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NL6413740A - - Google Patents

Info

Publication number
NL6413740A
NL6413740A NL6413740A NL6413740A NL6413740A NL 6413740 A NL6413740 A NL 6413740A NL 6413740 A NL6413740 A NL 6413740A NL 6413740 A NL6413740 A NL 6413740A NL 6413740 A NL6413740 A NL 6413740A
Authority
NL
Netherlands
Application number
NL6413740A
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 filed Critical
Publication of NL6413740A publication Critical patent/NL6413740A/xx

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/40Varying angle of sweep

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
NL6413740A 1963-12-27 1964-11-26 NL6413740A (xx)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR958702A FR1388089A (fr) 1963-12-27 1963-12-27 Avion à configuration variable

Publications (1)

Publication Number Publication Date
NL6413740A true NL6413740A (xx) 1965-06-28

Family

ID=8819847

Family Applications (1)

Application Number Title Priority Date Filing Date
NL6413740A NL6413740A (xx) 1963-12-27 1964-11-26

Country Status (5)

Country Link
US (1) US3292881A (xx)
DE (4) DE1781045C3 (xx)
FR (1) FR1388089A (xx)
GB (1) GB1083309A (xx)
NL (1) NL6413740A (xx)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR94080E (fr) * 1963-12-27 1969-06-27 Breguet Aviat Avion a configuration variable.
GB1135946A (en) * 1965-04-01 1968-12-11 British Aircraft Corp Ltd Improvements in aircraft
DE1481572A1 (de) * 1966-02-10 1969-03-20 Hamburger Flugzeugbau Gmbh Flugzeug,insbesondere UEberschallflugzeug,mit Ausgleich der Neutralpunktwanderung
FR1515159A (fr) * 1967-01-17 1968-03-01 Dassault Avions Dispositif d'obturateur mobile entre voilure et structure fixe pour avions ou aérodynes à géométrie variable
GB1191311A (en) * 1967-02-06 1970-05-13 British Aircraft Corp Ltd Form Improvements relating to Variable-Geometry Aircraft
FR1520645A (fr) * 1967-02-28 1968-04-12 Dassault Avions Dispositif de commande de la position de la voilure sur avions et aérodynes à géométrie variable
FR1531596A (fr) * 1967-05-23 1968-07-05 Dassault Avions Dispositif de liaison entre le fuselage et les ailes mobiles d'un avion à géométrie variable
US3447761A (en) * 1967-06-12 1969-06-03 Boeing Co Supersonic airplane variable-sweep integrated airfoil system
FR1569233A (xx) * 1967-07-05 1969-05-30
US3534924A (en) * 1967-09-07 1970-10-20 Nasa Variable geometry manned orbital vehicle
US3666210A (en) * 1969-12-18 1972-05-30 Hitco Gardena Variable aerodynamic structure
US3680816A (en) * 1969-12-29 1972-08-01 Mc Donnell Douglas Corp Aircraft having auxiliary airfoils
US5961068A (en) * 1997-10-23 1999-10-05 Northrop Grumman Corporation Aerodynamic control effector
US20050178884A1 (en) * 2001-11-06 2005-08-18 Konrad Schafroth Flight device with a lift-generating fuselage
WO2004098992A1 (de) * 2003-05-05 2004-11-18 Team Smartfish Gmbh Fluggerät mit auftrieb erzeugendem rumpf
JP4171913B2 (ja) * 2004-04-13 2008-10-29 独立行政法人 宇宙航空研究開発機構 低ブーム特性と低抵抗特性を両立する可変前進翼超音速航空機
DE102010048139A1 (de) * 2010-10-11 2012-04-12 Eads Deutschland Gmbh Fluggerät mit variabler Geometrie
US8708286B2 (en) * 2012-06-21 2014-04-29 The Boeing Company Swing tip assembly rotation joint
US9296471B2 (en) * 2013-10-06 2016-03-29 The Boeing Company Swing wing tip system, assembly and method with dual load path structure
CN109436290B (zh) * 2018-12-20 2023-08-22 中国航空工业集团公司沈阳空气动力研究所 一种飞行器翼面折叠机构
CN113899517B (zh) * 2021-12-06 2022-02-18 中国空气动力研究与发展中心超高速空气动力研究所 一种高超声速风洞模型弹翼变形试验方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB651436A (en) * 1948-06-04 1951-04-04 Blackburn & Gen Aircraft Ltd Improvements in aircraft
US2794608A (en) * 1949-04-19 1957-06-04 Lockheed Aircraft Corp Airplane with variable swept wings
GB695025A (en) * 1950-06-23 1953-08-05 Blackburn & Gen Aircraft Ltd Improvements in or relating to high speed aircraft
US2924400A (en) * 1953-05-22 1960-02-09 Nord Aviation Apparatus for enabling the manoeuvrability and the stability of a supersonic aircraft to be controlled
US2822995A (en) * 1954-01-27 1958-02-11 Bowen Max Adjustable wing aircraft
US2836381A (en) * 1955-08-16 1958-05-27 Jess Rink P Airplane with variable sweepback airfoils
DE1093214B (de) * 1958-09-29 1960-11-17 Vickers Armstrongs Aircraft Flugzeug mit schwenkbaren Tragflaechen
US3064928A (en) * 1960-08-23 1962-11-20 Thomas A Toll Variable sweep wing aircraft
US3104082A (en) * 1961-11-16 1963-09-17 Edward C Polhamus Variable sweep aircraft wing
GB972268A (en) * 1962-10-16 1964-10-14 Hunting Aircraft Ltd Improvements in aeroplanes having wings capable of adjustment in sweep

Also Published As

Publication number Publication date
DE1291635B (de) 1969-03-27
DE1781045B2 (de) 1975-05-07
GB1083309A (en) 1967-09-13
US3292881A (en) 1966-12-20
FR1388089A (fr) 1965-02-05
DE1781044A1 (de) 1970-09-10
DE1781045C3 (de) 1975-12-18
DE1781046A1 (de) 1970-09-10
DE1781045A1 (de) 1970-10-22

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