DE1481620A1 - Steuerungssystem fuer senkrecht startende und landende Flugzeuge - Google Patents

Steuerungssystem fuer senkrecht startende und landende Flugzeuge

Info

Publication number
DE1481620A1
DE1481620A1 DE19661481620 DE1481620A DE1481620A1 DE 1481620 A1 DE1481620 A1 DE 1481620A1 DE 19661481620 DE19661481620 DE 19661481620 DE 1481620 A DE1481620 A DE 1481620A DE 1481620 A1 DE1481620 A1 DE 1481620A1
Authority
DE
Germany
Prior art keywords
commands
control
engines
thrust
control system
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
DE19661481620
Other languages
German (de)
English (en)
Other versions
DE1481620B2 (enExample
Inventor
Rene Phillippot
Lariviere Jean Soulez
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nord Aviation Societe Nationale de Constructions Aeronautiques
Original Assignee
Nord Aviation Societe Nationale de Constructions Aeronautiques
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 Nord Aviation Societe Nationale de Constructions Aeronautiques filed Critical Nord Aviation Societe Nationale de Constructions Aeronautiques
Publication of DE1481620B2 publication Critical patent/DE1481620B2/de
Publication of DE1481620A1 publication Critical patent/DE1481620A1/de
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0091—Accessories not provided for elsewhere
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Preparation Of Clay, And Manufacture Of Mixtures Containing Clay Or Cement (AREA)
  • Toys (AREA)
  • Mechanical Control Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE19661481620 1965-06-10 1966-06-10 Steuerungssystem fuer senkrecht startende und landende Flugzeuge Pending DE1481620A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR20342A FR1458961A (fr) 1965-06-10 1965-06-10 Dispositif de liaison pour machine volante à décollage et à atterrissage verticaux

Publications (2)

Publication Number Publication Date
DE1481620B2 DE1481620B2 (enExample) 1969-03-27
DE1481620A1 true DE1481620A1 (de) 1969-03-27

Family

ID=8581578

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19661481620 Pending DE1481620A1 (de) 1965-06-10 1966-06-10 Steuerungssystem fuer senkrecht startende und landende Flugzeuge

Country Status (4)

Country Link
US (1) US3393882A (enExample)
DE (1) DE1481620A1 (enExample)
FR (1) FR1458961A (enExample)
GB (1) GB1149367A (enExample)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2700734B2 (ja) * 1991-09-20 1998-01-21 川崎重工業株式会社 垂直離着陸航空機
US5765783A (en) * 1994-03-04 1998-06-16 The Boeing Company Vertically launchable and recoverable winged aircraft
US5727757A (en) * 1996-01-17 1998-03-17 Mcdonnell Douglas Helicopter Co. Slotted cam control system
US6896221B1 (en) 2003-04-16 2005-05-24 Einar Einarsson Vertical takeoff and landing aircraft
FR2864030B1 (fr) * 2003-12-23 2006-02-17 Eurocopter France Aeronef convertible pourvu de deux "tilt fan" de part et d'autre du fuselage et d'un troisieme "tilt fan" agence sur la queue de l'aeronef
CN100503366C (zh) 2004-07-29 2009-06-24 贝尔直升机泰克斯特龙公司 用于倾转旋翼飞行器飞行控制的方法和装置
GB0422095D0 (en) * 2004-10-05 2004-11-03 Hardy Alexander S Aircraft
US7658346B2 (en) * 2005-02-25 2010-02-09 Honeywell International Inc. Double ducted hovering air-vehicle
US8074940B2 (en) * 2007-08-08 2011-12-13 Moog Inc. Control stick adapted for use in a fly-by-wire flight control system, and linkage for use therein
FR2946318B1 (fr) * 2009-06-04 2012-11-16 Eurocopter France Dispositif mecanique pour combiner un premier et un deuxieme ordres de commande,et aeronef muni d'un tel dispositif.
US9004393B2 (en) 2010-10-24 2015-04-14 University Of Kansas Supersonic hovering air vehicle
FR3022217A1 (fr) * 2014-06-12 2015-12-18 Bermond Gerome Aeronef convertible a aile basculante
US10107196B2 (en) 2014-08-08 2018-10-23 Thomas International, Inc. Adjustable size inlet system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3106369A (en) * 1960-02-23 1963-10-08 Curtiss Wright Corp Aircraft and method of operating same
FR1292361A (fr) * 1961-03-23 1962-05-04 Snecma Dispositif automatique de contrôle de transition pour avions décollant et atterrissant à la verticale

Also Published As

Publication number Publication date
US3393882A (en) 1968-07-23
FR1458961A (fr) 1966-04-29
DE1481620B2 (enExample) 1969-03-27
GB1149367A (en) 1969-04-23

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