BRPI0518305A2 - mÉtodo e sistema para monitoramento das condiÇÕes de funcionamento da engrenagem de aterrissagem de uma aeronave - Google Patents

mÉtodo e sistema para monitoramento das condiÇÕes de funcionamento da engrenagem de aterrissagem de uma aeronave

Info

Publication number
BRPI0518305A2
BRPI0518305A2 BRPI0518305-7A BRPI0518305A BRPI0518305A2 BR PI0518305 A2 BRPI0518305 A2 BR PI0518305A2 BR PI0518305 A BRPI0518305 A BR PI0518305A BR PI0518305 A2 BRPI0518305 A2 BR PI0518305A2
Authority
BR
Brazil
Prior art keywords
landing gear
monitoring
aircraft
operating conditions
conditions
Prior art date
Application number
BRPI0518305-7A
Other languages
English (en)
Inventor
Robert Kyle Schmidt
Steven A Gedeon
Original Assignee
Messier Dowty Inc
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 Messier Dowty Inc filed Critical Messier Dowty Inc
Publication of BRPI0518305A2 publication Critical patent/BRPI0518305A2/pt

Links

Classifications

    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00—Registering or indicating the working of vehicles
    • G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
    • G07C5/0808—Diagnosing performance data
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01G—WEIGHING
    • G01G19/00—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups
    • G01G19/02—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles
    • G01G19/07—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles for weighing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/008—Devices for detecting or indicating hard landing

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

MÉTODO E SISTEMA PARA MONITORAMENTO DAS CONDIÇÕES DE FUMCIONAMENTO DA ENGRENAGEM DE ATERRISSAGEM DE UMA AERONAVE. A invenção refere-se a um método e um sistema novos para monitorar as condições de funcionamento da engrenagem de aterrissagem de uma aeronave. O sistema incluí sensores que são presos à estrutura e equipamento da engrenagem de aterrissagem (como, por exemplo, um ou mais de freios, pneumáticos, componentes hidráulicos, sistemas e comutadores elétricos) e analisados de modo a se reportar e alertar o pessoal, como, por exemplo, pilotos, pessoal da manutenção, operadores de linhas aéreas, tripulação na terra e autoridades reguladoras, das condições de funcionamento da engrenagem de aterrissagem e da necessidade potencial de assistência técnica, manutenção ou substituição. O sistema monitora e reporta problemas críticos referentes às condições de funcionamento como informações em tempo real que podem ser analisadas em conjunto com um banco de dados de informações extensivo e utilizadas para alertar os pilotos ou outro pessoal relevante sobre a condição da engrenagem de aterrissagem e as providências que, consequentemente, podem ser necessárias.
BRPI0518305-7A 2004-11-18 2005-11-18 mÉtodo e sistema para monitoramento das condiÇÕes de funcionamento da engrenagem de aterrissagem de uma aeronave BRPI0518305A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CA002487704A CA2487704A1 (en) 2004-11-18 2004-11-18 Method and system for health monitoring of aircraft landing gear
PCT/CA2005/001750 WO2006053433A1 (en) 2004-11-18 2005-11-18 Method and system for health monitoring of aircraft landing gear

Publications (1)

Publication Number Publication Date
BRPI0518305A2 true BRPI0518305A2 (pt) 2008-11-11

Family

ID=36406130

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0518305-7A BRPI0518305A2 (pt) 2004-11-18 2005-11-18 mÉtodo e sistema para monitoramento das condiÇÕes de funcionamento da engrenagem de aterrissagem de uma aeronave

Country Status (5)

Country Link
US (2) US20060144997A1 (pt)
EP (1) EP1815224A4 (pt)
BR (1) BRPI0518305A2 (pt)
CA (1) CA2487704A1 (pt)
WO (1) WO2006053433A1 (pt)

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Also Published As

Publication number Publication date
EP1815224A4 (en) 2010-03-10
EP1815224A1 (en) 2007-08-08
CA2487704A1 (en) 2006-05-18
US8262019B2 (en) 2012-09-11
WO2006053433A1 (en) 2006-05-26
US20060144997A1 (en) 2006-07-06
US20120053784A1 (en) 2012-03-01

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