ATE316491T1 - Flugzeuganordnung mit verbesserter aerodynamik - Google Patents

Flugzeuganordnung mit verbesserter aerodynamik

Info

Publication number
ATE316491T1
ATE316491T1 AT02735215T AT02735215T ATE316491T1 AT E316491 T1 ATE316491 T1 AT E316491T1 AT 02735215 T AT02735215 T AT 02735215T AT 02735215 T AT02735215 T AT 02735215T AT E316491 T1 ATE316491 T1 AT E316491T1
Authority
AT
Austria
Prior art keywords
aircraft
optimised
attack
configuration
aerodynamic performance
Prior art date
Application number
AT02735215T
Other languages
English (en)
Inventor
Massimo Lucchesini
Pierclaudio Iaia
Original Assignee
Aermacchi S P A
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 Aermacchi S P A filed Critical Aermacchi S P A
Application granted granted Critical
Publication of ATE316491T1 publication Critical patent/ATE316491T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/0009—Aerodynamic aspects
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0045—Fuselages characterised by special shapes
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Tires In General (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Details Of Aerials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Retarders (AREA)
  • Radio Relay Systems (AREA)
  • Traffic Control Systems (AREA)
  • Feedback Control In General (AREA)
  • Laminated Bodies (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
AT02735215T 2001-10-18 2002-03-27 Flugzeuganordnung mit verbesserter aerodynamik ATE316491T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT2001MI002170A ITMI20012170A1 (it) 2001-10-18 2001-10-18 Configurazione velivolo a prestazioni aerodinamiche migliorate

Publications (1)

Publication Number Publication Date
ATE316491T1 true ATE316491T1 (de) 2006-02-15

Family

ID=11448524

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02735215T ATE316491T1 (de) 2001-10-18 2002-03-27 Flugzeuganordnung mit verbesserter aerodynamik

Country Status (14)

Country Link
US (1) US7520470B2 (de)
EP (1) EP1436193B1 (de)
KR (1) KR100846023B1 (de)
CN (1) CN1571745B (de)
AT (1) ATE316491T1 (de)
BR (1) BR0213312B1 (de)
DE (1) DE60208898T2 (de)
ES (1) ES2256481T3 (de)
IT (1) ITMI20012170A1 (de)
PT (1) PT1436193E (de)
RU (1) RU2302975C2 (de)
UA (1) UA77018C2 (de)
WO (1) WO2003035467A1 (de)
ZA (1) ZA200402805B (de)

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GB0707512D0 (en) 2007-04-18 2007-05-30 Go Science Ltd Annular airborne vehicle
RU2007134266A (ru) * 2007-09-14 2009-03-20 Геннадий Трофимович Крещишин (RU) Хвостовая часть самолета крещишина и способ модернизации с уменьшением полного сопротивления самолета крещишина
US8991768B1 (en) * 2007-10-16 2015-03-31 Aerion Corporation Highly efficient transonic laminar flow wing
US9233755B1 (en) * 2007-10-16 2016-01-12 Aerion Corporation Highly efficient supersonic laminar flow wing structure
FR2937617B1 (fr) * 2008-10-29 2011-05-13 Airbus France Procede pour ameliorer les performances d'un aeronef
FR2937952B1 (fr) * 2008-10-30 2010-12-17 Snecma Avion a moteurs partiellement encastres dans le fuselage
US8974177B2 (en) 2010-09-28 2015-03-10 United Technologies Corporation Nacelle with porous surfaces
ITTO20110122A1 (it) 2011-02-14 2012-08-15 Alenia Aermacchi Spa Configurazione velivolo a prestazioni aerodinamiche migliorate.
BR112015000821B1 (pt) * 2012-07-20 2022-01-25 Icon Aircraft, Inc Configuração para uma aeronave anfíbia de asa alta e sistema para configuração resistente a giro em parafuso
ITTO20120665A1 (it) 2012-07-27 2014-01-28 Alenia Aermacchi Spa Dispositivo elettronico di interfaccia tra reti di comunicazioni tra velivoli.
FR2997681B1 (fr) * 2012-11-08 2015-05-15 Snecma Avion propulse par un turboreacteur a soufflantes contrarotatives
US9153139B2 (en) * 2012-12-21 2015-10-06 Embraer S.A. Steep approach performance improvements and optimization
FR3009541A1 (fr) * 2013-08-09 2015-02-13 Joseph Pierre Ursulet Ensemble d'avions classiques personnalises et d'avions sans ailes equipes d'ailerons recuperateurs d'air et d'un bouclier de protection du fuselage
US9758253B2 (en) 2015-06-25 2017-09-12 Northrop Grumman Systems Corporation Swept gradient boundary layer diverter
CA3022403A1 (en) * 2016-04-29 2017-11-02 Schlumberger Canada Limited Driller's control station (rabbit cage)
US10592636B2 (en) * 2017-03-17 2020-03-17 General Electric Company Methods and systems for flight data based parameter tuning and deployment
CN109720535A (zh) * 2017-10-30 2019-05-07 成都飞机工业（集团）有限责任公司 一种翼身融合飞机
US20190185127A1 (en) * 2017-12-18 2019-06-20 Freedom Aircraft Ventures Llc Aircraft design and technology
US11167836B2 (en) 2018-06-21 2021-11-09 Sierra Nevada Corporation Devices and methods to attach composite core to a surrounding structure
GB2588340B (en) 2018-06-21 2023-08-09 Sierra Nevada Corp Net edge composite core splices for aircraft wing
CN110065622A (zh) * 2019-04-12 2019-07-30 西安飞机工业（集团）有限责任公司 一种飞机操纵面吻合性公差控制方法
CN110920871A (zh) * 2019-11-18 2020-03-27 北京航空航天大学 一种通过机身涡流发生器抑制飞机摇滚运动的方法
FR3111618B1 (fr) 2020-06-17 2022-08-12 Muadiamvita David Alain Kabeya Avion pour la formation au pilotage
GB2599686A (en) 2020-10-09 2022-04-13 Rolls Royce Plc An improved turbofan gas turbine engine
CN112572788A (zh) * 2020-12-04 2021-03-30 中国航空工业集团公司成都飞机设计研究所 一种兼顾跨、超声速气动性能的飞机
CN115238378B (zh) * 2022-07-12 2023-07-07 中国航空工业集团公司沈阳飞机设计研究所 一种大迎角气动力设计方法
CN116767496A (zh) * 2023-06-15 2023-09-19 中国空气动力研究与发展中心空天技术研究所 一种宽速域高隐身背负式超声速进气道

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Publication number Priority date Publication date Assignee Title
US3285542A (en) * 1965-01-15 1966-11-15 Boeing Co Pitch-stabilized, varying-sweep wing
US3478989A (en) * 1966-11-14 1969-11-18 Hamburger Flugzeugbau Gmbh Supersonic aircraft
SE318194B (de) * 1968-06-24 1969-12-01 Saab Ab
DE1926553B2 (de) * 1969-05-23 1973-03-29 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verschliessbarer, an der rumpfaussenseite angeordneter lufteinlaufkanal fuer ein strahltriebwerk
USD256791S (en) * 1978-11-09 1980-09-09 Fairchild Industries, Inc. Aircraft
US4739957A (en) 1986-05-08 1988-04-26 Advanced Aerodynamic Concepts, Inc. Strake fence flap
US5901925A (en) * 1996-08-28 1999-05-11 Administrator, National Aeronautics And Space Administration Serrated-planform lifting-surfaces
DE19719922C1 (de) * 1997-05-13 1998-11-12 Daimler Benz Aerospace Airbus Einrichtung zur Beeinflussung einer Wurzelströmung
RU2144885C1 (ru) * 1999-07-20 2000-01-27 Дондуков Александр Николаевич Маневренный учебно-тренировочный и многоцелевой самолет "як-130"

Also Published As

Publication number Publication date
BR0213312A (pt) 2004-10-13
ES2256481T3 (es) 2006-07-16
KR20040045867A (ko) 2004-06-02
DE60208898D1 (de) 2006-04-13
HK1070627A1 (en) 2005-06-24
CN1571745A (zh) 2005-01-26
RU2004111600A (ru) 2005-04-27
US20050029402A1 (en) 2005-02-10
DE60208898T2 (de) 2006-09-14
WO2003035467A1 (en) 2003-05-01
ITMI20012170A1 (it) 2003-04-18
BR0213312B1 (pt) 2011-02-22
PT1436193E (pt) 2006-06-30
RU2302975C2 (ru) 2007-07-20
EP1436193A1 (de) 2004-07-14
US7520470B2 (en) 2009-04-21
CN1571745B (zh) 2010-09-08
EP1436193B1 (de) 2006-01-25
UA77018C2 (en) 2006-10-16
KR100846023B1 (ko) 2008-07-11
ZA200402805B (en) 2005-06-29

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