DE69824945D1 - Flugzeugsteuerungseinrichtungen mit automatischer Kompensation - Google Patents

Flugzeugsteuerungseinrichtungen mit automatischer Kompensation

Info

Publication number
DE69824945D1
DE69824945D1 DE69824945T DE69824945T DE69824945D1 DE 69824945 D1 DE69824945 D1 DE 69824945D1 DE 69824945 T DE69824945 T DE 69824945T DE 69824945 T DE69824945 T DE 69824945T DE 69824945 D1 DE69824945 D1 DE 69824945D1
Authority
DE
Germany
Prior art keywords
control devices
aircraft control
automatic compensation
compensation
aircraft
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.)
Expired - Lifetime
Application number
DE69824945T
Other languages
English (en)
Inventor
Saiz Manuel Munoz
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of DE69824945D1 publication Critical patent/DE69824945D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/30—Balancing hinged surfaces, e.g. dynamically

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
DE69824945T 1998-01-14 1998-12-28 Flugzeugsteuerungseinrichtungen mit automatischer Kompensation Expired - Lifetime DE69824945D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES009800050A ES2156660B1 (es) 1998-01-14 1998-01-14 Mandos de vuelo con compensacion automatica.

Publications (1)

Publication Number Publication Date
DE69824945D1 true DE69824945D1 (de) 2004-08-12

Family

ID=8302377

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69824945T Expired - Lifetime DE69824945D1 (de) 1998-01-14 1998-12-28 Flugzeugsteuerungseinrichtungen mit automatischer Kompensation

Country Status (4)

Country Link
US (1) US6109567A (de)
EP (1) EP0937641B1 (de)
DE (1) DE69824945D1 (de)
ES (1) ES2156660B1 (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7509740B2 (en) * 2001-11-13 2009-03-31 The Boeing Company Method of manufacturing a wing
US6314630B1 (en) * 1996-03-22 2001-11-13 The Boeing Company Determinant wing assembly
DE69718659T2 (de) 1996-10-22 2003-05-22 Boeing Co Flugzeug mit ungepfeiltem schlitzflügel für den reiseflug
US6484971B2 (en) * 2000-07-24 2002-11-26 Thombi Layukallo Control of flow separation and related phenomena on aerodynamic surfaces
DE10147827A1 (de) * 2001-09-27 2003-04-24 Airbus Gmbh Vorrichtung zur Änderung der Quertriebsgröße eines Flugzeughauptelementes mit vorzugsweise flächenförmiger Hinterkante
US7258308B2 (en) * 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
FR2853622B1 (fr) * 2003-04-14 2005-05-27 Eurocopter France Volet rotatif et element sustentateur, en particulier pale d'helicoptere, muni d'un tel volet rotatif
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US6978971B1 (en) * 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
FR2929590B1 (fr) * 2008-04-02 2011-01-14 Airbus France Ensemble de surfaces aerodynamiques pour aeronef.
FR2930235B1 (fr) * 2008-04-21 2011-09-30 Airbus France Mat de suspension pour turbomoteur.
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
US8844879B2 (en) * 2011-12-12 2014-09-30 The Boeing Company Wing variable camber trailing edge tip
JP5906158B2 (ja) * 2012-08-10 2016-04-20 一般社団法人日本航空宇宙工業会 フラップ
CN102901595B (zh) * 2012-10-12 2014-07-16 中国航空工业集团公司沈阳飞机设计研究所 一种舵面铰链力矩测量方法
US10633078B2 (en) * 2017-12-07 2020-04-28 The Boeing Company Pre-deformed aircraft spoilers and droop panels designed to seal with flap in deflected state
CN108016591A (zh) * 2017-12-30 2018-05-11 镇江同舟螺旋桨有限公司 一种稍部折翼形螺旋桨叶片稍部造型装置
US11260958B2 (en) * 2019-09-04 2022-03-01 The Boeing Company Double over center crankshaft flap mechanism

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR360273A (fr) * 1905-12-09 1906-04-18 Fritz Reichenbach Commande de régulateur
US1413258A (en) * 1919-02-06 1922-04-18 Christmas Aeroplane Company In Flying machine
GB346251A (en) * 1930-08-27 1931-04-09 Ugo Antoni Improvements in and relating to the construction of flexible aeroplane wings having a variable profile
US3987984A (en) * 1973-04-09 1976-10-26 Albert George Fischer Semi-rigid aircraft wing
US3994452A (en) * 1974-03-28 1976-11-30 The Boeing Company Variable camber airfoil
US4053124A (en) * 1975-08-22 1977-10-11 The Boeing Company Variable camber airfoil
US5115996A (en) * 1990-01-31 1992-05-26 Moller International, Inc. Vtol aircraft
US5335886A (en) * 1992-01-30 1994-08-09 The United States Of America As Represented By The Seceretary Of The Navy Lift enhancement device
US5794893A (en) * 1995-06-07 1998-08-18 Northrop Grumman Corporation Elastomeric transition for aircraft control surface

Also Published As

Publication number Publication date
ES2156660B1 (es) 2002-02-16
ES2156660A1 (es) 2001-07-01
EP0937641A2 (de) 1999-08-25
EP0937641A3 (de) 2000-05-10
US6109567A (en) 2000-08-29
EP0937641B1 (de) 2004-07-07

Similar Documents

Publication Publication Date Title
DE69824945D1 (de) Flugzeugsteuerungseinrichtungen mit automatischer Kompensation
DE69915588D1 (de) Fernsteuervorrichtung mit ortsabhängiger schnittstelle
DE69817144D1 (de) Automatische Ölzuführungvorrichtung mit zentaler Steuervorrichtung
DE69819992D1 (de) Steuerungssystem mit Knoten
DE69838955D1 (de) Implantat mit durchflussregelung
DE69939393D1 (de) Positionssteuerung
DE69826289D1 (de) Mikroverkapselte ngf zusammensetzungen mit geregelter freigabe
DE69714476T2 (de) Schalttafel mit zusammenschnappbarer konstruktion
DE69721105D1 (de) Automatische Türsteuerung
DE69935091D1 (de) Fernbedienung
DE69510882T2 (de) Automatische Getriebesteuerung
DE59913540D1 (de) Niveauregeleinrichtung
DE69404763D1 (de) Gerät zur automatischen Flugzeugsteuerung
DE69913602D1 (de) Flugzeug mit verminderter Flügelbelastung
DE69401854D1 (de) Gerät zur automatischen Flugzeugsteuerung
DE69919553D1 (de) Empfänger mit offenem regelkreis
DE29720492U1 (de) Steuerungsanordnung mit separatem Multiplexer
DE29903698U1 (de) Uhrengehäuse mit Steuermitteln
DE69906424D1 (de) Optoelektronische Flugzeugsteuerungshilfevorrichtung
FR2782045B1 (fr) Servofrein automatique
DE69939089D1 (de) Schnittstellenschaltung mit steuerung der anstiegszeit
DE59912070D1 (de) Funkgerät mit fernbedienung
DE29806094U1 (de) Beleuchtungssystem mit Bedienelement
DE29817101U1 (de) Bedienteil
DE69903902T2 (de) Flugsteuerungssystem

Legal Events

Date Code Title Description
8332 No legal effect for de