FR3008953B1 - Aeronef a entrainement ameliore du systeme hypersustentateur - Google Patents

Aeronef a entrainement ameliore du systeme hypersustentateur Download PDF

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Publication number
FR3008953B1
FR3008953B1 FR1457157A FR1457157A FR3008953B1 FR 3008953 B1 FR3008953 B1 FR 3008953B1 FR 1457157 A FR1457157 A FR 1457157A FR 1457157 A FR1457157 A FR 1457157A FR 3008953 B1 FR3008953 B1 FR 3008953B1
Authority
FR
France
Prior art keywords
aircraft
driving device
hypersustent
improved training
lift 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.)
Active
Application number
FR1457157A
Other languages
English (en)
Other versions
FR3008953A1 (fr
Inventor
Bernhard Hauber
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.)
Liebherr Aerospace Lindenberg GmbH
Original Assignee
Liebherr Aerospace Lindenberg GmbH
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 Liebherr Aerospace Lindenberg GmbH filed Critical Liebherr Aerospace Lindenberg GmbH
Publication of FR3008953A1 publication Critical patent/FR3008953A1/fr
Application granted granted Critical
Publication of FR3008953B1 publication Critical patent/FR3008953B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/341—Transmitting means without power amplification or where power amplification is irrelevant mechanical having duplication or stand-by provisions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/36—Transmitting means without power amplification or where power amplification is irrelevant fluid
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Transmission Devices (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Eletrric Generators (AREA)

Abstract

L'invention se rapporte à un aéronef. Celui-ci comprend au moins un système hypersustentateur qui est agencé à l'aile de l'aéronef et qui comprend un dispositif d'entraînement pour la conversion de l'énergie électrique ou hydraulique en un mouvement de rotation à vitesse contrôlée. L'aéronef présente en outre au moins une unité de commande qui commande le système hypersustentateur, où le dispositif d'entraînement comprend un dispositif d'entraînement principal (10) et un dispositif d'entraînement alternatif, le dispositif d'entraînement alternatif (12), étant alimenté par une source d'énergie décentralisée (18). L'invention est applicable en particulier dans le domaine de l'aéronautique.
FR1457157A 2013-07-26 2014-07-24 Aeronef a entrainement ameliore du systeme hypersustentateur Active FR3008953B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102013012505.7 2013-07-26
DE102013012505 2013-07-26

Publications (2)

Publication Number Publication Date
FR3008953A1 FR3008953A1 (fr) 2015-01-30
FR3008953B1 true FR3008953B1 (fr) 2019-01-25

Family

ID=52274126

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1457157A Active FR3008953B1 (fr) 2013-07-26 2014-07-24 Aeronef a entrainement ameliore du systeme hypersustentateur

Country Status (4)

Country Link
US (1) US9352825B2 (fr)
CA (1) CA2857145C (fr)
DE (1) DE102014010356B4 (fr)
FR (1) FR3008953B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106741863B (zh) * 2016-11-17 2019-04-02 中国商用飞机有限责任公司 飞机的高升力系统
EP3653493B1 (fr) * 2018-11-16 2023-01-18 Bombardier Inc. Système d'actionnement pour hypersustentateurs avec actionnement centralisé des hypersustentateurs intérieurs et actionnement indépendant des hypersustentateurs extérieurs
US11383824B2 (en) 2019-05-22 2022-07-12 Honeywell International Inc. Actuator systems and methods for flight control surface

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004047008A1 (de) * 2004-09-28 2006-03-30 Liebherr-Aerospace Lindenberg Gmbh Vorrichtung zur Einstellung von Flugzeughöhenflossen
JP4890845B2 (ja) 2005-12-08 2012-03-07 ナブテスコ株式会社 アクチュエータ機構
US8335600B2 (en) 2007-12-14 2012-12-18 The Boeing Company Regenerative integrated actuation system and associated method
DE102008022092A1 (de) 2008-05-05 2009-11-19 Airbus Deutschland Gmbh Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse
US8789791B2 (en) 2008-06-10 2014-07-29 Lockheed Martin Corporation Electrical system and electrical accumulator for electrical actuation and related methods
GB0914576D0 (en) * 2009-08-20 2009-09-30 Airbus Operations Ltd Apparatus for use on an aircraft
DE102010021576A1 (de) * 2010-05-26 2011-12-01 Airbus Operations Gmbh Vorrichtung für eine Stellklappe eines Tragflügels
DE102012005346B4 (de) 2012-03-16 2023-08-24 Liebherr-Aerospace Lindenberg Gmbh Flugzeug
EP2690007B1 (fr) * 2012-07-26 2016-08-31 Airbus Operations GmbH Procédé de production d'énergie hydraulique dans un aéronef, utilisation d'une unité de commande d'énergie hybride et d'un système d'entraînement

Also Published As

Publication number Publication date
CA2857145A1 (fr) 2015-01-26
DE102014010356B4 (de) 2022-11-10
FR3008953A1 (fr) 2015-01-30
CA2857145C (fr) 2021-02-09
DE102014010356A1 (de) 2015-01-29
US20150076282A1 (en) 2015-03-19
US9352825B2 (en) 2016-05-31

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