BR0309781A - Monitoramento de parâmetros em componentes estruturais - Google Patents
Monitoramento de parâmetros em componentes estruturaisInfo
- Publication number
- BR0309781A BR0309781A BR0309781-1A BR0309781A BR0309781A BR 0309781 A BR0309781 A BR 0309781A BR 0309781 A BR0309781 A BR 0309781A BR 0309781 A BR0309781 A BR 0309781A
- Authority
- BR
- Brazil
- Prior art keywords
- sensor
- memory
- data
- processor
- battery
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D9/00—Recording measured values
- G01D9/005—Solid-state data loggers
-
- 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; 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
Abstract
"MONITORAMENTO DE PARâMETROS EM COMPONENTES ESTRUTURAIS". - A presente invenção refere-se a um aparelho para o monitoramento de um parâmetro associado com um componente estrutural que compreende um módulo (1) o qual é fixável no componente estrutural e o qual está associado com um sensor (2) para fazer as medições do dito parâmetro. O módulo incorpora uma fonte de alimentação (7) para alimentar o aparelho; uma memória (4) para armazenar os dados do sensor, e um processador (3) para processar os sinais de medição do sensor (2) e armazenar os dados na dita memória (4). Um mostrador (5) para exibir as medições feitas pelo sensor (2) pode também ser provido. O processador pode fazer uso de um algoritmo tal como um algoritmo de contagem rainflow para reduzir os dados armazenados. Para a economia de energia, o sensor (2) é somente ligado conforme requerido para fazer uma medição. O sensor (2) é interfaceado com o processador através de um subsistema de processamento de sinal (6) que consiste em um amplificador e um conversor analógico para digital, e cada um é ligado e desligado conforme requerido para alimentar o sensor (2) para medição. Um sensor tal como uma chave de inclinação (8) pode também ser utilizado para controlar a alimentação do sensor (2). Uma conexão de comunicação permite o carregamento de dados da memória, e a recarga da bateria (7). Alternativamente, a memória (4) e a bateria (7) estão incorporadas em uma unidade a qual é removível do aparelho de modo que os dados na memória possam ser processados em outro lugar.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0209584A GB2387912A (en) | 2002-04-26 | 2002-04-26 | Monitoring parameters in structural components |
PCT/GB2003/001820 WO2003091682A1 (en) | 2002-04-26 | 2003-04-28 | Monitoring a parameter with low power consumption for aircraft landing gear-data logger |
Publications (1)
Publication Number | Publication Date |
---|---|
BR0309781A true BR0309781A (pt) | 2005-03-22 |
Family
ID=9935576
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR0309781-1A BR0309781A (pt) | 2002-04-26 | 2003-04-28 | Monitoramento de parâmetros em componentes estruturais |
Country Status (10)
Country | Link |
---|---|
US (1) | US7680630B2 (pt) |
EP (1) | EP1499864B1 (pt) |
AT (1) | ATE349685T1 (pt) |
AU (1) | AU2003229956A1 (pt) |
BR (1) | BR0309781A (pt) |
CA (2) | CA2483404C (pt) |
DE (1) | DE60310703T2 (pt) |
ES (1) | ES2278159T3 (pt) |
GB (1) | GB2387912A (pt) |
WO (1) | WO2003091682A1 (pt) |
Families Citing this family (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7256505B2 (en) * | 2003-03-05 | 2007-08-14 | Microstrain, Inc. | Shaft mounted energy harvesting for wireless sensor operation and data transmission |
GB2387912A (en) | 2002-04-26 | 2003-10-29 | Messier Dowty Inc | Monitoring parameters in structural components |
DE102004040407B4 (de) * | 2004-08-19 | 2008-01-31 | Thiele Gmbh & Co. Kg | Vorrichtung zur Bestimmung der Lebensdauer von maschinentechnischen Einrichtungen |
US20060004499A1 (en) * | 2004-06-30 | 2006-01-05 | Angela Trego | Structural health management architecture using sensor technology |
GB0428378D0 (en) * | 2004-12-24 | 2005-02-02 | Airbus Uk Ltd | Apparatus and method for measuring loads sustained by a bearing pin |
TWI274248B (en) * | 2005-09-09 | 2007-02-21 | Asustek Comp Inc | Portable electronic device |
EP1944575A4 (en) * | 2005-10-11 | 2012-11-28 | Panasonic Corp | INERTIAL STRENGTH SENSOR OF THE VIBRATION TYPE AND ELECTRONIC APPARATUS USING THE SAME |
GB0605188D0 (en) * | 2006-03-16 | 2006-04-26 | Pte Ltd | Lifetime damage monitor |
US8180750B2 (en) | 2007-03-14 | 2012-05-15 | The Boeing Company | Support model integration system and method |
GB0704878D0 (en) | 2007-03-14 | 2007-04-18 | Trw Ltd | Aircraft landing gear monitoring apparatus |
NZ553955A (en) * | 2007-03-19 | 2008-05-30 | Commtest Instr Ltd | Method and system for vibration sensing power management |
FR2922011B1 (fr) * | 2007-10-05 | 2011-05-06 | Thales Sa | Instrument de secours pour aeronef. |
GB0722319D0 (en) | 2007-11-14 | 2007-12-27 | Rolls Royce Plc | Component monitoring arrangement |
FR2931978B1 (fr) * | 2008-06-02 | 2010-07-30 | Peugeot Citroen Automobiles Sa | Procede de surveillance d'un organe d'entrainement d'un vehicule. |
US8165730B2 (en) * | 2008-06-19 | 2012-04-24 | L-3 Communications Corporation | Flight recorder having integral reserve power supply within form factor of enclosure and method therefor |
CA2689744C (en) * | 2009-01-08 | 2015-05-05 | New Flyer Industries Canada Ulc | System and method for monitoring operation of vehicles |
IT1396260B1 (it) * | 2009-01-20 | 2012-11-16 | Aeronautical Service S R L | Sistema innovativo per il monitoraggio della vita di strutture/equipaggiamenti aeronautiche in materiali compositi. |
DE102010029590B4 (de) * | 2010-06-01 | 2014-07-10 | Robert Bosch Gmbh | Drehratensensor, Sensoranordnung, Verfahren zum Betrieb eines Drehratensensors und Verfahren zum Betrieb einer Sensoranordnung |
US8607640B2 (en) | 2010-07-19 | 2013-12-17 | Odd Harald Steen Eriksen | Sensor for measuring large mechanical strains in shear or lateral translation |
US8659307B2 (en) | 2010-08-17 | 2014-02-25 | Rosemount Aerospace Inc. | Capacitive sensors for monitoring load bearing on pins |
US8627727B2 (en) | 2010-07-19 | 2014-01-14 | United Technologies Corporation | Sensor for measuring large mechanical strains with fine adjustment device |
US8286508B2 (en) | 2010-07-19 | 2012-10-16 | Goodrich Corporation | Systems and methods for measuring angular motion |
US8359932B2 (en) | 2010-07-19 | 2013-01-29 | Goodrich Corporation | Systems and methods for mounting landing gear strain sensors |
US8933713B2 (en) | 2010-07-19 | 2015-01-13 | Goodrich Corporation | Capacitive sensors for monitoring loads |
US10131419B2 (en) | 2010-10-15 | 2018-11-20 | Goodrich Corporation | Systems and methods for detecting landing gear ground loads |
EP2694366B1 (en) | 2011-04-07 | 2015-03-04 | LORD Corporation | Aircraft rotary wing motion control and instrumented motion control fluid device |
GB2496426B (en) * | 2011-11-11 | 2013-12-25 | Messier Dowty Ltd | Gauge |
US9567097B2 (en) | 2012-02-03 | 2017-02-14 | Rosemount Aerospace Inc. | System and method for real-time aircraft performance monitoring |
TWI487883B (zh) * | 2012-07-19 | 2015-06-11 | Ind Tech Res Inst | 感測器的讀取裝置與驅動方法 |
EP3718960B1 (en) | 2014-12-10 | 2023-10-25 | Paul D. Okulov | Structural health and usage monitoring system |
FR3045905B1 (fr) | 2015-12-21 | 2017-12-15 | Sagem Defense Securite | Procede de surveillance du vieillissement d'un train d'atterrissage d'un aeronef |
EP3275789B1 (en) | 2016-07-27 | 2021-11-17 | Ratier-Figeac SAS | Actuator assembly |
IT201600099415A1 (it) * | 2016-10-04 | 2018-04-04 | C A I Confident Aircraft Ind S R L | Cellula per velivolo ultraleggero e/o leggero certificato. |
EP3336485B1 (en) | 2016-12-15 | 2020-09-23 | Safran Landing Systems UK Limited | Aircraft assembly including deflection sensor |
US11526199B2 (en) * | 2018-10-05 | 2022-12-13 | Teledyne Instruments, Inc. | Redundant memory for underwater instrumentation |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3712122A (en) | 1971-02-08 | 1973-01-23 | Electro Dev Corp | Aircraft hard landing indicator |
US3946358A (en) * | 1974-06-19 | 1976-03-23 | Sundstrand Data Control, Inc. | Aircraft ground proximity warning instrument |
US4409670A (en) * | 1981-06-26 | 1983-10-11 | United Technologies Corporation | Solid-state digital flight data recorder |
GB2110421B (en) * | 1981-07-17 | 1985-02-27 | Stress Engineering Services Li | Apparatus for dynamic analysis of analog signals |
US4644494A (en) * | 1984-02-06 | 1987-02-17 | Sundstrand Data Control, Inc. | Solid state memory for aircraft flight data recorder systems |
JP2719580B2 (ja) * | 1989-06-27 | 1998-02-25 | 山一電機株式会社 | 衝撃記憶ユニット |
US5421204A (en) * | 1993-06-08 | 1995-06-06 | Svaty, Jr.; Karl J. | Structural monitoring system |
JP3188838B2 (ja) | 1996-03-28 | 2001-07-16 | 株式会社福岡機器製作所 | レインフロー法による疲労解析用データ採取装置 |
US6354152B1 (en) * | 1996-05-08 | 2002-03-12 | Edward Charles Herlik | Method and system to measure dynamic loads or stresses in aircraft, machines, and structures |
US6138078A (en) * | 1996-08-22 | 2000-10-24 | Csi Technology, Inc. | Machine monitor with tethered sensors |
US6766950B2 (en) | 1997-12-16 | 2004-07-27 | Donald R. Hall | Modular architecture sensing and computing platform |
US6402031B1 (en) | 1997-12-16 | 2002-06-11 | Donald R Hall | Modular architecture sensing and computing platform |
US6246320B1 (en) | 1999-02-25 | 2001-06-12 | David A. Monroe | Ground link with on-board security surveillance system for aircraft and other commercial vehicles |
US6266588B1 (en) * | 1999-03-01 | 2001-07-24 | Mcclellan Scott B. | Vehicle motion detection and recording method and apparatus |
US6209390B1 (en) * | 1999-05-14 | 2001-04-03 | Larue Gerald Duane | Turbocharger fatigue life monitor |
US7068187B2 (en) * | 2000-02-03 | 2006-06-27 | Honeywell International Inc. | Method, apparatus and computer program product for unstabilized approach alerting |
US6898492B2 (en) * | 2000-03-15 | 2005-05-24 | De Leon Hilary Laing | Self-contained flight data recorder with wireless data retrieval |
AU7858201A (en) * | 2000-08-04 | 2002-02-18 | Dunlop Aerospace Ltd | Brake condition monitoring |
WO2003050625A2 (en) * | 2001-12-06 | 2003-06-19 | Fisher-Rosemount Systems, Inc. | Intrinsically safe field maintenance tool |
US7298671B2 (en) * | 2002-04-24 | 2007-11-20 | Ascend Geo, Llc | Seismic-data acquisition methods and apparatus |
GB2387912A (en) | 2002-04-26 | 2003-10-29 | Messier Dowty Inc | Monitoring parameters in structural components |
US6854689B1 (en) * | 2004-02-09 | 2005-02-15 | The Boeing Company | Methods and systems for operating aircraft landing gears |
WO2006119323A2 (en) * | 2005-05-03 | 2006-11-09 | Palomar Technology, Llc | Trusted monitoring system and method |
-
2002
- 2002-04-26 GB GB0209584A patent/GB2387912A/en not_active Withdrawn
-
2003
- 2003-04-28 US US10/512,661 patent/US7680630B2/en not_active Expired - Lifetime
- 2003-04-28 WO PCT/GB2003/001820 patent/WO2003091682A1/en active IP Right Grant
- 2003-04-28 CA CA2483404A patent/CA2483404C/en not_active Expired - Lifetime
- 2003-04-28 CA CA2738678A patent/CA2738678C/en not_active Expired - Lifetime
- 2003-04-28 ES ES03722795T patent/ES2278159T3/es not_active Expired - Lifetime
- 2003-04-28 EP EP03722795A patent/EP1499864B1/en not_active Expired - Lifetime
- 2003-04-28 DE DE60310703T patent/DE60310703T2/de not_active Expired - Lifetime
- 2003-04-28 BR BR0309781-1A patent/BR0309781A/pt active Search and Examination
- 2003-04-28 AU AU2003229956A patent/AU2003229956A1/en not_active Abandoned
- 2003-04-28 AT AT03722795T patent/ATE349685T1/de not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
GB0209584D0 (en) | 2002-06-05 |
US7680630B2 (en) | 2010-03-16 |
GB2387912A (en) | 2003-10-29 |
DE60310703D1 (de) | 2007-02-08 |
EP1499864B1 (en) | 2006-12-27 |
EP1499864A1 (en) | 2005-01-26 |
WO2003091682A1 (en) | 2003-11-06 |
CA2483404C (en) | 2011-11-29 |
US20060106582A1 (en) | 2006-05-18 |
CA2738678C (en) | 2015-11-10 |
CA2483404A1 (en) | 2003-11-06 |
DE60310703T2 (de) | 2007-10-04 |
ES2278159T3 (es) | 2007-08-01 |
AU2003229956A1 (en) | 2003-11-10 |
CA2738678A1 (en) | 2003-11-06 |
ATE349685T1 (de) | 2007-01-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B11D | Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time |