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IT8224675A0 - Sistema di installazione di gondola o navicella per motori di aereo. - Google Patents

Sistema di installazione di gondola o navicella per motori di aereo.

Info

Publication number
IT8224675A0
IT8224675A0 IT8224675A IT2467582A IT8224675A0 IT 8224675 A0 IT8224675 A0 IT 8224675A0 IT 8224675 A IT8224675 A IT 8224675A IT 2467582 A IT2467582 A IT 2467582A IT 8224675 A0 IT8224675 A0 IT 8224675A0
Authority
IT
Italy
Prior art keywords
nascella
gondola
installation system
aircraft engines
engines
Prior art date
Application number
IT8224675A
Other languages
English (en)
Other versions
IT1195962B (it
Inventor
Donald John Dusa
Conrad Dudley Wagenknecht
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT8224675A0 publication Critical patent/IT8224675A0/it
Application granted granted Critical
Publication of IT1195962B publication Critical patent/IT1195962B/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • 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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/02—Power-plant nacelles, fairings or cowlings associated with wings
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • F02K1/52—Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/17—Purpose of the control system to control boundary layer
    • F05D2270/173—Purpose of the control system to control boundary layer by the Coanda effect
    • 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
    • Y02T50/10—Drag reduction
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Massaging Devices (AREA)
IT24675/82A 1981-12-21 1982-12-10 Sistema di installazione di gondola o navicella per motori di aereo IT1195962B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/332,893 US4466587A (en) 1981-12-21 1981-12-21 Nacelle installation

Publications (2)

Publication Number Publication Date
IT8224675A0 true IT8224675A0 (it) 1982-12-10
IT1195962B IT1195962B (it) 1988-11-03

Family

ID=23300317

Family Applications (1)

Application Number Title Priority Date Filing Date
IT24675/82A IT1195962B (it) 1981-12-21 1982-12-10 Sistema di installazione di gondola o navicella per motori di aereo

Country Status (6)

Country Link
US (1) US4466587A (it)
JP (1) JPS58122294A (it)
DE (1) DE3246737A1 (it)
FR (1) FR2518492B1 (it)
GB (1) GB2112077B (it)
IT (1) IT1195962B (it)

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US5490644A (en) * 1993-12-20 1996-02-13 The Boeing Company Ducted boundary layer diverter
FR2740175B1 (fr) * 1995-10-18 1997-11-21 Snecma Dispositif de pylone associe au melangeur d'une tuyere d'ejection de turboreacteur a flux melangeur
JP3714722B2 (ja) * 1996-05-09 2005-11-09 本田技研工業株式会社 剥離抑制装置
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US5887822A (en) * 1997-03-28 1999-03-30 The Boeing Company Segmented engine flow control device
US5906097A (en) * 1997-03-28 1999-05-25 The Boeing Company Engine flow control device
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GB9804807D0 (en) * 1998-03-06 1998-04-29 Rolls Royce Plc A breather outlet
US7802752B2 (en) * 2002-03-20 2010-09-28 The Regents Of The University Of California Jet engine noise suppressor
DE102004034367B4 (de) 2004-07-16 2013-09-12 Airbus Operations Gmbh Betankungs-Pod eines Flugzeugs mit einer Ablenkvorrichtung
FR2901538B1 (fr) * 2006-05-23 2008-07-18 Airbus France Sas Aeronef comportant un dispositif de reduction de la trainee induite
US7721551B2 (en) * 2006-06-29 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle
US7520124B2 (en) * 2006-09-12 2009-04-21 United Technologies Corporation Asymmetric serrated nozzle for exhaust noise reduction
FR2905930B1 (fr) * 2006-09-18 2009-05-15 Airbus France Sa Generateur de tourbillon en sortie de gaz chauds
US7604201B2 (en) * 2006-11-17 2009-10-20 Pratt & Whitney Canada Corp. Nacelle drag reduction device for a turbofan gas turbine engine
FR2913665B1 (fr) * 2007-03-16 2009-06-05 Airbus France Sa Carenage aerodynamique arriere inferieur pour dispositif d'accrochage d'un moteur d'aeronef
US7966827B2 (en) * 2007-05-31 2011-06-28 United Technologies Corporation Gas turbine engine with fan variable area nozzle having a rotational valve system
EP2167380B1 (en) * 2007-06-15 2015-03-25 Airbus Operations GmbH Engine nacelle of an aircraft comprising a vortex generator arrangement
FR2920130B1 (fr) * 2007-08-24 2010-01-22 Airbus France Dispositif pour generer des perturbations aerodynamiques afin de proteger la surface exterieure d'un aeronef contre des temperatures elevees
FR2921342B1 (fr) * 2007-09-20 2010-03-12 Airbus France Carenage aerodynamique arriere inferieur pour dispositif d'accrochage d'un moteur d'aeronef
FR2928622B1 (fr) * 2008-03-14 2011-12-02 Airbus France Mat de suspension d'avion comportant au moins un element pour former des tourbillons d'air
FR2930235B1 (fr) * 2008-04-21 2011-09-30 Airbus France Mat de suspension pour turbomoteur.
US9181899B2 (en) * 2008-08-27 2015-11-10 General Electric Company Variable slope exhaust nozzle
US20100162680A1 (en) * 2008-12-31 2010-07-01 Syed Jalaluddin Khalid Gas turbine engine with ejector
US8572947B2 (en) * 2008-12-31 2013-11-05 Rolls-Royce Corporation Gas turbine engine with ejector
DE102009003084B4 (de) * 2009-05-13 2013-03-14 Airbus Operations Gmbh Verkleidung für eine Auftriebshilfe
GB0914031D0 (en) 2009-08-11 2009-09-16 Airbus Operations Gmbh Gas exhaust diverter
FR2952349B1 (fr) * 2009-11-06 2012-02-17 Airbus Operations Sas Procede de fabrication d'un mat reacteur equipe d'un generateur de tourbillons
US20110121137A1 (en) * 2009-11-24 2011-05-26 Electrofilm Manufacturing Company Llc Method and apparatus for directing waste away from aircraft
US8651426B2 (en) 2010-07-01 2014-02-18 Rolls-Royce Plc Jet engine installation
WO2012018615A1 (en) 2010-07-26 2012-02-09 Rolls-Royce Corporation Gas turbine engine with ejector
US8549834B2 (en) 2010-10-21 2013-10-08 United Technologies Corporation Gas turbine engine with variable area fan nozzle
FR2982236B1 (fr) * 2011-11-03 2014-06-27 Snecma Pylone d'accrochage pour turbomachine
EP2785590B1 (en) * 2011-11-29 2016-06-08 Short Brothers Plc System and method for cooling an aircraft wing
US9260974B2 (en) 2011-12-16 2016-02-16 General Electric Company System and method for active clearance control
US9783315B2 (en) * 2012-02-24 2017-10-10 Rohr, Inc. Nacelle with longitudinal translating cowling and rotatable sleeves
US9371138B2 (en) * 2012-06-07 2016-06-21 Rohr, Inc. Nacelle
US9630706B2 (en) 2013-02-22 2017-04-25 Rolls-Royce Corporation Positionable ejector member for ejector enhanced boundary layer alleviation
WO2014151673A1 (en) 2013-03-15 2014-09-25 United Technologies Corporation Aerodynamic track fairing for a gas turbine engine fan nacelle
EP2971727B1 (en) * 2013-03-15 2018-04-11 United Technologies Corporation Asymmetric fan nozzle in high-bpr separate-flow nacelle
US20150330254A1 (en) 2014-05-15 2015-11-19 United Technologies Corporation Compact Nacelle With Contoured Fan Nozzle
US9810178B2 (en) 2015-08-05 2017-11-07 General Electric Company Exhaust nozzle with non-coplanar and/or non-axisymmetric shape
FR3045012B1 (fr) * 2015-12-11 2017-12-08 Airbus Operations Sas Mat d'accrochage d'une turbomachine muni d'un element de protection thermique
US10961950B2 (en) * 2016-11-03 2021-03-30 The Boeing Company Fan nacelle trailing edge
GB2578447A (en) * 2018-10-26 2020-05-13 Airbus Operations Ltd Aircraft assembly with a hot-air exhaust outlet
WO2021138538A1 (en) * 2020-01-03 2021-07-08 University Of Kansas Methods and systems of mitigating high-speed jet noise
CN114715416A (zh) * 2022-03-22 2022-07-08 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种航空涡扇发动机及外涵道喷口

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Also Published As

Publication number Publication date
IT1195962B (it) 1988-11-03
FR2518492A1 (fr) 1983-06-24
FR2518492B1 (fr) 1987-08-28
GB2112077A (en) 1983-07-13
US4466587A (en) 1984-08-21
GB2112077B (en) 1985-08-07
JPS58122294A (ja) 1983-07-20
DE3246737A1 (de) 1983-06-30

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