BR0206879A - Interruptor para circuito com falha no aterramento aplicável em aeronave - Google Patents
Interruptor para circuito com falha no aterramento aplicável em aeronaveInfo
- Publication number
- BR0206879A BR0206879A BR0206879-6A BR0206879A BR0206879A BR 0206879 A BR0206879 A BR 0206879A BR 0206879 A BR0206879 A BR 0206879A BR 0206879 A BR0206879 A BR 0206879A
- Authority
- BR
- Brazil
- Prior art keywords
- power
- circuit breaker
- circuit
- sensor
- logic controller
- Prior art date
Links
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
- H02H3/00—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection
- H02H3/26—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection responsive to difference between voltages or between currents; responsive to phase angle between voltages or between currents
- H02H3/32—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection responsive to difference between voltages or between currents; responsive to phase angle between voltages or between currents involving comparison of the voltage or current values at corresponding points in different conductors of a single system, e.g. of currents in go and return conductors
- H02H3/34—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection responsive to difference between voltages or between currents; responsive to phase angle between voltages or between currents involving comparison of the voltage or current values at corresponding points in different conductors of a single system, e.g. of currents in go and return conductors of a three-phase system
- H02H3/347—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection responsive to difference between voltages or between currents; responsive to phase angle between voltages or between currents involving comparison of the voltage or current values at corresponding points in different conductors of a single system, e.g. of currents in go and return conductors of a three-phase system using summation current transformers
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
- H02H1/00—Details of emergency protective circuit arrangements
- H02H1/0007—Details of emergency protective circuit arrangements concerning the detecting means
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
- H02H1/00—Details of emergency protective circuit arrangements
- H02H1/06—Arrangements for supplying operative power
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
- H02H3/00—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection
- H02H3/02—Details
- H02H3/04—Details with warning or supervision in addition to disconnection, e.g. for indicating that protective apparatus has functioned
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
- H02H3/00—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection
- H02H3/08—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection responsive to excess current
- H02H3/10—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection responsive to excess current additionally responsive to some other abnormal electrical conditions
- H02H3/105—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal electric working condition with or without subsequent reconnection ; integrated protection responsive to excess current additionally responsive to some other abnormal electrical conditions responsive to excess current and fault current to earth
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Emergency Protection Circuit Devices (AREA)
- Testing Of Short-Circuits, Discontinuities, Leakage, Or Incorrect Line Connections (AREA)
- Breakers (AREA)
- Protection Of Generators And Motors (AREA)
Abstract
"INTERRUPTOR PARA CIRCUITO COM FALHA NO ATERRAMENTO APLICáVEL EM AERONAVE". A invenção refere-se a um interruptor de circuito com falha no aterramento em aeronave que interrompe um circuito quando um desequilíbrio de corrente é detectado. O interruptor de circuito inclui um fornecedor de energia, um sensor para detectar um desequilíbrio de corrente no lado de linha do circuito, um controlador lógico, e um controlador de energia. O fornecedor de energia provê energia ao sensor, ao controlador lógico, e ao controlador de energia. O controlador lógico recebe entrada do sensor, e o controle de energia recebe entrada do controlador lógico, e interrompe energia para o lado de carga do circuito quando o sensor detecta um desequilíbrio de corrente. Uma interrupção de energia, devido a um desequilíbrio de corrente detectado, é mantido até que a fonte de energia tenha percorrido um ciclo. O interruptor de circuito é preferivelmente autónomo, não requerendo sinais, entrada, ou fontes de energia adicionais.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/775,337 US6583975B2 (en) | 2001-02-01 | 2001-02-01 | Aircraft applicable ground fault circuit interrupter |
PCT/US2002/002893 WO2002061905A2 (en) | 2001-02-01 | 2002-01-30 | Aircraft applicable ground fault circuit interrupter |
Publications (1)
Publication Number | Publication Date |
---|---|
BR0206879A true BR0206879A (pt) | 2004-01-20 |
Family
ID=25104087
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR0206879-6A BR0206879A (pt) | 2001-02-01 | 2002-01-30 | Interruptor para circuito com falha no aterramento aplicável em aeronave |
Country Status (7)
Country | Link |
---|---|
US (9) | US6583975B2 (pt) |
EP (1) | EP1364437A2 (pt) |
JP (1) | JP2004519185A (pt) |
CN (1) | CN1323475C (pt) |
BR (1) | BR0206879A (pt) |
CA (1) | CA2437377C (pt) |
WO (1) | WO2002061905A2 (pt) |
Families Citing this family (54)
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US6583975B2 (en) * | 2001-02-01 | 2003-06-24 | Hydro-Aire, Inc. | Aircraft applicable ground fault circuit interrupter |
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JP4805396B2 (ja) * | 2010-03-31 | 2011-11-02 | ファナック株式会社 | モータ駆動装置 |
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TW201303318A (zh) * | 2011-04-28 | 2013-01-16 | Aerovironment Inc | 脈衝式失落接地偵測器電路 |
KR101298779B1 (ko) * | 2011-06-10 | 2013-08-22 | 한국항공우주산업 주식회사 | 항공기 다중형상 지원용 통합 실험 시스템 및 그 시스템을 제어하는 방법 |
CN102508437B (zh) * | 2011-09-14 | 2014-04-16 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机供电控制管理***仿真用多功能机电***仿真方法 |
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CN102903582A (zh) * | 2012-08-21 | 2013-01-30 | 江苏云意电气股份有限公司 | 一种智能型剩余电流断路器控制器装置 |
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BE1022018B1 (fr) * | 2013-08-14 | 2016-02-04 | Cockerill Maintenance & Ingenierie S.A. | Dispositif de commutation et protection a distance de systemes electriques. |
CN104300526A (zh) * | 2014-09-17 | 2015-01-21 | 安徽天健环保车辆部件有限公司 | 一种特种车电源接入保护器 |
CN105811377B (zh) * | 2014-12-31 | 2018-12-07 | 上海良信电器股份有限公司 | 断路器更换控制器用内置式保护模块控制电路 |
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CN104820751B (zh) * | 2015-05-11 | 2017-11-14 | 中国民航大学 | 基于广义状态空间平均的飞机电力***小扰动稳定性分析方法 |
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CN105571710A (zh) * | 2015-12-11 | 2016-05-11 | 中国航空工业集团公司西安航空计算技术研究所 | 一种发动机机载振动信号采集电路 |
US10177757B2 (en) | 2016-12-07 | 2019-01-08 | Hamilton Sundstrand Corporation-Pcss | Single event latchup mitigation with sample and hold |
CN110603451B (zh) * | 2017-05-11 | 2022-02-22 | 三菱电机株式会社 | 电子控制装置 |
EP3499669A1 (en) * | 2017-12-13 | 2019-06-19 | Ovh | Circuit and system implementing a smart fuse for a power supply |
US10700603B2 (en) | 2017-12-13 | 2020-06-30 | Ovh | Circuit and system implementing a power supply configured for spark prevention |
US11133665B2 (en) * | 2018-08-29 | 2021-09-28 | Hamilton Sundstrand Corporation | Direct current over voltage monitoring and protection |
US11562872B2 (en) * | 2020-09-16 | 2023-01-24 | Abb Schweiz Ag | Circuit interrupter for detecting breaker fault conditions and interrupting an electric current |
CN114326367B (zh) * | 2021-12-06 | 2024-04-02 | 中国商用飞机有限责任公司 | 一种用于飞行器的电路保护装置管理*** |
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-
2001
- 2001-02-01 US US09/775,337 patent/US6583975B2/en not_active Expired - Lifetime
- 2001-09-14 US US09/954,474 patent/US6618229B2/en not_active Expired - Lifetime
-
2002
- 2002-01-30 CA CA2437377A patent/CA2437377C/en not_active Expired - Fee Related
- 2002-01-30 CN CNB028044576A patent/CN1323475C/zh not_active Expired - Fee Related
- 2002-01-30 JP JP2002561338A patent/JP2004519185A/ja active Pending
- 2002-01-30 BR BR0206879-6A patent/BR0206879A/pt not_active Application Discontinuation
- 2002-01-30 WO PCT/US2002/002893 patent/WO2002061905A2/en not_active Application Discontinuation
- 2002-01-30 EP EP02706101A patent/EP1364437A2/en not_active Withdrawn
-
2003
- 2003-07-01 US US10/611,218 patent/US6788505B2/en not_active Expired - Lifetime
-
2004
- 2004-10-18 US US10/967,482 patent/US7064941B2/en not_active Expired - Lifetime
-
2006
- 2006-04-28 US US11/413,737 patent/US7312965B2/en not_active Expired - Lifetime
-
2007
- 2007-10-31 US US11/931,803 patent/US7630182B2/en not_active Expired - Fee Related
-
2008
- 2008-03-20 US US12/052,451 patent/US7672099B2/en not_active Expired - Fee Related
- 2008-03-21 US US12/052,975 patent/US7667935B2/en not_active Expired - Fee Related
- 2008-03-21 US US12/053,071 patent/US7688558B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US7688558B2 (en) | 2010-03-30 |
US7672099B2 (en) | 2010-03-02 |
US20080316658A1 (en) | 2008-12-25 |
US7630182B2 (en) | 2009-12-08 |
US20080062592A1 (en) | 2008-03-13 |
US20040090724A1 (en) | 2004-05-13 |
US7064941B2 (en) | 2006-06-20 |
WO2002061905A2 (en) | 2002-08-08 |
CN1323475C (zh) | 2007-06-27 |
US20060250730A1 (en) | 2006-11-09 |
US20050146818A1 (en) | 2005-07-07 |
JP2004519185A (ja) | 2004-06-24 |
US20090086396A1 (en) | 2009-04-02 |
US20080304190A1 (en) | 2008-12-11 |
US7312965B2 (en) | 2007-12-25 |
CN1498448A (zh) | 2004-05-19 |
CA2437377C (en) | 2012-03-27 |
US6788505B2 (en) | 2004-09-07 |
EP1364437A2 (en) | 2003-11-26 |
US20020101698A1 (en) | 2002-08-01 |
CA2437377A1 (en) | 2002-08-08 |
US6618229B2 (en) | 2003-09-09 |
US6583975B2 (en) | 2003-06-24 |
WO2002061905A9 (en) | 2004-04-01 |
WO2002061905A3 (en) | 2003-03-13 |
US7667935B2 (en) | 2010-02-23 |
US20020105764A1 (en) | 2002-08-08 |
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