BR0211655A - Sistema residente de teste para comutadores de indicação integrantes da instrumentação de uma aeronave - Google Patents

Sistema residente de teste para comutadores de indicação integrantes da instrumentação de uma aeronave

Info

Publication number
BR0211655A
BR0211655A BR0211655-3A BR0211655A BR0211655A BR 0211655 A BR0211655 A BR 0211655A BR 0211655 A BR0211655 A BR 0211655A BR 0211655 A BR0211655 A BR 0211655A
Authority
BR
Brazil
Prior art keywords
test system
indication switches
aircraft
aircraft instrumentation
indication
Prior art date
Application number
BR0211655-3A
Other languages
English (en)
Inventor
Thomas Mulera
David Robinson
Original Assignee
Honeywell Int 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 Honeywell Int Inc filed Critical Honeywell Int Inc
Publication of BR0211655A publication Critical patent/BR0211655A/pt

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/005—Testing of electric installations on transport means
    • G01R31/008—Testing of electric installations on transport means on air- or spacecraft, railway rolling stock or sea-going vessels
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/327—Testing of circuit interrupters, switches or circuit-breakers
    • G01R31/3277—Testing of circuit interrupters, switches or circuit-breakers of low voltage devices, e.g. domestic or industrial devices, such as motor protections, relays, rotation switches
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H47/00—Circuit arrangements not adapted to a particular application of the relay and designed to obtain desired operating characteristics or to provide energising current
    • H01H47/002—Monitoring or fail-safe circuits
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H9/00—Details of switching devices, not covered by groups H01H1/00 - H01H7/00
    • H01H9/16—Indicators for switching condition, e.g. "on" or "off"
    • H01H9/167—Circuits for remote indication

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Electric Properties And Detecting Electric Faults (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)
  • Switch Cases, Indication, And Locking (AREA)

Abstract

"SISTEMA RESIDENTE DE TESTE PARA COMUTADORES DE INDICAçãO INTEGRANTES DA INSTRUMENTAçãO DE UMA AERONAVE". Trata-se de um sistema residente (10) de teste para comutadores de indicação integrantes da instrumentação de uma aeronave compreendendo uma pluralidade de comutadores (11, 12, 13) de indicação de aeronave e uma primeira rede de adição de resistores possuindo resistores de entrada (20, 21, 22) individualmente ligados a primeiros contatos de diferentes comutadores de indicação. O sistema de teste inclui adicionalmente uma segunda rede de adição de resistores possuindo resistores de entrada (30, 31, 32) individualmente ligados a segundos contatos de diferentes comutadores de indicação. São providos circuitos de saída para acoplamento de saídas das primeira e segunda redes de adição de resistores a uma unidade de controle eletrónico da aeronave.
BR0211655-3A 2001-08-02 2002-07-23 Sistema residente de teste para comutadores de indicação integrantes da instrumentação de uma aeronave BR0211655A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/922,204 US6593758B2 (en) 2001-08-02 2001-08-02 Built-in test system for aircraft indication switches
PCT/US2002/023430 WO2003016932A1 (en) 2001-08-02 2002-07-23 Built-in test system for aircraft indication switches

Publications (1)

Publication Number Publication Date
BR0211655A true BR0211655A (pt) 2005-01-04

Family

ID=25446689

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0211655-3A BR0211655A (pt) 2001-08-02 2002-07-23 Sistema residente de teste para comutadores de indicação integrantes da instrumentação de uma aeronave

Country Status (7)

Country Link
US (1) US6593758B2 (pt)
EP (1) EP1415169B1 (pt)
AT (1) ATE461459T1 (pt)
BR (1) BR0211655A (pt)
CA (1) CA2454808C (pt)
DE (1) DE60235704D1 (pt)
WO (1) WO2003016932A1 (pt)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10234854A1 (de) * 2002-07-31 2004-02-12 Robert Bosch Gmbh Schalter zum Abschalten wenigstens eines Airbags
US8311697B2 (en) * 2004-07-27 2012-11-13 Honeywell International Inc. Impact assessment system and method for determining emergent criticality
US20070180329A1 (en) * 2006-01-31 2007-08-02 Lanus Mark S Method of latent fault checking a management network
FR2899373B1 (fr) * 2006-04-04 2013-03-15 Airbus France Dispositif de detection d'etat d'un interrupteur
FR2946023B1 (fr) * 2009-06-02 2014-11-28 Airbus France Procede et dispositif de traitement de pannes
FR2946395B1 (fr) * 2009-06-04 2016-03-04 Airbus France Procede pour la detection de l'ouverture d'un inverseur de poussee de turboreacteur d'aeronef
CN102055339B (zh) * 2009-10-30 2014-03-26 深圳富泰宏精密工业有限公司 测试用电源装置
FR2956519B1 (fr) * 2010-02-18 2012-02-03 Snecma Circuit de detection des positions de contacteurs dans une turbomachine
DE102010026919A1 (de) * 2010-07-13 2012-01-19 Leopold Kostal Gmbh & Co. Kg Verfahren zur Erfassung einer Schaltstellung einer Schalteinrichtung
GB2486493B (en) * 2010-12-17 2016-06-15 Ge Aviat Systems Ltd Switching circuits and methods of testing
US8836338B2 (en) 2011-12-16 2014-09-16 Ge Aviation Systems Limited Switching circuits and methods of testing thereof
CN103543379A (zh) * 2013-10-11 2014-01-29 联合汽车电子有限公司 汽车发动机管理系统电路故障模拟装置
JP6248672B2 (ja) * 2014-02-10 2017-12-20 株式会社デンソー リレー制御装置
CN108680820B (zh) * 2018-04-10 2020-08-14 上海空间电源研究所 多航天器串联状态检测电路及实现方法
US11675011B2 (en) * 2019-08-15 2023-06-13 Analog Devices International Unlimited Company Switch condition monitoring

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3550090A (en) 1968-01-16 1970-12-22 Hb Eng Corp Method and system for determining whether a switch is open or closed
US3821733A (en) 1971-06-15 1974-06-28 Gulf & Western Mfg Co Alarm circuitry
US4027286A (en) 1976-04-23 1977-05-31 Trw Inc. Multiplexed data monitoring system
US4491828A (en) * 1978-10-16 1985-01-01 American District Telegraph Company Two-wire multi-zone alarm system
US4359721A (en) 1978-10-16 1982-11-16 American District Telegraph Company Two-wire multi-zone alarm system
US4423410A (en) * 1978-10-16 1983-12-27 American District Telegraph Company Two-wire multi-zone alarm system
FR2488335B1 (fr) 1980-08-11 1986-01-31 Snecma Dispositif detecteur de position d'un inverseur de poussee de turboreacteur et de son verrouillage
GB2090682B (en) 1981-01-06 1985-09-04 Racal Mesl Security Ltd Electrical circuits for security system
GB2117150B (en) * 1982-02-26 1986-03-19 Morrison John M Intruder alarm system
DE3908993A1 (de) * 1989-03-18 1990-09-20 Daimler Benz Ag Einrichtung zur ueberwachung der ordnungsgemaessen funktion eines den schliesszustand eines gurtschlosses in einem kraftfahrzeug abfragenden schaltbauelements
US5161158A (en) 1989-10-16 1992-11-03 The Boeing Company Failure analysis system
GB9015373D0 (en) 1990-07-12 1990-08-29 Rolls Royce Plc Gas turbine engine thrust reverser control
FR2709017B1 (fr) * 1993-08-12 1995-09-22 Snecma Circuit de détection de la position de plusieurs contacteurs bipolaires et application à un inverseur de poussée d'un turboréacteur.
US5720449A (en) 1993-11-19 1998-02-24 Societe De Construction Des Avions Hurel-Dubois Thrust reverser with doors for aircraft engine, equipped with safety systems preventing the untimely opening of the doors
FR2792416B1 (fr) * 1999-04-16 2001-06-08 Texton Procede de controle de la fin de course d'un organe mobile et dispositif pour sa mise en oeuvre

Also Published As

Publication number Publication date
EP1415169B1 (en) 2010-03-17
US6593758B2 (en) 2003-07-15
CA2454808A1 (en) 2003-02-27
CA2454808C (en) 2008-09-23
WO2003016932A1 (en) 2003-02-27
DE60235704D1 (de) 2010-04-29
EP1415169A1 (en) 2004-05-06
US20030025515A1 (en) 2003-02-06
ATE461459T1 (de) 2010-04-15

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE 4A., 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: REFERENTE AO DESPACHO 8.6 DA RPI 2029 DE 24/11/2009.