ES2391115T3 - Sistemas y métodos para dirigir de forma pasiva los flujos de tobera de motor de un avión - Google Patents

Sistemas y métodos para dirigir de forma pasiva los flujos de tobera de motor de un avión Download PDF

Info

Publication number
ES2391115T3
ES2391115T3 ES07122560T ES07122560T ES2391115T3 ES 2391115 T3 ES2391115 T3 ES 2391115T3 ES 07122560 T ES07122560 T ES 07122560T ES 07122560 T ES07122560 T ES 07122560T ES 2391115 T3 ES2391115 T3 ES 2391115T3
Authority
ES
Spain
Prior art keywords
flow path
flow
nozzle
wall
engine
Prior art date
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.)
Active
Application number
ES07122560T
Other languages
English (en)
Spanish (es)
Inventor
Stanley F. Birch
Dmitriy A. Lyubimov
Vladimir P. Maslov
Alexandr N. Secundov
Konstantin M. Khritov
Aleksey K. Mironov
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ES2391115T3 publication Critical patent/ES2391115T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/34Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for attenuating noise
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00Power-plant nacelles, fairings or cowlings
    • B64D29/02Power-plant nacelles, fairings or cowlings associated with wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/30Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet
    • F02K1/386Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/13Two-dimensional trapezoidal
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/17Purpose of the control system to control boundary layer
    • F05D2270/173Purpose of the control system to control boundary layer by the Coanda effect
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)
ES07122560T 2006-12-06 2007-12-06 Sistemas y métodos para dirigir de forma pasiva los flujos de tobera de motor de un avión Active ES2391115T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US635737 2006-12-06
US11/635,737 US7870722B2 (en) 2006-12-06 2006-12-06 Systems and methods for passively directing aircraft engine nozzle flows

Publications (1)

Publication Number Publication Date
ES2391115T3 true ES2391115T3 (es) 2012-11-21

Family

ID=39144413

Family Applications (1)

Application Number Title Priority Date Filing Date
ES07122560T Active ES2391115T3 (es) 2006-12-06 2007-12-06 Sistemas y métodos para dirigir de forma pasiva los flujos de tobera de motor de un avión

Country Status (5)

Country Link
US (2) US7870722B2 (enExample)
EP (1) EP1936172B1 (enExample)
JP (1) JP5241215B2 (enExample)
CN (1) CN101200220B (enExample)
ES (1) ES2391115T3 (enExample)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090261206A1 (en) * 2005-01-21 2009-10-22 Alvi Farrukh S Method of using microjet actuators for the control of flow separation and distortion
US7966824B2 (en) * 2006-08-09 2011-06-28 The Boeing Company Jet engine nozzle exit configurations and associated systems and methods
US8157207B2 (en) * 2006-08-09 2012-04-17 The Boeing Company Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods
US7870722B2 (en) * 2006-12-06 2011-01-18 The Boeing Company Systems and methods for passively directing aircraft engine nozzle flows
US7966826B2 (en) * 2007-02-14 2011-06-28 The Boeing Company Systems and methods for reducing noise from jet engine exhaust
US9494084B2 (en) * 2007-08-23 2016-11-15 United Technologies Corporation Gas turbine engine with fan variable area nozzle for low fan pressure ratio
US10167813B2 (en) 2007-08-23 2019-01-01 United Technologies Corporation Gas turbine engine with fan variable area nozzle to reduce fan instability
US9701415B2 (en) 2007-08-23 2017-07-11 United Technologies Corporation Gas turbine engine with axial movable fan variable area nozzle
FR2929334B1 (fr) * 2008-03-31 2012-06-01 Airbus France Dispositif de reduction du bruit genere par reacteur d'aeronef a conduits de fluide coudes
FR2929336B1 (fr) * 2008-03-31 2012-06-01 Airbus France Dispositif a jets plans de reduction du bruit genere par un reacteur d'aeronef
FR2929335B1 (fr) * 2008-03-31 2012-06-01 Airbus France Dispositif de reduction du bruit genere par un reacteur d'aeronef a jets de fluide de meme orientation
FR2929337B1 (fr) * 2008-03-31 2012-06-01 Airbus France Dispositif a jets secondaires de reduction du bruit genere par un reacteur d'aeronef
US8087250B2 (en) * 2008-06-26 2012-01-03 General Electric Company Duplex tab exhaust nozzle
FR2934009B1 (fr) * 2008-07-21 2010-09-03 Ge Energy Products France Snc Diffuseur d'echappement pour turbine a gaz
US9885313B2 (en) 2009-03-17 2018-02-06 United Technologes Corporation Gas turbine engine bifurcation located fan variable area nozzle
US8714919B2 (en) * 2009-11-06 2014-05-06 Raytheon Company Inlet and exhaust system
GB201007215D0 (en) 2010-04-30 2010-06-16 Rolls Royce Plc Gas turbine engine
GB201016455D0 (en) 2010-09-30 2010-11-17 Imp Innovations Ltd Fluid flow modification
FR2971553B1 (fr) * 2011-02-10 2015-05-29 Eads Europ Aeronautic Defence Reacteur a signature acoustique reduite
FR2978989B1 (fr) * 2011-08-12 2013-07-26 Aircelle Sa Cone d'ejection pour turboreacteur d'aeronef
EP2696040B1 (de) * 2012-08-09 2017-03-15 MTU Aero Engines AG Strömungsleitanordnung zur Kühlung des Niederdruckturbinengehäuses eines Gasturbinenstrahltriebwerk
GB201220378D0 (en) * 2012-11-13 2012-12-26 Rolls Royce Plc A gas turbine engine exhaust nozzle
JP6183837B2 (ja) 2013-08-19 2017-08-23 国立研究開発法人宇宙航空研究開発機構 排気ノズル
FR3016863B1 (fr) * 2014-01-29 2017-05-26 Snecma Nacelle pour turboreacteur d'avion
US10094332B2 (en) 2014-09-03 2018-10-09 The Boeing Company Core cowl for a turbofan engine
CN107636289A (zh) * 2015-03-26 2018-01-26 赛峰飞机发动机公司 具有用于微射流的格栅以降低涡轮发动机的喷射噪声的装置
US10711702B2 (en) * 2015-08-18 2020-07-14 General Electric Company Mixed flow turbocore
US10563613B2 (en) 2015-08-31 2020-02-18 Rolls-Royce North American Technologies Inc. Coanda device for a round exhaust nozzle
US11248526B2 (en) 2016-09-08 2022-02-15 Unison Industries, Llc Fan casing assembly and method
CN108019295B (zh) * 2017-12-15 2021-03-30 中国航发沈阳发动机研究所 一种航空发动机扰流降噪装置
GB201820936D0 (en) * 2018-12-21 2019-02-06 Rolls Royce Plc Low noise gas turbine engine
US11440671B2 (en) * 2019-01-24 2022-09-13 Amazon Technologies, Inc. Adjustable motor fairings for aerial vehicles
FR3095241B1 (fr) * 2019-04-17 2021-06-25 Safran Aircraft Engines Entrée d’air de nacelle de turboréacteur comprenant une conduite de circulation pour favoriser une phase d’inversion de poussée
CA3145745A1 (en) * 2019-07-01 2021-01-07 Chuanrui ZHANG Aerodynamic techniques and methods for quieter supersonic flight
JP7297574B2 (ja) * 2019-07-12 2023-06-26 三菱重工業株式会社 ガスタービンシステムおよびそれを備えた移動体

Family Cites Families (55)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1127659A (en) 1966-09-16 1968-09-18 Rolls Royce Improvements in gas turbine engines
US3568792A (en) * 1969-06-18 1971-03-09 Rohr Corp Sound-suppressing and thrust-reversing apparatus
FR2091911B1 (enExample) 1970-04-21 1974-03-01 Snecma
US3648800A (en) 1970-04-27 1972-03-14 Gen Electric Coanda expansion exhaust nozzle suppressor
FR2126922B1 (enExample) * 1971-01-20 1975-01-17 Snecma
US4043522A (en) 1975-12-22 1977-08-23 The Boeing Company Common pod for housing a plurality of different turbofan jet propulsion engines
US4372110A (en) 1976-02-13 1983-02-08 Nasa Noise suppressor for turbo fan jet engines
US4215536A (en) 1978-12-26 1980-08-05 The Boeing Company Gas turbine mixer apparatus
GB2104967B (en) 1981-09-03 1985-07-17 Rolls Royce Exhaust mixer for turbofan aeroengine
US4501393A (en) * 1982-03-17 1985-02-26 The Boeing Company Internally ventilated noise suppressor with large plug nozzle
US4819425A (en) 1982-03-18 1989-04-11 The Boeing Company Primary-secondary ventilated flow mixer nozzle for high bypass turbo fan jet propulsion system
GB2146702B (en) 1983-09-14 1987-12-23 Rolls Royce Exhaust mixer for turbofan aeroengine
GB2149456B (en) 1983-11-08 1987-07-29 Rolls Royce Exhaust mixing in turbofan aeroengines
GB2207468A (en) 1987-06-01 1989-02-01 Secr Defence Vortex silencing in gas turbine engines
US5117628A (en) * 1990-01-25 1992-06-02 General Electric Company Mixed flow augmentor pre-mixer
US5884472A (en) 1995-10-11 1999-03-23 Stage Iii Technologies, L.C. Alternating lobed mixer/ejector concept suppressor
US5924632A (en) 1996-05-02 1999-07-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Jet nozzle having centerbody for enhanced exit area mixing
US6082635A (en) 1996-06-12 2000-07-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Undulated nozzle for enhanced exit area mixing
US5947412A (en) 1997-01-10 1999-09-07 Titan Corporation Jet engine noise suppressor assembly
US6360528B1 (en) 1997-10-31 2002-03-26 General Electric Company Chevron exhaust nozzle for a gas turbine engine
US6314721B1 (en) 1998-09-04 2001-11-13 United Technologies Corporation Tabbed nozzle for jet noise suppression
EP1076765B1 (de) 1999-03-05 2006-06-14 Rolls-Royce Deutschland Ltd & Co KG Blütenmischer für ein zweikreis-strahltriebwerk
US6612106B2 (en) 2000-05-05 2003-09-02 The Boeing Company Segmented mixing device having chevrons for exhaust noise reduction in jet engines
US7159383B2 (en) 2000-10-02 2007-01-09 Rohr, Inc. Apparatus, method and system for gas turbine engine noise reduction
US6640537B2 (en) 2000-12-18 2003-11-04 Pratt & Whitney Canada Corp. Aero-engine exhaust jet noise reduction assembly
US6837456B1 (en) 2001-01-10 2005-01-04 Florida State University Research Foundation Microjet based control system
GB0105349D0 (en) * 2001-03-03 2001-04-18 Rolls Royce Plc Gas turbine engine exhaust nozzle
US6532729B2 (en) 2001-05-31 2003-03-18 General Electric Company Shelf truncated chevron exhaust nozzle for reduction of exhaust noise and infrared (IR) signature
DE10145489B4 (de) * 2001-09-14 2008-11-06 Mtu Aero Engines Gmbh Anordnung zum Vermischen von zwei ursprünglich getrennt geführten Fluidströmen in einem Zweikreis-Strahltriebwerk
BR0213262B1 (pt) 2001-10-23 2011-05-31 tubeira de exaustão variável confluente.
CA2476503C (en) 2002-02-22 2011-05-24 The Nordam Group, Inc. Duplex mixer exhaust nozzle
US6658839B2 (en) 2002-02-28 2003-12-09 The Boeing Company Convergent/divergent segmented exhaust nozzle
GB0205701D0 (en) 2002-03-12 2002-04-24 Rolls Royce Plc Variable area nozzle
US7293401B2 (en) * 2002-03-20 2007-11-13 The Regents Of The University Of California Jet engine noise suppressor
US6983912B2 (en) 2002-04-30 2006-01-10 The Boeing Company Hybrid exhaust heat shield for pylon mounted gas turbine engines
US6718752B2 (en) 2002-05-29 2004-04-13 The Boeing Company Deployable segmented exhaust nozzle for a jet engine
GB0226228D0 (en) 2002-11-09 2002-12-18 Rolls Royce Plc Suppression of part of the noise from a gas turbine engine
US6969028B2 (en) * 2003-01-22 2005-11-29 The Boeing Company Scarf nozzle for a jet engine and method of using the same
US7010905B2 (en) 2003-02-21 2006-03-14 The Nordam Group, Inc. Ventilated confluent exhaust nozzle
US6971229B2 (en) 2003-02-26 2005-12-06 The Nordam Group, Inc. Confluent exhaust nozzle
US7055329B2 (en) 2003-03-31 2006-06-06 General Electric Company Method and apparatus for noise attenuation for gas turbine engines using at least one synthetic jet actuator for injecting air
FR2855558B1 (fr) 2003-05-28 2005-07-15 Snecma Moteurs Tuyere de turbomachine a reduction de bruit
FR2857416B1 (fr) 2003-07-09 2007-05-25 Snecma Moteurs Dispositif de reduction du bruit de jet d'une turbomachine
FR2868131B1 (fr) 2004-03-25 2006-06-09 Airbus France Sas Tuyere primaire a chevrons pour turboreacteur a double flux d'aeronef et aeronef comportant une telle tuyere
US7246481B2 (en) 2004-03-26 2007-07-24 General Electric Company Methods and apparatus for operating gas turbine engines
FR2872549B1 (fr) * 2004-07-05 2006-09-22 Centre Nat Rech Scient Cnrse Reacteur d'avion equipe d'un dispositif de reduction de bruit des jets propulsifs
US7246451B2 (en) * 2004-09-30 2007-07-24 Technophar Equipment & Service Limited Tumbler-dryer for capsules
GB0505246D0 (en) 2005-03-15 2005-04-20 Rolls Royce Plc Engine noise
US7559538B2 (en) * 2006-01-27 2009-07-14 Dbs Manufacturing, Inc. Wastewater treatment system and method of using same
US7721551B2 (en) * 2006-06-29 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle
US8157207B2 (en) 2006-08-09 2012-04-17 The Boeing Company Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods
US7966824B2 (en) * 2006-08-09 2011-06-28 The Boeing Company Jet engine nozzle exit configurations and associated systems and methods
US7520124B2 (en) 2006-09-12 2009-04-21 United Technologies Corporation Asymmetric serrated nozzle for exhaust noise reduction
US8015819B2 (en) 2006-09-29 2011-09-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Wet active chevron nozzle for controllable jet noise reduction
US7870722B2 (en) * 2006-12-06 2011-01-18 The Boeing Company Systems and methods for passively directing aircraft engine nozzle flows

Also Published As

Publication number Publication date
EP1936172B1 (en) 2012-07-11
CN101200220B (zh) 2013-08-14
US8166768B2 (en) 2012-05-01
JP2008144764A (ja) 2008-06-26
EP1936172A3 (en) 2010-04-21
US20080134665A1 (en) 2008-06-12
EP1936172A2 (en) 2008-06-25
JP5241215B2 (ja) 2013-07-17
CN101200220A (zh) 2008-06-18
US7870722B2 (en) 2011-01-18
US20110072781A1 (en) 2011-03-31

Similar Documents

Publication Publication Date Title
ES2391115T3 (es) Sistemas y métodos para dirigir de forma pasiva los flujos de tobera de motor de un avión
JP5220400B2 (ja) ダクト燃焼式混成流ターボファン
US9004399B2 (en) Nacelle flow assembly
CN115723945B (zh) 具有后发动机的飞行器和用于该飞行器的空气注入组件
CN107848629B (zh) 在机身后部上包括具有风扇的推进组件的飞机
BR102016021634B1 (pt) Motor traseiro e aeronave
BRPI0407675B1 (pt) Bocal de escapamento convergente
US10443398B2 (en) Turbine blade
JP2009215895A (ja) 高バイパス比ターボファンジェットエンジン
US20110155859A1 (en) Aircraft vertical lift device
BR102016021636B1 (pt) Aeronave e motor
CN103608260A (zh) 叶片,特别是变螺距叶片,包括这种叶片的螺旋桨和相应的涡轮机
BR102016027313A2 (pt) Gas turbine engine with high deviation rate, caring and core coupling assembly
US11208901B2 (en) Trailing edge cooling for a turbine blade
JP2017082774A (ja) タービンブレード
CN109477394A (zh) 动叶平台的冲击冷却
US7032387B2 (en) Axisymmetric flap on gas turbine exhaust centerbody
EP3483395A2 (en) Inter-turbine ducts with flow control mechanisms
EP3306067A1 (en) System and method for reduction of turbine exhaust gas impingement on adjacent aircraft structure
CN109083688B (zh) 具有偏转器的涡轮发动机部件
BR112012028535B1 (pt) Bocal de exaustão de gás e turbojato multifluxo
RU2731780C2 (ru) Устройство с решетками для выталкивания микроструй для уменьшения шума реактивной струи газотурбинного двигателя
US10974813B2 (en) Engine nacelle for an aircraft
US11920539B1 (en) Gas turbine exhaust nozzle noise abatement
US20230041941A1 (en) Methods and systems of mitigating high-speed jet noise