Method to perform coating for acoustic treatment, including cellular structure of complex shape, and coating for acoustic treatment obtained thereof
US7708230B2 (en) * 2007-05-29 2010-05-04 United Technologies Corporation Flow distribution system for inlet flow control
US7874137B2 (en) * 2007-06-18 2011-01-25 Honeywell International Inc. Gas turbine engine anti-ice formation device and system
US7856824B2 (en) * 2007-06-25 2010-12-28 Honeywell International Inc. Cooling systems for use on aircraft
FR2925878B1 (en) * 2007-12-28 2010-04-23 Airbus France PROPELLANT AIRCRAFT ASSEMBLY COMPRISING HOT AIR COLLECTION SYSTEMS
DE102008007278B4 (en) * 2008-02-01 2010-04-08 Airbus Deutschland Gmbh Bleedairduct segment, Bleedairduct arrangement with such Bleedairduct segments and Bleedairduct system with regulation device
US8769924B2 (en) * 2008-05-30 2014-07-08 United Technologies Corporation Gas turbine engine assembly including accessory components within the nacelle
US8061657B2 (en) * 2008-12-31 2011-11-22 General Electric Company Method and apparatus for aircraft anti-icing
US20100329836A1 (en) * 2009-06-30 2010-12-30 Wayne Garcia Edmondson Method of operating a heated guide vane assembly
US20100326041A1 (en) * 2009-06-30 2010-12-30 Wayne Garcia Edmondson Heated guide vane
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US8382039B2 (en) * 2009-12-30 2013-02-26 MRA Systems Inc. Turbomachine nacelle and anti-icing system and method therefor
US9114877B2 (en) * 2010-08-30 2015-08-25 Ge Aviation Systems, Llc Method and system for vehicle thermal management
FR2966127B1 (en) * 2010-10-15 2013-06-14 Airbus Operations Sas AIRCRAFT NACELLE INCORPORATING AT LEAST ONE RADIAL PITCH BETWEEN TWO CONDUITS
US8397487B2 (en) 2011-02-28 2013-03-19 General Electric Company Environmental control system supply precooler bypass
WO2012125895A1 (en) * 2011-03-17 2012-09-20 Bombardier Inc. System and method for operating a precooler in an aircraft
US8444093B1 (en) * 2011-04-18 2013-05-21 Eran Epstein Airplane leading edge de-icing apparatus
US8463496B2 (en) 2011-07-06 2013-06-11 Hamilton Sundstrand Corporation Decoupling control architecture for pressure and flow controls in series
US9239005B2 (en) 2011-11-25 2016-01-19 Pratt & Whitney Canada Corp. Cooling system for engine and aircraft air
US9222411B2 (en) 2011-12-21 2015-12-29 General Electric Company Bleed air and hot section component cooling air system and method
US9109514B2 (en) * 2012-01-10 2015-08-18 Hamilton Sundstrand Corporation Air recovery system for precooler heat-exchanger
US8452516B1 (en) 2012-01-31 2013-05-28 United Technologies Corporation Variable vane scheduling based on flight conditions for inclement weather
FR2987602B1 (en) * 2012-03-02 2014-02-28 Aircelle Sa TURBOMOTEUR NACELLE EQUIPPED WITH A HEAT EXCHANGER
US20130327012A1 (en) * 2012-06-11 2013-12-12 General Electric Company Gas turbine anti-icing system
WO2014030024A1 (en) 2012-08-22 2014-02-27 Bombardier Inc. Pre-cooler system with bypass valve, controller therefor, method and aircraft using the same
US10385777B2 (en) * 2012-10-01 2019-08-20 United Technologies Corporation Bifurcated inlet scoop for gas turbine engine
US9187180B2 (en) * 2013-05-24 2015-11-17 Hamilton Sundstrand Corporation Thermal pneumatic deicing system for an aircraft RAM air heat exchanger
FR3007738B1 (en) * 2013-06-28 2015-07-31 Aircelle Sa DEFROSTING AND PACKAGING DEVICE FOR AIRCRAFT
GB2516648B (en) * 2013-07-29 2016-08-31 Charles Wells John Fitting for a gas turbine engine
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US10144520B2 (en) * 2014-04-14 2018-12-04 Rohr, Inc. De-icing system with thermal management
FR3021350B1 (en) * 2014-05-20 2016-07-01 Snecma METHOD FOR DETECTING FLUID LEAKAGE IN TURBOMACHINE AND FLUID DISPENSING SYSTEM
US10487690B2 (en) * 2014-08-18 2019-11-26 Rohr, Inc. Actively controlled cooling air exhaust door on an aircraft engine nacelle
GB201416928D0 (en) * 2014-09-25 2014-11-12 Rolls Royce Plc A gas turbine and a method of washing a gas turbine engine
US10421551B2 (en) * 2014-12-15 2019-09-24 United Technologies Corporation Aircraft anti-icing system
US10100733B2 (en) * 2015-07-31 2018-10-16 Ge Aviation Systems Llc Turbine engine with anti-ice valve assembly, bleed air valve, and method of operating
US10393020B2 (en) * 2015-08-26 2019-08-27 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
US10017262B2 (en) * 2015-09-22 2018-07-10 Rohr, Inc. Pulsed deicing system
US11473497B2 (en) * 2016-03-15 2022-10-18 Hamilton Sundstrand Corporation Engine bleed system with motorized compressor
US10450954B2 (en) 2016-03-17 2019-10-22 General Electric Company Internally heated engine inlet screen for aircraft engines
US10239626B2 (en) * 2016-03-29 2019-03-26 Gulfstream Aerospace Corporation Arrangements and methods for supplying heated air to a wing anti-icing system
US10189572B2 (en) * 2016-05-02 2019-01-29 The Boeing Company Systems and methods for preventing ice formation on portions of an aircraft
US10513978B2 (en) 2016-05-02 2019-12-24 General Electric Company Directed flow nozzle swirl enhancer
US10267334B2 (en) * 2016-08-01 2019-04-23 United Technologies Corporation Annular heatshield
US10708979B2 (en) 2016-10-07 2020-07-07 De-Ice Technologies Heating a bulk medium
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US11242767B2 (en) * 2017-05-01 2022-02-08 General Electric Company Additively manufactured component including an impingement structure
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FR3089204B1 (en) * 2018-11-29 2022-04-01 Safran Air management system in particular for air conditioning and defrosting pack
US11255264B2 (en) 2020-02-25 2022-02-22 General Electric Company Frame for a heat engine
US11560843B2 (en) * 2020-02-25 2023-01-24 General Electric Company Frame for a heat engine
US11326519B2 (en) 2020-02-25 2022-05-10 General Electric Company Frame for a heat engine
US12123350B2 (en) 2021-03-02 2024-10-22 General Electric Company Three-stream engine having a heat exchanger
US11965697B2 (en) 2021-03-02 2024-04-23 General Electric Company Multi-fluid heat exchanger
US11788465B2 (en) 2022-01-19 2023-10-17 General Electric Company Bleed flow assembly for a gas turbine engine
US12116929B2 (en) 2022-01-19 2024-10-15 General Electric Company Bleed flow assembly for a gas turbine engine
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US11834992B2 (en) 2022-04-27 2023-12-05 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
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US12060829B2 (en) 2022-04-27 2024-08-13 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2552816A1 (en) * 1983-10-03 1985-04-05 Nuovo Pignone Spa ANTI-ICING SYSTEM FOR A GAS TURBINE
EP2685065A3 (en) * 2012-07-12 2018-03-07 Rolls-Royce plc A gas turbine engine
EP2900957A4 (en) * 2012-09-27 2016-04-27 United Technologies Corp Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
US9879599B2 (en) 2012-09-27 2018-01-30 United Technologies Corporation Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
EP2900957B1 (en) * 2012-09-27 2019-11-20 United Technologies Corporation Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
EP2842872A1 (en) * 2013-09-03 2015-03-04 Hamilton Sundstrand Corporation Bleed air system
CN103628984A (en) * 2013-12-06 2014-03-12 中国电力工程顾问集团西南电力设计院 Loop heating system for gas turbine anti-freezing device and working method of loop heating system
CN103628984B (en) * 2013-12-06 2015-07-08 中国电力工程顾问集团西南电力设计院有限公司 Loop heating system for gas turbine anti-freezing device and working method of loop heating system
EP2990335A1 (en) * 2014-08-26 2016-03-02 Rolls-Royce plc Gas turbine engine anti-icing system
US9945247B2 (en) 2014-08-26 2018-04-17 Rolls-Royce Plc Gas turbine engine anti-icing system
EP3115298A1 (en) * 2015-07-07 2017-01-11 United Technologies Corporation Nacelle anti-ice system and method with equalized flow

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