ES2156660A1 - Mandos de vuelo con compensacion automatica. - Google Patents

Mandos de vuelo con compensacion automatica.

Info

Publication number
ES2156660A1
ES2156660A1 ES009800050A ES9800050A ES2156660A1 ES 2156660 A1 ES2156660 A1 ES 2156660A1 ES 009800050 A ES009800050 A ES 009800050A ES 9800050 A ES9800050 A ES 9800050A ES 2156660 A1 ES2156660 A1 ES 2156660A1
Authority
ES
Spain
Prior art keywords
aileron
flight controls
balance
automatique
rotates
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.)
Granted
Application number
ES009800050A
Other languages
English (en)
Other versions
ES2156660B1 (es
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
Priority to ES009800050A priority Critical patent/ES2156660B1/es
Priority to US09/110,744 priority patent/US6109567A/en
Priority to US09/139,524 priority patent/US6220551B1/en
Priority to EP98500280A priority patent/EP0937641B1/en
Priority to DE69824945T priority patent/DE69824945D1/de
Publication of ES2156660A1 publication Critical patent/ES2156660A1/es
Application granted granted Critical
Publication of ES2156660B1 publication Critical patent/ES2156660B1/es
Anticipated expiration legal-status Critical
Expired - Fee Related 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)

Abstract

Mandos de vuelo con compensación automática que consiste en alerones formados de dos partes, los cuales a baja velocidad adoptan una forma de alerón convencional y giran en su totalidad con el mismo ángulo y a altas velocidades una porción de él gira o se extiende a un ángulo determinado movido por el actuador y el resto del alerón, que es flexible y está unido a la porción principal del alerón al que está integrado, gira respecto a la porción principal en función de la presión del aire, oponiendose a este giro por medio de su disposición flexible.
ES009800050A 1998-01-14 1998-01-14 Mandos de vuelo con compensacion automatica. Expired - Fee Related ES2156660B1 (es)

Priority Applications (5)

Application Number Priority Date Filing Date Title
ES009800050A ES2156660B1 (es) 1998-01-14 1998-01-14 Mandos de vuelo con compensacion automatica.
US09/110,744 US6109567A (en) 1998-01-14 1998-07-02 Flight controls with automatic balance
US09/139,524 US6220551B1 (en) 1998-01-14 1998-08-25 Flight controls with automatic balance
EP98500280A EP0937641B1 (en) 1998-01-14 1998-12-28 Flight controls with automatique balance
DE69824945T DE69824945D1 (de) 1998-01-14 1998-12-28 Flugzeugsteuerungseinrichtungen mit automatischer Kompensation

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 (2)

Publication Number Publication Date
ES2156660A1 true ES2156660A1 (es) 2001-07-01
ES2156660B1 ES2156660B1 (es) 2002-02-16

Family

ID=8302377

Family Applications (1)

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

Country Status (4)

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

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* 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
WO1997034734A1 (en) * 1996-03-22 1997-09-25 The Boeing Company Determinant wing assembly
USRE44313E1 (en) 1996-10-22 2013-06-25 The Boeing Company Airplane with unswept slotted cruise wing airfoil
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
US7059563B2 (en) 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US7243881B2 (en) 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7357358B2 (en) 2004-02-27 2008-04-15 The Boeing Company Aircraft leading edge device systems and corresponding sizing methods
US7270305B2 (en) 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding 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
US7322547B2 (en) 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7300021B2 (en) 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US7500641B2 (en) 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
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
US7578484B2 (en) 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and 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

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
GB360273A (es) * 1930-01-21 1931-11-05 Jacques Gerin
US4053124A (en) * 1975-08-22 1977-10-11 The Boeing Company Variable camber airfoil
US5335886A (en) * 1992-01-30 1994-08-09 The United States Of America As Represented By The Seceretary Of The Navy Lift enhancement device

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US5115996A (en) * 1990-01-31 1992-05-26 Moller International, Inc. Vtol aircraft
US5794893A (en) * 1995-06-07 1998-08-18 Northrop Grumman Corporation Elastomeric transition for aircraft control surface

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1413258A (en) * 1919-02-06 1922-04-18 Christmas Aeroplane Company In Flying machine
GB360273A (es) * 1930-01-21 1931-11-05 Jacques Gerin
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
US4053124A (en) * 1975-08-22 1977-10-11 The Boeing Company Variable camber airfoil
US5335886A (en) * 1992-01-30 1994-08-09 The United States Of America As Represented By The Seceretary Of The Navy Lift enhancement device

Also Published As

Publication number Publication date
EP0937641A3 (en) 2000-05-10
EP0937641B1 (en) 2004-07-07
US6109567A (en) 2000-08-29
ES2156660B1 (es) 2002-02-16
EP0937641A2 (en) 1999-08-25
DE69824945D1 (de) 2004-08-12

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