ES2188476T3 - Sistema de impulsion de una superficie de alto esfuerzo ascensional en un avion. - Google Patents

Sistema de impulsion de una superficie de alto esfuerzo ascensional en un avion.

Info

Publication number
ES2188476T3
ES2188476T3 ES00301400T ES00301400T ES2188476T3 ES 2188476 T3 ES2188476 T3 ES 2188476T3 ES 00301400 T ES00301400 T ES 00301400T ES 00301400 T ES00301400 T ES 00301400T ES 2188476 T3 ES2188476 T3 ES 2188476T3
Authority
ES
Spain
Prior art keywords
ascensional
airplane
coupling
drive
stress
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
ES00301400T
Other languages
English (en)
Inventor
Valentin G Barba
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.)
GE Aviation Systems LLC
Original Assignee
Smiths Aerospace LLC
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 Smiths Aerospace LLC filed Critical Smiths Aerospace LLC
Application granted granted Critical
Publication of ES2188476T3 publication Critical patent/ES2188476T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Multiple Motors (AREA)
  • Transmission Devices (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Current-Collector Devices For Electrically Propelled Vehicles (AREA)

Abstract

Sistema de impulsión de una superficie de alto esfuerzo ascensional en un avión, que comprende: un primer motor eléctrico (M1) para su acoplamiento de impulsión a una primera superficie de elevado esfuerzo ascensional (10); un segundo motor eléctrico (M2) destinado a su acoplamiento de accionamiento a una segunda superficie de alto esfuerzo ascensional (20); y un dispositivo (50) para asegurar el movimiento sincronizado de dichas primera y segunda superficies de alto esfuerzo ascensional, de manera que dichos medios están destinados a su acoplamiento mecánico entre dichas primera y segundas superficies de alto esfuerzo ascensional, caracterizándose porque dichos primero y segundo motores eléctricos están eléctricamente conectados en serie entre sí.
ES00301400T 1999-02-26 2000-02-22 Sistema de impulsion de una superficie de alto esfuerzo ascensional en un avion. Expired - Lifetime ES2188476T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/258,470 US6224022B1 (en) 1999-02-26 1999-02-26 Airplane high lift surface drive system

Publications (1)

Publication Number Publication Date
ES2188476T3 true ES2188476T3 (es) 2003-07-01

Family

ID=22980686

Family Applications (1)

Application Number Title Priority Date Filing Date
ES00301400T Expired - Lifetime ES2188476T3 (es) 1999-02-26 2000-02-22 Sistema de impulsion de una superficie de alto esfuerzo ascensional en un avion.

Country Status (5)

Country Link
US (1) US6224022B1 (es)
EP (1) EP1038765B1 (es)
AT (1) ATE228459T1 (es)
DE (1) DE60000839T2 (es)
ES (1) ES2188476T3 (es)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9903500D0 (en) * 1999-02-17 1999-04-07 Lucas Ind Plc Detection apparatus
DE10313728B4 (de) * 2003-03-27 2011-07-21 Airbus Operations GmbH, 21129 Klappensystem am Tragflügel eines Starrflügel-Flugzeuges
US20040200928A1 (en) * 2003-04-14 2004-10-14 Arthur Degenholtz Actuator and flap arrangement with actuator interconnection
DE10361891A1 (de) 2003-12-23 2005-08-04 Airbus Deutschland Gmbh Vorrichtung zur Ansteuerung und Verstellung von Klappen an Flugzeugtragflächen
DE102005008331A1 (de) * 2005-02-23 2006-08-31 Airbus Deutschland Gmbh Einrichtung zur Bestimmung eines Rotationswinkels einer Welle in einem Luftfahrzeug
DE102005018686B4 (de) * 2005-04-21 2007-03-22 Barthelt, Hans-Peter, Dipl.-Ing. Pflegebett mit Doppelmotorantrieb
US20070007385A1 (en) * 2005-06-27 2007-01-11 Honeywell International, Inc. Electric flight control surface actuation system electronic architecture
DE102005059369B4 (de) * 2005-12-13 2012-06-14 Airbus Operations Gmbh Verfahren und Einrichtung zur automatischen Entlastung eines Hochauftriebsflächensystems, insbesondere eines Landeklappensystems, eines Flugzeugs
FR2972175B1 (fr) * 2011-03-01 2013-10-25 Sagem Defense Securite Procede de commande simultanee d'actionneurs de deplacement de volets d'aeronef, dispositif de motorisation de volets d'aeronef et aeronef pourvu d'un tel dispositif
EP4393815A1 (en) * 2022-12-30 2024-07-03 Airbus Operations GmbH Aircraft flap system

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1373873A (en) * 1920-05-29 1921-04-05 Gen Electric Ship propulsion
US1407425A (en) * 1920-06-28 1922-02-21 Junkers Hugo Stabilization of flying machines
US1802184A (en) * 1922-11-01 1931-04-21 Gen Electric Propulsion of multiple-screw ships
US1856093A (en) * 1931-03-17 1932-05-03 Merrill Aircraft Company Airplane
FR857515A (fr) * 1938-09-14 1940-09-17 Dornier Werke Gmbh Gouvernail commandé par moteur
US3935754A (en) 1974-06-14 1976-02-03 The Boeing Company Failure detector and indicator for aircraft flap actuation system
US3958779A (en) * 1975-05-27 1976-05-25 Fairchild Industries Inc. Aircraft control system with a jam isolating coupling
US4159642A (en) * 1978-03-02 1979-07-03 Avco Corporation Aircraft transmission test set
US4398683A (en) * 1978-12-26 1983-08-16 Schmetzer William M Aircraft with thrust and lift augmenting airfoil
US4688744A (en) * 1982-09-03 1987-08-25 Sundstrand Corporation Jam tolerant rotary actuation system
DE3464875D1 (en) 1983-12-20 1987-08-27 Lucas Ind Plc Braking arrangement for a rotary drive system
US4695014A (en) * 1984-05-25 1987-09-22 Western Gear Corporation Aircraft wing section movement apparatus
US4779822A (en) * 1986-05-23 1988-10-25 Sundstrand Corporation Actuator system
JPH0667738B2 (ja) * 1986-12-09 1994-08-31 東海テイ−ア−ルダブリユ−株式会社 電動機制動機能を備えた電動パワ−ステアリング装置
IL90789A0 (en) * 1988-08-05 1990-01-18 Rieter Ag Maschf Textile machine with drawframes
DE4033277A1 (de) 1990-10-19 1992-04-23 Airbus Gmbh Antriebsvorrichtung fuer an flugzeugtragfluegeln angeordneten klappen
US5884872A (en) * 1993-05-26 1999-03-23 The United States Of America As Represented By The Secretary Of The Navy Oscillating flap lift enhancement device
US5686907A (en) * 1995-05-15 1997-11-11 The Boeing Company Skew and loss detection system for individual high lift devices
DE19525593C2 (de) * 1995-07-13 1997-04-30 Roland Man Druckmasch Mehrmotorenantrieb für eine Druckmaschine
JP3536658B2 (ja) * 1998-03-31 2004-06-14 日産自動車株式会社 ハイブリッド車両の駆動制御装置

Also Published As

Publication number Publication date
EP1038765A1 (en) 2000-09-27
ATE228459T1 (de) 2002-12-15
US6224022B1 (en) 2001-05-01
DE60000839T2 (de) 2003-09-25
DE60000839D1 (de) 2003-01-09
EP1038765B1 (en) 2002-11-27

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