DE60039870D1 - Vorrichtung und verfahren zur aktiven kontrolle einer düsenströmung - Google Patents

Vorrichtung und verfahren zur aktiven kontrolle einer düsenströmung

Info

Publication number
DE60039870D1
DE60039870D1 DE60039870T DE60039870T DE60039870D1 DE 60039870 D1 DE60039870 D1 DE 60039870D1 DE 60039870 T DE60039870 T DE 60039870T DE 60039870 T DE60039870 T DE 60039870T DE 60039870 D1 DE60039870 D1 DE 60039870D1
Authority
DE
Germany
Prior art keywords
active control
nozzle flow
nozzle
flow
active
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.)
Expired - Lifetime
Application number
DE60039870T
Other languages
English (en)
Inventor
Valdis Kibens
John Doris Iii
David M Smith
David E Parekh
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=23297488&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE60039870(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE60039870D1 publication Critical patent/DE60039870D1/de
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
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28—Plants 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
    • F02K1/34—Plants 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

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)
DE60039870T 1999-06-11 2000-06-08 Vorrichtung und verfahren zur aktiven kontrolle einer düsenströmung Expired - Lifetime DE60039870D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/332,268 US6308898B1 (en) 1999-06-11 1999-06-11 Apparatus and methods for active flow control of a nozzle exhaust plume
PCT/US2000/015787 WO2000077380A1 (en) 1999-06-11 2000-06-08 Apparatus and methods for active flow control of a nozzle exhaust plume

Publications (1)

Publication Number Publication Date
DE60039870D1 true DE60039870D1 (de) 2008-09-25

Family

ID=23297488

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60039870T Expired - Lifetime DE60039870D1 (de) 1999-06-11 2000-06-08 Vorrichtung und verfahren zur aktiven kontrolle einer düsenströmung

Country Status (6)

Country Link
US (1) US6308898B1 (de)
EP (1) EP1185779B2 (de)
AU (1) AU5474600A (de)
DE (1) DE60039870D1 (de)
ES (1) ES2311461T5 (de)
WO (1) WO2000077380A1 (de)

Families Citing this family (38)

* Cited by examiner, † Cited by third party
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FR2829802B1 (fr) * 2001-09-19 2004-05-28 Centre Nat Rech Scient Dispositif de controle de melange de jets propulsifs pour reacteur d'avion
US6705547B2 (en) * 2002-02-01 2004-03-16 Luis Manuel Braga Da Costa Campos Active noise reducing nozzle
US6883304B2 (en) * 2002-09-16 2005-04-26 The Boeing Company Pulsejet ejector thrust augmentor
US6793174B2 (en) 2002-09-16 2004-09-21 The Boeing Company Pulsejet augmentor powered VTOL aircraft
GB0226228D0 (en) * 2002-11-09 2002-12-18 Rolls Royce Plc Suppression of part of the noise from a gas turbine engine
US20040168939A1 (en) * 2003-02-28 2004-09-02 Deshazer Angela M. Sports ball carry bag
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
US8225592B1 (en) * 2003-06-09 2012-07-24 Florida State University Research Foundation Microjet noise suppression system for jet engines
US6926235B2 (en) * 2003-06-20 2005-08-09 The Boeing Company Runway-independent omni-role modularity enhancement (ROME) vehicle
US7581692B2 (en) * 2003-06-30 2009-09-01 General Electric Company Fluidic chevrons and configurable thermal shield for jet noise reduction
US20050091963A1 (en) * 2003-10-30 2005-05-05 Gongling Li Aircraft turbine engine and an air ejection assembly for use therewith
US7096888B1 (en) 2003-11-26 2006-08-29 Honeywell International, Inc. Fluidic pulse generator system
US7308966B2 (en) * 2003-12-30 2007-12-18 General Electric Company Device for reducing jet engine exhaust noise using oscillating jets
US7412832B2 (en) * 2004-03-26 2008-08-19 General Electric Company Method and apparatus for operating gas turbine engines
US7377108B2 (en) * 2004-04-09 2008-05-27 The Boeing Company Apparatus and method for reduction jet noise from single jets
US7377109B2 (en) * 2004-04-09 2008-05-27 The Boeing Company Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flows
US7424413B2 (en) * 2005-02-21 2008-09-09 General Electric Company Method for optimizing turbine engine exhaust system
GB0504272D0 (en) * 2005-03-02 2005-04-06 Rolls Royce Plc A turbine engine and a method of operating a turbine engine
US7685806B2 (en) * 2005-12-29 2010-03-30 General Electric Company Method and apparatus for supersonic and shock noise reduction in aircraft engines using pneumatic corrugations
FR2901321B1 (fr) * 2006-05-18 2011-08-12 Aircelle Sa Procede d'homogeneisation de l'air en sortie de turboreacteur pour abaisser le bruit genere
FR2904663B1 (fr) * 2006-08-01 2012-02-03 Snecma Turbomachine a double flux a variation artificielle de sa section de col
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
US8480350B2 (en) * 2006-10-12 2013-07-09 United Technologies Corporation Turbofan engine with variable bypass nozzle exit area and method of operation
US7937945B2 (en) 2006-10-27 2011-05-10 Kinde Sr Ronald August Combining a series of more efficient engines into a unit, or modular units
GB2452459B (en) * 2007-01-17 2011-10-26 United Technologies Corp Core reflex nozzle for turbofan engine
US8127532B2 (en) 2008-11-26 2012-03-06 The Boeing Company Pivoting fan nozzle nacelle
US8959889B2 (en) 2008-11-26 2015-02-24 The Boeing Company Method of varying a fan duct nozzle throat area of a gas turbine engine
DE102009032841A1 (de) * 2009-07-13 2011-01-20 Rolls-Royce Deutschland Ltd & Co Kg Geräuschreduziertes Flugzeugtriebwerk sowie Verfahren zur Verminderung von Geräuschemissionen eines Flugzeugtriebwerks
US9551296B2 (en) * 2010-03-18 2017-01-24 The Boeing Company Method and apparatus for nozzle thrust vectoring
FR2960028B1 (fr) * 2010-05-12 2016-07-15 Snecma Dispositif pour attenuer le bruit emis par le jet d'un moteur de propulsion d'un aeronef.
US8316631B2 (en) 2010-09-30 2012-11-27 Lockheed Martin Corporation Exhaust plume heat effect reducing method and apparatus
DE102012109647B4 (de) * 2012-10-10 2015-09-03 Airbus Defence and Space GmbH Flugtriebwerk mit einer Einrichtung zum pulsierenden Ausblasen eines Gases in die Abgasdüse
DE102012220358A1 (de) 2012-11-08 2014-06-12 Rolls-Royce Deutschland Ltd & Co Kg Düse mit Leitvorrichtungen
DE102012220360A1 (de) 2012-11-08 2014-05-08 Rolls-Royce Deutschland Ltd & Co Kg Düse mit Leitvorrichtungen
US9541030B2 (en) * 2013-11-27 2017-01-10 Lockheed Martin Corporation Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices
US10787245B2 (en) 2016-06-01 2020-09-29 The Boeing Company Distributed compressor for improved integration and performance of an active fluid flow control system
CN109408923B (zh) * 2018-10-12 2023-01-20 北京环境特性研究所 羽流流动数据处理方法、装置和计算机设备
US11085398B2 (en) 2019-03-12 2021-08-10 Rohr, Inc. Core air flow to equalize temperature differential

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH323712A (fr) 1950-06-16 1957-08-15 Snecma Ajutage de décharge pourvu d'un dispositif pour produire une déviation de la veine de fluide déchargée
US2943821A (en) 1950-12-30 1960-07-05 United Aircraft Corp Directional control means for a supersonic vehicle
FR1072523A (fr) 1952-12-12 1954-09-14 Snecma Dispositif de contrôle d'un écoulement de fluide par un éeoulement auxiliaire
US2886946A (en) * 1955-04-14 1959-05-19 Canadair Ltd Thrust reversing device for turbojet engines
US3121312A (en) 1961-02-28 1964-02-18 United Aircraft Corp Unified pitch, yaw and roll shock control
US3204405A (en) * 1964-02-20 1965-09-07 Raymond W Warren Three dimensional jet vectoring system
FR1456926A (fr) 1965-09-17 1966-07-08 Bertin & Cie Perfectionnements apportés aux dispositifs de déviation de fluides et à leur application à la dilution
US3420060A (en) 1966-04-22 1969-01-07 Mc Donnell Douglas Corp Pressure induced jet vectoring augmentation apparatus
US3698642A (en) 1966-11-04 1972-10-17 Thiokol Chemical Corp Thrust vector control system
GB1134996A (en) 1967-04-21 1968-11-27 Lev Iosifovich Sorkin Jet noise suppressor in jet engine
GB8610297D0 (en) 1986-04-28 1986-10-01 Rolls Royce Turbomachinery
US5261227A (en) 1992-11-24 1993-11-16 General Electric Company Variable specific thrust turbofan engine
US5664415A (en) 1994-06-01 1997-09-09 Lockheed Fort Worth Company After-burning turbo-fan engine with a fixed geometry exhaust nozzle having a variable flow coefficient
US5833433A (en) 1997-01-07 1998-11-10 Mcdonnell Douglas Corporation Rotating machinery noise control device

Also Published As

Publication number Publication date
EP1185779B1 (de) 2008-08-13
ES2311461T3 (es) 2009-02-16
ES2311461T5 (es) 2017-04-26
US6308898B1 (en) 2001-10-30
AU5474600A (en) 2001-01-02
EP1185779A1 (de) 2002-03-13
EP1185779B2 (de) 2016-09-07
WO2000077380A1 (en) 2000-12-21

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Legal Events

Date Code Title Description
8363 Opposition against the patent