UA96129C2 - Способ контроля двигателей самолета - Google Patents
Способ контроля двигателей самолетаInfo
- Publication number
- UA96129C2 UA96129C2 UAA200801060A UAA200801060A UA96129C2 UA 96129 C2 UA96129 C2 UA 96129C2 UA A200801060 A UAA200801060 A UA A200801060A UA A200801060 A UAA200801060 A UA A200801060A UA 96129 C2 UA96129 C2 UA 96129C2
- Authority
- UA
- Ukraine
- Prior art keywords
- engines
- monitoring
- calculator
- engine
- monitoring plane
- Prior art date
Links
- 238000012544 monitoring process Methods 0.000 title abstract 4
- 238000000034 method Methods 0.000 title abstract 3
- 230000002159 abnormal effect Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0218—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults
- G05B23/0224—Process history based detection method, e.g. whereby history implies the availability of large amounts of data
- G05B23/0227—Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions
- G05B23/0237—Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions based on parallel systems, e.g. comparing signals produced at the same time by same type systems and detect faulty ones by noticing differences among their responses
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Testing And Monitoring For Control Systems (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Testing Of Engines (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Burglar Alarm Systems (AREA)
- Safety Devices In Control Systems (AREA)
- Hybrid Electric Vehicles (AREA)
Abstract
Заявлен способ контроля двигателей самолета, который содержит минимум два двигателя (m1, m2, m3, m4), каждый из которых управляется компьютером (1, 2, 3, 4) управления двигателем, при этом компьютеры (1, 2, 3, 4) соединены между собой с помощью сети (5) связи, и каждый компьютер (1, 2, 3, 4) контролирует рабочие параметры (р, V) двигателя (m1, m2, m3, m4), которым он управляет. Способ характеризуется тем, что направляют (60; 100) в сеть (5) значения (V (k)), по крайней мере, одного из упомянутых параметров (p(k)) из двух компьютеров (1, 2, 3, 4), сравнивают (62; 102, 103, 104) эти значения со значениями (V (k ')) этого параметра (p (k) = p (k')), поступающего от другого компьютера (1, 2, 3, 4), и если одно значение (V (k)) отличается от другого (V (k ')) на величину разницы (d1 (k), d2 (k), d3 (k)), которая превышает заранее определенное пороговое значение (S), делают вывод о том, что один из диагностируемых двигателей (m (k)) работает ненормально.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0700642A FR2911972B1 (fr) | 2007-01-30 | 2007-01-30 | Procede de surveillance de moteurs d'avion |
Publications (1)
Publication Number | Publication Date |
---|---|
UA96129C2 true UA96129C2 (ru) | 2011-10-10 |
Family
ID=38519671
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA200801060A UA96129C2 (ru) | 2007-01-30 | 2008-01-29 | Способ контроля двигателей самолета |
Country Status (14)
Country | Link |
---|---|
US (1) | US7840320B2 (ru) |
EP (1) | EP1953614B1 (ru) |
JP (1) | JP5473226B2 (ru) |
CN (1) | CN101236129B (ru) |
BR (1) | BRPI0800201B1 (ru) |
CA (1) | CA2619143C (ru) |
FR (1) | FR2911972B1 (ru) |
IL (1) | IL189215A (ru) |
MA (1) | MA29724B1 (ru) |
MX (1) | MX2008001440A (ru) |
RU (1) | RU2388661C2 (ru) |
SG (1) | SG144885A1 (ru) |
UA (1) | UA96129C2 (ru) |
ZA (1) | ZA200800923B (ru) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2939170B1 (fr) | 2008-11-28 | 2010-12-31 | Snecma | Detection d'anomalie dans un moteur d'aeronef. |
FR2971595B1 (fr) * | 2011-02-15 | 2013-03-22 | Snecma | Surveillance d'un moteur d'aeronef pour anticiper les operations de maintenance |
FR2981474B1 (fr) * | 2011-10-17 | 2013-12-27 | Alstom Technology Ltd | Procede de detection preventive d'une panne d'un appareil, programme d'ordinateur, installation et module de detection preventive d'une panne d'un appareil |
US20140100806A1 (en) * | 2012-10-04 | 2014-04-10 | Globalfoundries Inc. | Method and apparatus for matching tools based on time trace data |
US9391495B2 (en) * | 2013-03-05 | 2016-07-12 | Joy Mm Delaware, Inc. | Predicting motor failure based on relationship of motor pair characteristics |
GB2513132B (en) * | 2013-04-16 | 2015-05-27 | Ge Aviat Systems Ltd | Method for predicting a bleed air system fault |
CN104343490B (zh) * | 2013-07-24 | 2017-10-03 | 中国国际航空股份有限公司 | 一种发动机滑油监控系统及方法 |
US9209721B2 (en) * | 2014-04-29 | 2015-12-08 | The Boeing Company | Systems and methods for the control and operation of a parallel motor controller architecture |
CN105270353B (zh) * | 2014-06-26 | 2019-02-22 | 山东朗进科技股份有限公司 | 一种轨道车辆空调机组检修方法 |
US10035609B2 (en) | 2016-03-08 | 2018-07-31 | Harris Corporation | Wireless engine monitoring system for environmental emission control and aircraft networking |
US10223846B2 (en) * | 2016-10-10 | 2019-03-05 | General Electric Company | Aerial vehicle engine health prediction |
FR3064602B1 (fr) * | 2017-03-29 | 2019-06-07 | Airbus Operations | Mode de fonctionnement degrade d'un groupe propulseur d'aeronef permettant le deplafonnement d'une consigne de poussee |
FR3065995B1 (fr) * | 2017-05-05 | 2019-07-05 | Safran Aircraft Engines | Systeme et procede de surveillance d'une turbomachine a detection d'anomalie corrigee par un facteur d'usure |
FR3074590B1 (fr) * | 2017-12-04 | 2023-03-17 | Soc Air France | Methode de prediction d'une anomalie de fonctionnement d'un ou plusieurs equipements d'un ensemble |
CN109143839A (zh) * | 2018-09-04 | 2019-01-04 | 广西质量技术工程学校 | 一种高容错的传感器冗余控制方法 |
CN109799803B (zh) * | 2018-12-11 | 2020-06-16 | 大连理工大学 | 一种基于lft的航空发动机传感器及执行机构故障诊断方法 |
FR3095271B1 (fr) * | 2019-04-18 | 2021-07-30 | Safran | Système de surveillance de la santé d’un hélicoptère |
CN110481804B (zh) * | 2019-08-22 | 2021-05-25 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | 一种飞行辅助系统和飞机 |
US11561873B2 (en) | 2019-09-26 | 2023-01-24 | General Electric Company | Test equipment interface add-on having a production support equipment module and a selectively removable test support equipment module |
JP7176543B2 (ja) * | 2020-02-18 | 2022-11-22 | 株式会社デンソー | 異常診断システム、異常診断方法およびコンピュータプログラム |
US11748183B2 (en) * | 2020-10-11 | 2023-09-05 | Textron Innovations Inc. | Reasonableness monitor |
CN112373719B (zh) * | 2020-10-30 | 2023-03-14 | 哈尔滨飞机工业集团有限责任公司 | 一种直升机发动机维护信息采集显示方法 |
CN112607042A (zh) * | 2020-12-28 | 2021-04-06 | 中国人民解放军陆军炮兵防空兵学院 | 一种无人机装载通信频谱侦测装置 |
CN113341927B (zh) * | 2021-06-11 | 2022-12-02 | 江西洪都航空工业集团有限责任公司 | 飞控系统伺服作动器bit故障检测方法及装置 |
CN114783162B (zh) * | 2022-06-20 | 2022-10-28 | 商飞软件有限公司 | 一种飞机三余度系统告警表决方法 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4106730A (en) * | 1976-10-01 | 1978-08-15 | The Boeing Company | Engine out control system for STOL aircraft |
FR2488696A1 (fr) * | 1980-08-13 | 1982-02-19 | Snecma | Procede et dispositif de detection du decollement tournant apparaissant dans une turbomachine a deux corps tournants |
US4651563A (en) * | 1985-10-16 | 1987-03-24 | Sperry Corporation | Jet engine testing apparatus |
US4785403A (en) * | 1986-05-02 | 1988-11-15 | United Technologies Corporation | Distributed flight condition data validation system and method |
JPH0588701A (ja) * | 1991-09-30 | 1993-04-09 | Mitsubishi Heavy Ind Ltd | 3重冗長系用同期装置 |
US5349654A (en) * | 1992-02-20 | 1994-09-20 | The Boeing Company | Fault tolerant data exchange unit |
JPH06250868A (ja) * | 1993-02-25 | 1994-09-09 | Mitsubishi Electric Corp | 計算機 |
CA2440887A1 (en) * | 2001-03-12 | 2002-09-19 | Honeywell International Inc. | Method of recovering a flight critical computer after a radiation event |
EP1444658B1 (en) * | 2001-11-13 | 2010-02-10 | Goodrich Pump & Engine Control Systems, Inc. | Fault management system for gas turbine engines |
FR2846377B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromecanique pour turboreacteur a controle permanent de position |
FR2846375B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromacanique pour turboreacteur a asservissement du deplacement des portes |
US6983199B2 (en) * | 2003-04-30 | 2006-01-03 | General Electric Company | Vibration measurement and recording system and method |
JP2004352071A (ja) * | 2003-05-29 | 2004-12-16 | Ishikawajima Harima Heavy Ind Co Ltd | 航空機用エンジンの機上トラブル対処装置 |
-
2007
- 2007-01-30 FR FR0700642A patent/FR2911972B1/fr active Active
-
2008
- 2008-01-23 EP EP08100793.2A patent/EP1953614B1/fr active Active
- 2008-01-25 MA MA30598A patent/MA29724B1/fr unknown
- 2008-01-28 IL IL189215A patent/IL189215A/en active IP Right Grant
- 2008-01-29 US US12/021,643 patent/US7840320B2/en active Active
- 2008-01-29 BR BRPI0800201A patent/BRPI0800201B1/pt active IP Right Grant
- 2008-01-29 UA UAA200801060A patent/UA96129C2/ru unknown
- 2008-01-29 SG SG200800794-0A patent/SG144885A1/en unknown
- 2008-01-29 JP JP2008017157A patent/JP5473226B2/ja active Active
- 2008-01-29 RU RU2008103374/11A patent/RU2388661C2/ru active
- 2008-01-29 CA CA2619143A patent/CA2619143C/fr active Active
- 2008-01-29 ZA ZA200800923A patent/ZA200800923B/en unknown
- 2008-01-30 CN CN200810000256.7A patent/CN101236129B/zh active Active
- 2008-01-30 MX MX2008001440A patent/MX2008001440A/es active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
MX2008001440A (es) | 2009-02-24 |
JP5473226B2 (ja) | 2014-04-16 |
MA29724B1 (fr) | 2008-09-01 |
CA2619143A1 (fr) | 2008-07-30 |
JP2008215345A (ja) | 2008-09-18 |
ZA200800923B (en) | 2008-11-26 |
EP1953614B1 (fr) | 2019-01-23 |
BRPI0800201B1 (pt) | 2018-10-09 |
EP1953614A3 (fr) | 2009-07-08 |
BRPI0800201A (pt) | 2008-09-16 |
CN101236129A (zh) | 2008-08-06 |
CN101236129B (zh) | 2013-03-20 |
CA2619143C (fr) | 2014-12-09 |
RU2388661C2 (ru) | 2010-05-10 |
IL189215A0 (en) | 2008-11-03 |
RU2008103374A (ru) | 2009-08-10 |
US20080262663A1 (en) | 2008-10-23 |
FR2911972B1 (fr) | 2009-03-27 |
IL189215A (en) | 2013-10-31 |
SG144885A1 (en) | 2008-08-28 |
EP1953614A2 (fr) | 2008-08-06 |
US7840320B2 (en) | 2010-11-23 |
FR2911972A1 (fr) | 2008-08-01 |
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