ATE525282T1 - FLUGSTEUERUNGSSYSTEM FÜR ßMEHR ELEKTRISCHß FLUGZEUG - Google Patents

FLUGSTEUERUNGSSYSTEM FÜR ßMEHR ELEKTRISCHß FLUGZEUG

Info

Publication number
ATE525282T1
ATE525282T1 AT10150044T AT10150044T ATE525282T1 AT E525282 T1 ATE525282 T1 AT E525282T1 AT 10150044 T AT10150044 T AT 10150044T AT 10150044 T AT10150044 T AT 10150044T AT E525282 T1 ATE525282 T1 AT E525282T1
Authority
AT
Austria
Prior art keywords
flight control
generators
control system
powered
servo controls
Prior art date
Application number
AT10150044T
Other languages
English (en)
Inventor
Marc Fervel
Alexandre Gentilhomme
Original Assignee
Airbus Operations Sas
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 Airbus Operations Sas filed Critical Airbus Operations Sas
Application granted granted Critical
Publication of ATE525282T1 publication Critical patent/ATE525282T1/de

Links

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
    • 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
    • B64C13/504—Transmitting means with power amplification using electrical energy using electro-hydrostatic actuators [EHA's]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Toys (AREA)
AT10150044T 2009-01-08 2010-01-04 FLUGSTEUERUNGSSYSTEM FÜR ßMEHR ELEKTRISCHß FLUGZEUG ATE525282T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0950081A FR2940787A1 (fr) 2009-01-08 2009-01-08 Systeme de commandes de vol plus electrique a bord d'un aeronef

Publications (1)

Publication Number Publication Date
ATE525282T1 true ATE525282T1 (de) 2011-10-15

Family

ID=40942477

Family Applications (1)

Application Number Title Priority Date Filing Date
AT10150044T ATE525282T1 (de) 2009-01-08 2010-01-04 FLUGSTEUERUNGSSYSTEM FÜR ßMEHR ELEKTRISCHß FLUGZEUG

Country Status (4)

Country Link
US (1) US8740155B2 (de)
EP (1) EP2206645B1 (de)
AT (1) ATE525282T1 (de)
FR (1) FR2940787A1 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2943037B1 (fr) 2009-03-11 2012-09-21 Airbus France Systeme de commande d'aeronef a architecture modulaire integre.
FR2943036B1 (fr) 2009-03-11 2011-04-15 Airbus France Systeme distribue de commande de vol implemente selon une architecture avionique modulaire integree.
US9190942B2 (en) 2010-07-22 2015-11-17 Parker-Hannifin Corporation Near synchronous controlled induction motor drive actuation system
GB2492965B (en) 2011-07-15 2018-05-02 Agustawestland Ltd A system and method for reducing the transmission of vibration from a first vibrating body to a second body
WO2017001984A1 (en) 2015-06-30 2017-01-05 Bombardier Inc. Aircraft with distributed hydraulic system
US10889385B2 (en) 2015-09-11 2021-01-12 Bombardier Inc. Apparatus and methods for distributing electric power on an aircraft during a limited power availability condition
US10315753B2 (en) 2016-03-29 2019-06-11 The Boeing Company System and method for controlling aircraft wing flap motion
EP3650336A1 (de) 2018-11-12 2020-05-13 Goodrich Actuation Systems SAS Trimsteuerungssystem
US11524767B2 (en) * 2021-03-31 2022-12-13 Beta Air, Llc Methods and systems for flight control configured for use in an electric aircraft
US12434814B2 (en) 2021-03-10 2025-10-07 Beta Air Llc System and methods for flight control for an electric aircraft
US11952105B2 (en) 2021-03-10 2024-04-09 BETA Technologies, Inc. System and method for flight control in electric aircraft
EP4660076A1 (de) * 2024-06-04 2025-12-10 Goodrich Actuation Systems SAS Aktuatoranordnungsarchitektur

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3710218A (en) * 1970-10-08 1973-01-09 Micro Magnetic Ind Inc Induction motor speed control
US4649484A (en) * 1983-08-01 1987-03-10 The Boeing Company Avionic control system
US4994684A (en) * 1989-01-30 1991-02-19 The State Of Oregon Acting By And Through The State Board Of Higher Education On Behalf Of Oregon State University Doubly fed generator variable speed generation control system
US5054713A (en) * 1989-04-03 1991-10-08 Langley Lawrence W Circular airplane
FR2684953B1 (fr) * 1991-12-11 1994-04-01 Aerospatiale Ste Nationale Indle Dispositif a vulnerabilite reduite pour la commande d'un rotor d'helicoptere par plateaux cycliques.
US7182583B2 (en) * 2004-02-06 2007-02-27 Sauer-Danfoss Inc. Electro-hydraulic power unit with a rotary cam hydraulic power unit
US7922117B2 (en) * 2004-08-30 2011-04-12 Hamilton Sundstrand Corporation Primary panel and motor controller integration for aircraft power distribution system

Also Published As

Publication number Publication date
EP2206645B1 (de) 2011-09-21
EP2206645A1 (de) 2010-07-14
US20100170999A1 (en) 2010-07-08
FR2940787A1 (fr) 2010-07-09
US8740155B2 (en) 2014-06-03

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties