DE602006007226D1 - Lärmarmes flugzeug, beispielsweise beim start und bei der landung - Google Patents

Lärmarmes flugzeug, beispielsweise beim start und bei der landung

Info

Publication number
DE602006007226D1
DE602006007226D1 DE602006007226T DE602006007226T DE602006007226D1 DE 602006007226 D1 DE602006007226 D1 DE 602006007226D1 DE 602006007226 T DE602006007226 T DE 602006007226T DE 602006007226 T DE602006007226 T DE 602006007226T DE 602006007226 D1 DE602006007226 D1 DE 602006007226D1
Authority
DE
Germany
Prior art keywords
engine
noise
wings
channel
disposed
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
DE602006007226T
Other languages
English (en)
Inventor
Christophe Cros
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE602006007226D1 publication Critical patent/DE602006007226D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Toys (AREA)
  • Sorption Type Refrigeration Machines (AREA)
  • Filters That Use Time-Delay Elements (AREA)
  • Road Paving Structures (AREA)
  • Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
DE602006007226T 2005-04-28 2006-04-11 Lärmarmes flugzeug, beispielsweise beim start und bei der landung Active DE602006007226D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0504281A FR2885114B1 (fr) 2005-04-28 2005-04-28 Aeronef a faible bruit, notamment lors des decollages et des atterrissages
PCT/FR2006/000795 WO2006114493A2 (fr) 2005-04-28 2006-04-11 Aeronef a faible bruit, notamment lors des decollages et des atterrissages

Publications (1)

Publication Number Publication Date
DE602006007226D1 true DE602006007226D1 (de) 2009-07-23

Family

ID=35429329

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006007226T Active DE602006007226D1 (de) 2005-04-28 2006-04-11 Lärmarmes flugzeug, beispielsweise beim start und bei der landung

Country Status (11)

Country Link
US (1) US20080179465A1 (de)
EP (1) EP1874623B1 (de)
JP (1) JP2008539118A (de)
CN (1) CN101166664B (de)
AT (1) ATE433412T1 (de)
BR (1) BRPI0613207A2 (de)
CA (1) CA2603824C (de)
DE (1) DE602006007226D1 (de)
FR (1) FR2885114B1 (de)
RU (1) RU2388651C2 (de)
WO (1) WO2006114493A2 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2905356B1 (fr) * 2006-09-05 2008-11-07 Airbus France Sas Procede pour la realisation d'un aeronef a impact environnemental reduit et aeronef obtenu
US8382436B2 (en) 2009-01-06 2013-02-26 General Electric Company Non-integral turbine blade platforms and systems
US8262345B2 (en) 2009-02-06 2012-09-11 General Electric Company Ceramic matrix composite turbine engine
FR3001257B1 (fr) * 2013-01-18 2018-05-11 Safran Aircraft Engines Manche d'entree d'air acoustiquement optimisee

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2628043A (en) * 1951-02-13 1953-02-10 Lloyd Avon Ltd Tailless airplane
US2968452A (en) * 1957-08-28 1961-01-17 Cook Alexander Wellington Jet-stream aviating system for aircraft
GB1480340A (en) * 1973-07-30 1977-07-20 Hawker Siddeley Aviation Ltd Aircraft
US4240597A (en) * 1978-08-28 1980-12-23 Gates Learjet Corporation Wing with improved leading edge for aircraft
US5322242A (en) * 1991-07-08 1994-06-21 Tracy Richard R High efficiency, supersonic aircraft
JPH05286498A (ja) * 1992-04-08 1993-11-02 Honda Motor Co Ltd 航空機
JPH06255587A (ja) * 1993-03-09 1994-09-13 Honda Motor Co Ltd 航空機
DE69430198T2 (de) * 1994-12-16 2003-07-10 Aldo Frediani Grossraumflugzeug
US6116539A (en) * 1999-03-19 2000-09-12 Williams International Co. L.L.C. Aeroelastically stable forward swept wing
USD530658S1 (en) * 2003-04-25 2006-10-24 Airbus S.A.S. Airplanes
USD500981S1 (en) * 2004-02-25 2005-01-18 Adam Aircraft Industries Aircraft
USD592582S1 (en) * 2006-10-11 2009-05-19 Mte Meerestechnik Engineering Gmbh Flying boat

Also Published As

Publication number Publication date
CN101166664A (zh) 2008-04-23
FR2885114B1 (fr) 2007-06-08
FR2885114A1 (fr) 2006-11-03
RU2388651C2 (ru) 2010-05-10
RU2007144088A (ru) 2009-06-10
US20080179465A1 (en) 2008-07-31
WO2006114493A2 (fr) 2006-11-02
CA2603824A1 (fr) 2006-11-02
WO2006114493A3 (fr) 2006-12-14
ATE433412T1 (de) 2009-06-15
CA2603824C (fr) 2013-01-15
JP2008539118A (ja) 2008-11-13
CN101166664B (zh) 2012-03-21
BRPI0613207A2 (pt) 2010-12-28
EP1874623A2 (de) 2008-01-09
EP1874623B1 (de) 2009-06-10

Similar Documents

Publication Publication Date Title
US7600384B2 (en) Gas exhaust nozzle for a bypass turbomachine having an exhaust or throat section that can be varied by moving the secondary cowl
US9260974B2 (en) System and method for active clearance control
RU2007141933A (ru) Воздушное судно с низким уровнем шума, в частности-при взлете и посадке
EP2784267A3 (de) Gasturbinenmotor- Kühlungsanordnung
US10352274B2 (en) Direct drive aft fan engine
DE602007003981D1 (de) Strukturgondel
WO2008043903A3 (fr) Nacelle pour turboréacteur double flux
DE602006004477D1 (de) Turbojet für flugzeug, mit solch einem turbojet ausgestattetes flugzeug und verfahren zur befestigung solch eines turbojets an einem flugzeug
FR2892999B1 (fr) Aeronef comportant un carenage central ajusteur de pression voilure par deformations geometriques locales
JP2008121676A (ja) ターボファンエンジンノズル組立体及びターボファンエンジン組立体
FR2890696B1 (fr) Turbomoteur a bruit de jet attenue
US20120192543A1 (en) Exhaust nozzle for a bypass airplane turbojet having a deployable secondary cover and a retractable central body
WO2009024662A3 (fr) Systeme de liaison entre une structure interne et une structure externe d'une nacelle de turboreacteur
GB2549439A (en) Aircraft propulsion unit comprising an unducted-fan turbine engine and an attachment pylon
WO2015012920A3 (en) Secondary nozzle for jet engine
US10308368B2 (en) Turbofan engine and method of reducing air flow separation therein
BRPI0814918A2 (pt) "nacela para um motor a jato e aeronave"
DE602006007226D1 (de) Lärmarmes flugzeug, beispielsweise beim start und bei der landung
US7845156B2 (en) Turbofan exhaust system
ATE502194T1 (de) Integrierte motorabgassysteme und verfahren zur reduzierung von widerstand und wärmebelastung
US10704415B2 (en) Gas turbine engine with low fan noise
WO2010061071A3 (fr) Nacelle integree sur aile volante
EP2527744A3 (de) System und Verfahren für eine Turbinenbrennkammermontageanordnung
Van Zante et al. Environmentally responsible aviation: propulsion research to enable fuel burn, noise and emissions reduction
US10677091B2 (en) Airfoil with sealed baffle

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
R082 Change of representative

Ref document number: 1874623

Country of ref document: EP

Representative=s name: MEISSNER & MEISSNER, 14199 BERLIN, DE