IT7830825A0 - Impennaggio direzionale di alta efficienza, con geometria alare variabile. - Google Patents

Impennaggio direzionale di alta efficienza, con geometria alare variabile.

Info

Publication number
IT7830825A0
IT7830825A0 IT7830825A IT3082578A IT7830825A0 IT 7830825 A0 IT7830825 A0 IT 7830825A0 IT 7830825 A IT7830825 A IT 7830825A IT 3082578 A IT3082578 A IT 3082578A IT 7830825 A0 IT7830825 A0 IT 7830825A0
Authority
IT
Italy
Prior art keywords
fleece
high efficiency
variable wing
wing geometry
efficiency directional
Prior art date
Application number
IT7830825A
Other languages
English (en)
Other versions
IT1100627B (it
Original Assignee
Messerschmitt Bolkon Blohm Gmb
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 Messerschmitt Bolkon Blohm Gmb filed Critical Messerschmitt Bolkon Blohm Gmb
Publication of IT7830825A0 publication Critical patent/IT7830825A0/it
Application granted granted Critical
Publication of IT1100627B publication Critical patent/IT1100627B/it

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/08—Stabilising surfaces mounted on, or supported by, wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Tires In General (AREA)
IT30825/78A 1977-12-16 1978-12-14 Impennaggio direzionale di alta efficienza,con geometria alare variabile IT1100627B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2756107A DE2756107C2 (de) 1977-12-16 1977-12-16 Hochwirksames Seitenleitwerk mit variabler Flügelgeometrie

Publications (2)

Publication Number Publication Date
IT7830825A0 true IT7830825A0 (it) 1978-12-14
IT1100627B IT1100627B (it) 1985-09-28

Family

ID=6026294

Family Applications (1)

Application Number Title Priority Date Filing Date
IT30825/78A IT1100627B (it) 1977-12-16 1978-12-14 Impennaggio direzionale di alta efficienza,con geometria alare variabile

Country Status (6)

Country Link
US (1) US4247062A (it)
JP (1) JPS54113196A (it)
DE (1) DE2756107C2 (it)
FR (1) FR2411758A1 (it)
GB (1) GB2010195B (it)
IT (1) IT1100627B (it)

Families Citing this family (53)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3103095C2 (de) * 1981-01-30 1985-05-09 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flugzeug mit Tragflächen negativer Pfeilung und einem Heckleitwerk
US4538779A (en) * 1982-09-30 1985-09-03 The Boeing Company Caster type empennage assembly for aircraft
DE3242584A1 (de) * 1982-11-18 1984-05-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Anordnung von zusatzflaechen an den spitzen eines tragfluegels
US4545552A (en) * 1983-06-20 1985-10-08 Welles Stanley W Airframe design
US4542866A (en) * 1983-09-30 1985-09-24 The Boeing Company Aircraft with directional controlling canards
US4682746A (en) * 1984-12-05 1987-07-28 Lockheed Corporation Control force generator
EP0188998A1 (de) * 1985-01-23 1986-07-30 FIDES TREUHAND GmbH Supermanövrierbares Flugzeug
JPH0412842Y2 (it) * 1986-07-14 1992-03-26
DE3638347A1 (de) * 1986-11-10 1988-05-19 Andreas Heinrich Rudersystem zur steuerung von flugzeugen
EP0416268A3 (en) * 1989-09-04 1991-04-03 British Aerospace Public Limited Company Tail unit
US5072894A (en) * 1989-10-02 1991-12-17 Rockwell International Corporation Apparatus and method for increasing the angle of attack operating range of an aircraft
US5078338A (en) * 1990-01-19 1992-01-07 Neill Terrence O Means for maintaining a desired relationship between roll and yaw stability in a swept-wing aircraft by varying dihedral as a function of lift coefficient
US5156358A (en) * 1991-04-11 1992-10-20 Northrop Corporation Aircraft outboard control
US5398888A (en) * 1993-05-12 1995-03-21 Northrop Grumman Corporation Skewed hinge control surface
GB9321510D0 (en) * 1993-10-19 1993-12-22 Short Brothers Plc Aircraft flight control system
USD378955S (en) 1995-05-04 1997-04-29 Colgate-Palmolive Co. Toothbrush handle
FR2841532B1 (fr) * 2002-06-27 2004-12-17 Airbus France Avion a controle actif du vrillage de ses ailes
GB0326228D0 (en) * 2003-11-10 2003-12-17 Airbus Uk Ltd Wing tip device
US7475848B2 (en) * 2003-11-11 2009-01-13 Morgenstern John M Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
GB0518755D0 (en) 2005-09-14 2005-10-19 Airbus Uk Ltd Wing tip device
CN102149599B (zh) 2008-06-20 2014-11-19 航空伙伴股份有限公司 弯曲的机翼末梢
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
US20110127383A1 (en) * 2009-12-01 2011-06-02 Guida Associates Consulting, Inc. Active winglet
US9162755B2 (en) 2009-12-01 2015-10-20 Tamarack Aerospace Group, Inc. Multiple controllable airflow modification devices
FR2954275B1 (fr) * 2009-12-22 2012-01-13 Astrium Sas Vehicule aerien ultra-rapide et procede de locomotion aerienne associe
GB201011843D0 (en) 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
DE102010048139A1 (de) * 2010-10-11 2012-04-12 Eads Deutschland Gmbh Fluggerät mit variabler Geometrie
GB201018185D0 (en) * 2010-10-28 2010-12-08 Airbus Operations Ltd Wing tip device attachment apparatus and method
DK3372493T3 (da) * 2011-06-09 2019-12-09 Aviation Partners Inc Den delt-formet blandede winglet
US10538307B2 (en) * 2011-10-01 2020-01-21 The Boeing Company Hinged raked wing tip
US9481446B2 (en) 2012-10-30 2016-11-01 The Boeing Company System for latching and locking a foldable airfoil
GB201301680D0 (en) * 2013-01-31 2013-03-13 Airbus Uk Ltd Downwardly extending wing tip device
US9567066B2 (en) * 2013-02-05 2017-02-14 Tamarack Aerospace Group, Inc. Controllable airflow modification device periodic load control
US10562613B2 (en) * 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
CN105015795A (zh) * 2014-04-28 2015-11-04 张焰 飞机设计方法与方案
US10011350B2 (en) * 2014-05-20 2018-07-03 Sikorsky Aircraft Corporation Vertical take-off and landing drag rudder
FR3037560B1 (fr) * 2015-06-16 2018-06-01 Airbus Operations Aile d'aeronef comprenant un embout d'aile pilotable en incidence
CN105035304A (zh) * 2015-08-13 2015-11-11 中国航空工业集团公司西安飞机设计研究所 一种带分裂式翼尖的无尾飞翼布局飞机
RU2616458C1 (ru) * 2016-04-01 2017-04-17 Борис Владимирович Мищенко Сверхзвуковой летательный аппарат
EP3269635A1 (en) * 2016-07-12 2018-01-17 The Aircraft Performance Company UG Airplane wing
GB2565768B (en) * 2017-08-15 2022-05-18 Bae Systems Plc A vehicle
EP3668787B1 (en) 2017-08-15 2023-06-07 BAE Systems PLC A vehicle
EP3486162B1 (en) * 2017-11-17 2020-07-01 Airbus Operations GmbH Method for operating a wing for an aircraft including a foldable wing tip portion
EP3511243B1 (en) * 2018-01-15 2021-12-29 The Aircraft Performance Company GmbH Airplane wing
US11440638B2 (en) * 2018-05-03 2022-09-13 Airbus Operations Gmbh Wing for an aircraft
US20190351994A1 (en) * 2018-05-16 2019-11-21 Richard Michael Truhill Retractable aircraft control surface
US11370526B2 (en) * 2018-05-31 2022-06-28 Airbus Operations Gmbh Latching device for a wing arrangement for an aircraft
US11319054B2 (en) * 2018-05-31 2022-05-03 Airbus Operations Gmbh Wing arrangement for an aircraft
US11214353B2 (en) * 2018-06-01 2022-01-04 Airbus Operations Gmbh Wing arrangement for an aircraft and aircraft
EP3587252A1 (en) * 2018-06-28 2020-01-01 Airbus Operations GmbH Arresting system for arresting a first aircraft component relative to a second aircraft component
US11254412B2 (en) 2019-03-29 2022-02-22 The Boeing Company Foldable raked wing tips having aerodynamic devices
GB2615311A (en) * 2022-01-31 2023-08-09 Airbus Operations Ltd Aircraft wing with movable wing tip device
GB2616252A (en) * 2022-01-31 2023-09-06 Airbus Operations Ltd Aircraft with movable wing tip device

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3104079A (en) * 1960-10-07 1963-09-17 William H Phillips Variable-geometry winged reentry vehicle
GB934286A (en) * 1961-06-16 1963-08-14 English Electric Co Ltd Improvements in and relating to wing tip folding mechanisms

Also Published As

Publication number Publication date
IT1100627B (it) 1985-09-28
JPS54113196A (en) 1979-09-04
FR2411758B3 (it) 1981-01-02
FR2411758A1 (fr) 1979-07-13
DE2756107B1 (de) 1979-06-28
DE2756107C2 (de) 1980-02-28
GB2010195A (en) 1979-06-27
GB2010195B (en) 1982-03-03
US4247062A (en) 1981-01-27

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