BR112013027295A2 - conjunto de monitoramento para detectar defeitos estruturais que podem aparecer em uma nacela de avião em serviço e método de monitoramento - Google Patents

conjunto de monitoramento para detectar defeitos estruturais que podem aparecer em uma nacela de avião em serviço e método de monitoramento

Info

Publication number
BR112013027295A2
BR112013027295A2 BR112013027295A BR112013027295A BR112013027295A2 BR 112013027295 A2 BR112013027295 A2 BR 112013027295A2 BR 112013027295 A BR112013027295 A BR 112013027295A BR 112013027295 A BR112013027295 A BR 112013027295A BR 112013027295 A2 BR112013027295 A2 BR 112013027295A2
Authority
BR
Brazil
Prior art keywords
monitoring
appear
structural defects
signals
monitoring method
Prior art date
Application number
BR112013027295A
Other languages
English (en)
Inventor
Maalioune Hakim
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Publication of BR112013027295A2 publication Critical patent/BR112013027295A2/pt

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/44—Processing the detected response signal, e.g. electronic circuits specially adapted therefor
    • G01N29/4445—Classification of defects
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0033—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining damage, crack or wear
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0066—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by exciting or detecting vibration or acceleration
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0091—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by using electromagnetic excitation or detection
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/04—Analysing solids
    • G01N29/12—Analysing solids by measuring frequency or resonance of acoustic waves

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Immunology (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • Pathology (AREA)
  • Electromagnetism (AREA)
  • Acoustics & Sound (AREA)
  • Signal Processing (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Abstract

conjunto de monitoramento para detectar defeitos estruturais que podem aparecer em uma nacela de avião em serviço e método de monitoramento a invenção refere-se a uma unidade de monitoramento (11) que inclui uma estrutura de impressão de compósito (10) formando uma porção da necela de avião (1), uma pluralidade de sensores (14) para gerar sinais representativos de uma amplitude e/ou frequência de vibrações. cada sensor (14) transmite referidos sinais por meio de ondas eletromagnéticas, por exemplo, por radiofrequências. cada sensor (14) é um microssistema eletromecânico incluindo um meio para converter energia mecânica em energia elétrica. uma unidade de computação (15) é adequada para : avaliar as diferenças entre uma função de transferência de corrente resultando dos referidos sinais e uma função de transferência nominal predeterminada; comparando cada uma das referidas diferenças com um limite de detecção respectivo; e, da referida comparação, estimar ou avaliar o tamanho e/ou posição do referido estrutural na estrutura (10).
BR112013027295A 2011-05-02 2012-04-12 conjunto de monitoramento para detectar defeitos estruturais que podem aparecer em uma nacela de avião em serviço e método de monitoramento BR112013027295A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1153717A FR2974900B1 (fr) 2011-05-02 2011-05-02 Ensemble et procede de surveillance pour detecter des defauts structurels pouvant apparaitre dans une nacelle d'aeronef
PCT/FR2012/050799 WO2012150394A1 (fr) 2011-05-02 2012-04-12 Ensemble et procede de surveillance pour detecter des defauts structurels pouvant apparaitre dans une nacelle d'aeronef en service

Publications (1)

Publication Number Publication Date
BR112013027295A2 true BR112013027295A2 (pt) 2019-02-12

Family

ID=46146907

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013027295A BR112013027295A2 (pt) 2011-05-02 2012-04-12 conjunto de monitoramento para detectar defeitos estruturais que podem aparecer em uma nacela de avião em serviço e método de monitoramento

Country Status (8)

Country Link
US (1) US20140053649A1 (pt)
EP (1) EP2705343A1 (pt)
CN (1) CN103534569A (pt)
BR (1) BR112013027295A2 (pt)
CA (1) CA2834757A1 (pt)
FR (1) FR2974900B1 (pt)
RU (1) RU2013152414A (pt)
WO (1) WO2012150394A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105241959A (zh) * 2015-10-19 2016-01-13 中北大学 一种基于阵列阻抗特性的复合材料缺陷检测系统
FR3050876B1 (fr) * 2016-04-28 2019-07-05 Turbomeca Capot pour moteur d'aeronef comprenant une antenne de lecteur de radio-identification
US10816436B2 (en) * 2018-07-06 2020-10-27 The Boeing Company System for temperature insensitive damage detection
US10958542B2 (en) * 2018-10-30 2021-03-23 United Technologies Corporation System for active data acquisition management in a gas turbine engine
EP3748327A1 (en) * 2019-06-07 2020-12-09 Ostbayerische Technische Hochschule Regensburg Method and system for evaluating a structural integrity of an aerial vehicle
US20230061579A1 (en) * 2021-08-24 2023-03-02 Woodward, Inc. Jam detection and jam tolerant motion control

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE181401T1 (de) * 1992-08-10 1999-07-15 Dow Deutschland Inc Vorrichtung zur verkrustungsdetektion eines axialverdichters.
US6006163A (en) * 1997-09-15 1999-12-21 Mcdonnell Douglas Corporation Active damage interrogation method for structural health monitoring
US7668667B2 (en) * 2005-03-07 2010-02-23 Microstrain, Inc. Miniature stimulating and sensing system
US7276703B2 (en) * 2005-11-23 2007-10-02 Lockheed Martin Corporation System to monitor the health of a structure, sensor nodes, program product, and related methods
FR2901610B1 (fr) * 2006-05-24 2009-01-16 Airbus France Sas Dispositif de controle non destructif d'une struture par analyse vibratoire
US7860664B2 (en) * 2008-04-15 2010-12-28 Spirit Aerosystems, Inc. System and method for self-contained structural health monitoring for composite structures
US8387469B2 (en) * 2009-01-22 2013-03-05 Florida State University Research Foundation Systems, methods, and apparatus for structural health monitoring

Also Published As

Publication number Publication date
WO2012150394A1 (fr) 2012-11-08
RU2013152414A (ru) 2015-06-10
CN103534569A (zh) 2014-01-22
US20140053649A1 (en) 2014-02-27
CA2834757A1 (fr) 2012-11-08
FR2974900A1 (fr) 2012-11-09
FR2974900B1 (fr) 2013-05-17
EP2705343A1 (fr) 2014-03-12

Similar Documents

Publication Publication Date Title
BR112013027295A2 (pt) conjunto de monitoramento para detectar defeitos estruturais que podem aparecer em uma nacela de avião em serviço e método de monitoramento
EP3112857A3 (en) Ultrasonic test system, ultrasonic test method and aircraft structural object
WO2013102079A3 (en) Enhanced printer functionality and maintenance with dynamic identifier code
BR112014012286A2 (pt) método para controlar o arranjo de iluminação de voo de um parque eólico, e, uso de um dispositivo de monitoração acústica
NZ631607A (en) Buildings with wind-energy-conversion systems
WO2012015614A3 (en) System and method for monitoring a wind turbine gearbox
GB201203273D0 (en) Monitoring transport network infrastructure
EP2506083A3 (en) Fuser unit
WO2016039202A8 (ja) 鉄道車両用軸受異常検知システム
WO2011163316A3 (en) Method and system for detecting pushrod faults
WO2012044161A3 (en) Method and system for wind gust detection in a wind turbine
WO2012021202A3 (en) Real time active helicopter vibration control and rotor track and balance systems
TR201910357T4 (tr) Aletli sönümleyici ve bu tür bir sönümleyiciyi içeren performans takip sistemi.
BR112013009576A8 (pt) Dispositivo e método para monitoração de componentes giratórios e rotor de uma bomba centrífuga equipado com o dito dispositivo
SG10201811452VA (en) Systems and methods for braking or launching a ride vehicle
EP2660614A3 (en) Systems and methods to detect generator collector flashover
EP2492892A3 (en) Aircraft systems and methods for providing exhaust warnings
EP2610604A3 (en) Method for oscillation measurement on rotor blades of wind power installations
WO2015015262A8 (en) Method for attachment of a pre-assembled powerplant and pylon assembly to an aircraft
CN202789321U (zh) 一种能够对主轴的裂缝进行监测的风力涡轮机
MX2013010106A (es) Metodo para operar una central termoelectrica.
BR112013007197A2 (pt) método para transmissão sem contato de energia elétrica e/ou de sinais elétricos entre uma parede e uma folha fixada na referida parede, e, dispositivo para realizar o mesmo
WO2013041484A3 (de) Verfahren und einrichtung zur detektion eines inselbetriebs von energieerzeugungsanlagen
EP2792596A3 (en) Harmonic data transfer in rotary wing aircraft
Schubert et al. Source mechanisms of acoustic emissions as an indicator of injury during a full scale fatigue test of a wind turbine rotor blade

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 5A, 6A E 7A ANUIDADES.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2515 DE 19-03-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.

B350 Update of information on the portal [chapter 15.35 patent gazette]