BR112023026714A2 - Método e aparelho para realização de monitoramento de integridade - Google Patents

Método e aparelho para realização de monitoramento de integridade

Info

Publication number
BR112023026714A2
BR112023026714A2 BR112023026714A BR112023026714A BR112023026714A2 BR 112023026714 A2 BR112023026714 A2 BR 112023026714A2 BR 112023026714 A BR112023026714 A BR 112023026714A BR 112023026714 A BR112023026714 A BR 112023026714A BR 112023026714 A2 BR112023026714 A2 BR 112023026714A2
Authority
BR
Brazil
Prior art keywords
control surface
load
load sensor
integrity monitoring
flight control
Prior art date
Application number
BR112023026714A
Other languages
English (en)
Inventor
Andreas Fleddermann
Christian Kohlöffel
Van Balen Elko
Arend Van Bruggen Jan
Tobias Hartmann
Original Assignee
Airbus Operations Gmbh
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 Airbus Operations Gmbh, Liebherr Aerospace Lindenberg GmbH filed Critical Airbus Operations Gmbh
Publication of BR112023026714A2 publication Critical patent/BR112023026714A2/pt

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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • 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
    • B64C13/40—Transmitting means with power amplification using fluid pressure
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60—Testing or inspecting aircraft components or systems
    • 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
    • B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Braking Arrangements (AREA)
  • Tires In General (AREA)

Abstract

método e aparelho para realização de monitoramento de integridade. a fim de reduzir o trabalho de manutenção e melhorar a confiabilidade a longo prazo, a invenção fornece um método de monitoramento de integridade para verificar a funcionalidade de um aparelho de acionamento da superfície de controle de voo (104) usando pelo menos um sensor de carga (110) para detectar uma carga imposta em um dispositivo de acionamento da superfície de controle (106), o método compreendendo pelo menos uma das etapas: a) bloquear o movimento do dispositivo de transmissão (108) por meio de um dispositivo de freio (118), b) comandar o dispositivo de acionamento da superfície de controle (106) para aplicar uma carga no dispositivo de transmissão bloqueado (108), e c) determinar se pelo menos um sinal de saída do sensor de carga (62) de pelo menos um sensor de carga (110) está dentro de uma faixa predeterminada. além disso, são descritos um aparelho de acionamento da superfície de controle de voo (104), um sistema de controle de voo (100) e uma aeronave (10) compreendendo um dispositivo de controle (112) configurado para comandar automaticamente a condução de tal método de monitoramento de integridade.
BR112023026714A 2021-06-29 2022-06-27 Método e aparelho para realização de monitoramento de integridade BR112023026714A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP21182478.4A EP4112452A1 (en) 2021-06-29 2021-06-29 Method and apparatus for conducting health monitoring
PCT/EP2022/067485 WO2023274914A1 (en) 2021-06-29 2022-06-27 Method and apparatus for conducting health monitoring

Publications (1)

Publication Number Publication Date
BR112023026714A2 true BR112023026714A2 (pt) 2024-03-12

Family

ID=76708095

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112023026714A BR112023026714A2 (pt) 2021-06-29 2022-06-27 Método e aparelho para realização de monitoramento de integridade

Country Status (4)

Country Link
EP (1) EP4112452A1 (pt)
CN (1) CN117715826A (pt)
BR (1) BR112023026714A2 (pt)
WO (1) WO2023274914A1 (pt)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3037346B1 (en) * 2014-12-22 2018-10-24 Airbus Operations GmbH Method for testing a component in a high lift system of an aircraft
EP3037347B1 (en) * 2014-12-22 2019-02-06 Airbus Operations GmbH Method for determining a state of a component in a high lift system of an aircraft
US10336437B2 (en) * 2017-05-05 2019-07-02 Hamilton Sundstrand Corporation Method to measure aircraft high-lift system brake response time

Also Published As

Publication number Publication date
EP4112452A1 (en) 2023-01-04
WO2023274914A1 (en) 2023-01-05
CN117715826A (zh) 2024-03-15

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