ATE279355T1 - Flugzeugseitenflosse und ruder - Google Patents

Flugzeugseitenflosse und ruder

Info

Publication number
ATE279355T1
ATE279355T1 AT99936881T AT99936881T ATE279355T1 AT E279355 T1 ATE279355 T1 AT E279355T1 AT 99936881 T AT99936881 T AT 99936881T AT 99936881 T AT99936881 T AT 99936881T AT E279355 T1 ATE279355 T1 AT E279355T1
Authority
AT
Austria
Prior art keywords
rudder
side fin
aircraft side
end plate
fin
Prior art date
Application number
AT99936881T
Other languages
English (en)
Inventor
Leslie Leigh Hyde
Original Assignee
Airbus Uk Ltd
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 Uk Ltd filed Critical Airbus Uk Ltd
Application granted granted Critical
Publication of ATE279355T1 publication Critical patent/ATE279355T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/06—Fins

Landscapes

  • Aviation & Aerospace Engineering (AREA)
  • Engineering & Computer Science (AREA)
  • Sealing Devices (AREA)
  • Toys (AREA)
  • Lining And Supports For Tunnels (AREA)
  • Traffic Control Systems (AREA)
  • Moulding By Coating Moulds (AREA)
  • Earth Drilling (AREA)
  • Details Of Aerials (AREA)
  • Current-Collector Devices For Electrically Propelled Vehicles (AREA)
  • Buildings Adapted To Withstand Abnormal External Influences (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)
AT99936881T 1998-08-05 1999-08-03 Flugzeugseitenflosse und ruder ATE279355T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9816938.6A GB9816938D0 (en) 1998-08-05 1998-08-05 An aircraft fin and rudder
PCT/GB1999/002568 WO2000007875A1 (en) 1998-08-05 1999-08-03 An aircraft fin and rudder

Publications (1)

Publication Number Publication Date
ATE279355T1 true ATE279355T1 (de) 2004-10-15

Family

ID=10836673

Family Applications (1)

Application Number Title Priority Date Filing Date
AT99936881T ATE279355T1 (de) 1998-08-05 1999-08-03 Flugzeugseitenflosse und ruder

Country Status (12)

Country Link
US (1) US6202959B1 (de)
EP (1) EP1100718B1 (de)
JP (1) JP3364720B2 (de)
AT (1) ATE279355T1 (de)
AU (1) AU5185199A (de)
BR (1) BR9912754A (de)
CA (1) CA2339208C (de)
DE (1) DE69921144T2 (de)
ES (1) ES2228077T3 (de)
GB (1) GB9816938D0 (de)
TW (1) TW424063B (de)
WO (1) WO2000007875A1 (de)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2832668B1 (fr) * 2001-11-26 2004-02-13 Airbus France Procede de fabrication d'un ensemble en materiau composite et voilure et element stabilisateur d'aeronef obtenus par ce procede
US6715717B2 (en) 2002-09-06 2004-04-06 Charles J. Dixon Method and apparatus for inducing controlled vortices to reduce afterbody drag
FR2945790B1 (fr) * 2009-05-20 2011-07-22 Airbus France Procede pour l'amelioration de l'efficacite aerodynamique de l'empennage vertical d'un aeronef.
USD764384S1 (en) * 2014-07-15 2016-08-23 Icon Aircraft, Inc. Aircraft delta fin
FR3052742B1 (fr) 2016-06-16 2021-10-29 Airbus Operations Sas Aeronef presentant des gouvernes de profondeur independantes
FR3105967B1 (fr) * 2020-01-02 2022-08-26 Safran Nacelles Empennage d’aéronef comprenant une gouverne et des ailettes de pressurisation de cette gouverne
CN115123515A (zh) * 2022-06-30 2022-09-30 中国电子科技集团公司第三十八研究所 一种开合式翼梢的尾翼单元和飞艇

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1724110A (en) * 1927-02-24 1929-08-13 Elliott G Reid Aircraft
FR824296A (fr) * 1937-07-13 1938-02-04 Perfectionnements aux gouvernails et aux hélices des navires et bateaux de toutes sortes, ainsi que des aéroplanes et d'autres aéronefs
US3067971A (en) 1959-10-01 1962-12-11 North American Aviation Inc Super drag flap
FR1570966A (de) * 1968-06-20 1969-06-13
GB8310224D0 (en) * 1983-04-15 1983-05-18 British Aerospace Wing tip arrangement
US4718620A (en) 1984-10-15 1988-01-12 Braden John A Terraced channels for reducing afterbody drag
US4736913A (en) 1986-09-19 1988-04-12 Lockheed Corporation Fluid flow control device
US4790494A (en) 1986-10-14 1988-12-13 Grumman Aerospace Corporation Aircraft empennage with fixed trailing edge horizontal stabilizer
JPH0478793A (ja) * 1990-07-19 1992-03-12 Mitsubishi Heavy Ind Ltd 航空機
GB2264679A (en) 1992-03-03 1993-09-08 Secr Defence Vtol aircraft.
US5518210A (en) * 1994-04-11 1996-05-21 Mcdonnell Douglas Corporation Seal plate for aircraft movable flight control surfaces

Also Published As

Publication number Publication date
EP1100718A1 (de) 2001-05-23
CA2339208C (en) 2007-11-13
WO2000007875A1 (en) 2000-02-17
JP3364720B2 (ja) 2003-01-08
EP1100718B1 (de) 2004-10-13
DE69921144D1 (de) 2004-11-18
JP2001501894A (ja) 2001-02-13
AU5185199A (en) 2000-02-28
TW424063B (en) 2001-03-01
ES2228077T3 (es) 2005-04-01
US6202959B1 (en) 2001-03-20
BR9912754A (pt) 2001-05-15
CA2339208A1 (en) 2000-02-17
GB9816938D0 (en) 1998-09-30
DE69921144T2 (de) 2005-02-17

Similar Documents

Publication Publication Date Title
MY119073A (en) Adjustable double deck elevator
TR199801422T2 (xx) Kablo ek ba�lant�s�.
IT7883451A0 (it) Fune d' acciaio-alluminio particolarmente idonea per la conduzione di elettricita' eprocedimento per la produzione ditale fune.
BR8804874A (pt) Conjunto valvula-regulador para tornar uma fonte de gas de alta pressao compativel com um ponto de aplicacao de pressao mais baixa
ITTO930221A0 (it) Trasduttore misuratore di corrente funzionante sul principio di com- pensazione.
FR2718706B1 (fr) Structure anti-étincelage, notamment pour aéronef.
EP1108646A3 (de) Strukturbauteil
ATE279355T1 (de) Flugzeugseitenflosse und ruder
KR900700040A (ko) 칫 솔
BRPI0416865A (pt) módulo de peneiramento para um conjunto de peneiramento, e, conjunto de peneiramento
BR0107627A (pt) Dispositivo para a conservação do frescor
DE59909972D1 (de) Abformmaterial
PT1075199E (pt) Caixa de distribuicao de alimentos
BR0015893A (pt) Montagem de laminado que retem imagem, e, métodos de formar um laminado e um meio que retenha imagem
IT8119148A0 (it) Cilindro principale per freni, munito di valvola centrale.
EP1553319A4 (de) Bremsmechanismus für hebezeug
BR0106499A (pt) Prensa com tucho
TW311571U (en) Improved point rail for switching gear
DE69915055D1 (de) Antitumorale 1,5-diazaanthraquinone
IT1267370B1 (it) Perfezionamenti al procedimento di scavo ad elica continua e relativa attrezzatura.
GB9825876D0 (en) New wing design
IT1304846B1 (it) Composizione ecologica autoestinguente per la realizzazione di formeplastiche, stucchi, pannelli e simili.
ES1029667Y (es) Catamaran impulsado por el viento.
IT8921076A0 (it) Apparecchiatura di stampa con mezzi di regolazione dei cilindri di stampa, particolarmente per tessuti e simili.
IT8621826A0 (it) Procedimento per guidare pezzi su assottigliatrici, e dispositivo diguida per attuare il procedimento.

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties