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
Other languages
English (en)
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 (de) 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 (de)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2552816A1 (fr) * 1983-10-03 1985-04-05 Nuovo Pignone Spa Systeme antigivrage pour une turbine a gaz
CN103628984A (zh) * 2013-12-06 2014-03-12 中国电力工程顾问集团西南电力设计院 一种燃机防冰冻装置的循环加热系统及其工作方法
EP2842872A1 (de) * 2013-09-03 2015-03-04 Hamilton Sundstrand Corporation Zapfluftsystem
EP2990335A1 (de) * 2014-08-26 2016-03-02 Rolls-Royce plc Gasturbinenmotorenteisungssystem
EP2900957A4 (de) * 2012-09-27 2016-04-27 United Technologies Corp Als kompressorstabilitäts-entlüftungsventil während des startens verwendetes gondelenteisungsventil
EP3115298A1 (de) * 2015-07-07 2017-01-11 United Technologies Corporation Gondelvereisungsschutzsystem und verfahren mit ausgeglichenem durchfluss
EP2685065A3 (de) * 2012-07-12 2018-03-07 Rolls-Royce plc Gasturbinenmotor

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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 (de) * 1982-04-03 1983-08-11 Dornier System Gmbh, 7990 Friedrichshafen Verfahren und Vorrichtung zur Temperaturregelung der von einer am Hochdruckausgang einer Verdichterstufe eines Strahltriebwerks ausgehenden Zapfluft
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 (fr) * 1993-06-03 1995-07-07 Snecma Système de dégivrage des parties avant d'une 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 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
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
GB0122672D0 (en) * 2001-09-20 2001-11-14 Honeywell Normalair Garrett Environmental control systems
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 (de) * 2003-12-30 2007-10-04 Airbus Deutschland Gmbh Vorrichtung und Verfahren zur Fußbodenheizung in einem Flugzeug
US7784739B2 (en) * 2004-05-26 2010-08-31 The Boeing Company Detection system and method for ice and other debris
FR2875542B1 (fr) * 2004-09-21 2009-02-13 Airbus France Sas Dispositif de protection contre le givrage pour moteurs d'aeronefs et procedes de degivrage associe
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
DE602005007201D1 (de) * 2005-07-01 2008-07-10 Saab Ab Vorrichtung und diese Vorrichtung enthaltendes Enteisungssystem für ein Luftfahrzeug
EP2140120A2 (de) * 2007-02-20 2010-01-06 AIRBUS France Verfahren zur herstellung einer schallbehandlungsbeschichtung mit einer zellularen struktur von komplexer form sowie in diesem verfahren hergestellte schallbehandlungsbeschichtung
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 (fr) * 2007-12-28 2010-04-23 Airbus France Ensemble propulsif d'aeronef comprenant des systemes de prelevement d'air chaud
DE102008007278B4 (de) * 2008-02-01 2010-04-08 Airbus Deutschland Gmbh Bleedairduct-Segment, Bleedairduct-Anordnung mit solchen Bleedairduct-Segmenten und Bleedairduct-System mit Regulierungsvorrichtung
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
US20100326041A1 (en) * 2009-06-30 2010-12-30 Wayne Garcia Edmondson Heated guide vane
US20100329836A1 (en) * 2009-06-30 2010-12-30 Wayne Garcia Edmondson Method of operating a heated guide vane assembly
DE102009055879A1 (de) 2009-11-26 2011-06-01 Rolls-Royce Deutschland Ltd & Co Kg Flugzeugenteisungsvorrichtung und Triebwerksgondel einer Fluggasturbine mit Enteisungsvorrichtung
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 (fr) * 2010-10-15 2013-06-14 Airbus Operations Sas Nacelle d'aeronef incorporant au moins une cloison radiale entre deux 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 (fr) * 2012-03-02 2014-02-28 Aircelle Sa Nacelle de turbomoteur equipe d'un echangeur de chaleur
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 (fr) * 2013-06-28 2015-07-31 Aircelle Sa Dispositif de degivrage et de conditionnement pour aeronef
GB2516648B (en) * 2013-07-29 2016-08-31 Charles Wells John Fitting for a gas turbine engine
US10618636B2 (en) 2014-03-04 2020-04-14 Parker-Hannifin Corporation Heat exchanger for laminar-flow aircraft
US10144520B2 (en) * 2014-04-14 2018-12-04 Rohr, Inc. De-icing system with thermal management
FR3021350B1 (fr) * 2014-05-20 2016-07-01 Snecma Procede de detection de fuite de fluide dans une turbomachine et systeme de distribution de fluide
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
US10513978B2 (en) 2016-05-02 2019-12-24 General Electric Company Directed flow nozzle swirl enhancer
US10189572B2 (en) * 2016-05-02 2019-01-29 The Boeing Company Systems and methods for preventing ice formation on portions of an aircraft
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
US10407164B2 (en) 2016-10-28 2019-09-10 Honeywell International Inc. Air distribution system with drag reducing inlet
US11242767B2 (en) * 2017-05-01 2022-02-08 General Electric Company Additively manufactured component including an impingement structure
GB201716499D0 (en) * 2017-10-09 2017-11-22 Rolls Royce Plc Gas turbine engine fireproofing
US11333438B2 (en) 2018-06-26 2022-05-17 Hamilton Sundstrand Corporation Heat exchanger with water extraction
US10995997B2 (en) 2018-06-26 2021-05-04 Hamilton Sunstrand Corporation Heat exchanger with integral features
FR3088961A1 (fr) * 2018-11-22 2020-05-29 Airbus Operations (S.A.S.) Turbomachine équipée d’un système de dégivrage de l’entrée d’air.
FR3089204B1 (fr) * 2018-11-29 2022-04-01 Safran Système de gestion d’air notamment pour pack de conditionnement d’air et dégivrage
US11326519B2 (en) 2020-02-25 2022-05-10 General Electric Company Frame for a heat engine
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
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
US11808281B2 (en) 2022-03-04 2023-11-07 General Electric Company Gas turbine engine with variable pitch inlet pre-swirl features
US11834995B2 (en) 2022-03-29 2023-12-05 General Electric Company Air-to-air heat exchanger potential in gas turbine engines
US11680530B1 (en) 2022-04-27 2023-06-20 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine
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
US11927134B1 (en) 2023-01-27 2024-03-12 General Electric Company Gas turbine engine having a heat exchanger located in an annular duct

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2552816A1 (fr) * 1983-10-03 1985-04-05 Nuovo Pignone Spa Systeme antigivrage pour une turbine a gaz
EP2685065A3 (de) * 2012-07-12 2018-03-07 Rolls-Royce plc Gasturbinenmotor
EP2900957A4 (de) * 2012-09-27 2016-04-27 United Technologies Corp Als kompressorstabilitäts-entlüftungsventil während des startens verwendetes gondelenteisungsventil
US9879599B2 (en) 2012-09-27 2018-01-30 United Technologies Corporation Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
EP2900957B1 (de) * 2012-09-27 2019-11-20 United Technologies Corporation Als kompressorstabilitäts-entlüftungsventil während des startens verwendetes gondelenteisungsventil
EP2842872A1 (de) * 2013-09-03 2015-03-04 Hamilton Sundstrand Corporation Zapfluftsystem
CN103628984A (zh) * 2013-12-06 2014-03-12 中国电力工程顾问集团西南电力设计院 一种燃机防冰冻装置的循环加热系统及其工作方法
CN103628984B (zh) * 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 一种燃机防冰冻装置的循环加热系统及其工作方法
EP2990335A1 (de) * 2014-08-26 2016-03-02 Rolls-Royce plc Gasturbinenmotorenteisungssystem
US9945247B2 (en) 2014-08-26 2018-04-17 Rolls-Royce Plc Gas turbine engine anti-icing system
EP3115298A1 (de) * 2015-07-07 2017-01-11 United Technologies Corporation Gondelvereisungsschutzsystem und verfahren mit ausgeglichenem durchfluss

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Publication number Publication date
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