JP4171610B2 - エンジン始動装置をモニタするシステム及び方法 - Google Patents

エンジン始動装置をモニタするシステム及び方法 Download PDF

Info

Publication number
JP4171610B2
JP4171610B2 JP2002140856A JP2002140856A JP4171610B2 JP 4171610 B2 JP4171610 B2 JP 4171610B2 JP 2002140856 A JP2002140856 A JP 2002140856A JP 2002140856 A JP2002140856 A JP 2002140856A JP 4171610 B2 JP4171610 B2 JP 4171610B2
Authority
JP
Japan
Prior art keywords
data
engine
performance
gas turbine
met
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
JP2002140856A
Other languages
English (en)
Japanese (ja)
Other versions
JP2003090232A5 (https=
JP2003090232A (ja
Inventor
ケビン・リチャード・リーミー
マーク・ジェラルド・バッツ
ロバート・ウィリアム・ラムバート
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JP2003090232A publication Critical patent/JP2003090232A/ja
Publication of JP2003090232A5 publication Critical patent/JP2003090232A5/ja
Application granted granted Critical
Publication of JP4171610B2 publication Critical patent/JP4171610B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N11/00—Starting of engines by means of electric motors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Testing Of Engines (AREA)
JP2002140856A 2001-05-18 2002-05-16 エンジン始動装置をモニタするシステム及び方法 Expired - Fee Related JP4171610B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/861,336 US6470258B1 (en) 2001-05-18 2001-05-18 System and method for monitoring engine starting systems
US09/861336 2001-05-18

Publications (3)

Publication Number Publication Date
JP2003090232A JP2003090232A (ja) 2003-03-28
JP2003090232A5 JP2003090232A5 (https=) 2005-08-25
JP4171610B2 true JP4171610B2 (ja) 2008-10-22

Family

ID=25335523

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002140856A Expired - Fee Related JP4171610B2 (ja) 2001-05-18 2002-05-16 エンジン始動装置をモニタするシステム及び方法

Country Status (4)

Country Link
US (1) US6470258B1 (https=)
EP (1) EP1260690B1 (https=)
JP (1) JP4171610B2 (https=)
DE (1) DE60234287D1 (https=)

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6498978B2 (en) * 2001-05-18 2002-12-24 General Electric Company System and method for monitoring thermal state to normalize engine trending data
US6942451B1 (en) 2003-06-03 2005-09-13 Hamilton Sundstrand Corporation Damping system for an expendable gas turbine engine
US7194866B1 (en) 2003-06-20 2007-03-27 Hamilton Sundstrand Corporation Static structure for an expendable gas turbine engine
US6943699B2 (en) 2003-07-23 2005-09-13 Harris Corporation Wireless engine monitoring system
US8438858B1 (en) 2003-08-20 2013-05-14 Hamilton Sundstrand Corporation Rotational system for an expendable gas turbine engine
US7072797B2 (en) 2003-08-29 2006-07-04 Honeywell International, Inc. Trending system and method using monotonic regression
US7231180B2 (en) * 2004-03-24 2007-06-12 Honeywell International, Inc. Aircraft engine sensor network using wireless sensor communication modules
US7216489B2 (en) * 2004-05-26 2007-05-15 Honeywell International, Inc. System and method for lightoff detection in turbine engines
US7140240B2 (en) * 2004-06-21 2006-11-28 Hamilton Sundstrand Electric engine start system with inspection mode
US7254491B2 (en) * 2004-06-28 2007-08-07 Honeywell International, Inc. Clustering system and method for blade erosion detection
US7506517B2 (en) * 2004-11-23 2009-03-24 Honeywell International, Inc. System and method for turbine engine startup profile characterization
US20060129301A1 (en) * 2004-12-14 2006-06-15 General Electric Company Method and apparatus for assessing gas turbine acceleration capability
US7693643B2 (en) * 2005-02-14 2010-04-06 Honeywell International Inc. Fault detection system and method for turbine engine fuel systems
US7191084B2 (en) * 2005-04-20 2007-03-13 General Electric Company Method and apparatus for gas turbine engine ignition systems
US7577549B2 (en) * 2005-07-18 2009-08-18 General Electric Company System and method for trending exhaust gas temperature in a turbine engine
US7369932B2 (en) * 2006-05-04 2008-05-06 Honeywell International, Inc. System and method for turbine engine fault detection using discrete event system modeling
CN104189968B (zh) 2008-06-26 2017-04-12 甘布罗伦迪亚股份公司 用于处理时间相关的测量信号的方法及装置
US9121769B2 (en) * 2008-08-20 2015-09-01 United Technologies Corporation Sensor and antenna arrangement
US8467949B2 (en) * 2009-05-29 2013-06-18 Honeywell International Inc. Methods and systems for turbine line replaceable unit fault detection and isolation during engine startup
US8370045B2 (en) * 2009-08-14 2013-02-05 Lockheed Martin Corporation Starter control valve failure prediction machine to predict and trend starter control valve failures in gas turbine engines using a starter control valve health prognostic, program product and related methods
US9053468B2 (en) * 2011-04-07 2015-06-09 General Electric Company Methods and systems for monitoring operation of equipment
US20130212210A1 (en) * 2012-02-10 2013-08-15 General Electric Company Rule engine manager in memory data transfers
FR2998003B1 (fr) * 2012-11-12 2014-11-07 Snecma Procede de surveillance d'une sequence d'allumage d'un moteur de turbomachine
US10309317B2 (en) * 2013-06-21 2019-06-04 Hamilton Sundstrand Corporation Air turbine starter pressure monitor system
GB201313140D0 (en) * 2013-07-23 2013-09-04 Rolls Royce Engine Control Systems Ltd System for performing staging control of a multi-stage combustor
CN104343476B (zh) * 2013-07-24 2016-06-08 中国国际航空股份有限公司 飞机辅助动力单元涡轮效率监控方法和装置
BR112016007478A2 (pt) * 2013-10-07 2017-08-01 Ge Aviat Systems Ltd método para diagnosticar uma falha de unidade auxiliar de potência em uma aeronave
FR3018546B1 (fr) * 2014-03-13 2022-01-21 Snecma Procede de surveillance de l'etat d'un moteur par surveillance des gaz d'echappement
US10553120B2 (en) * 2014-09-15 2020-02-04 L3 Technologies, Inc. Fail safe aircraft monitoring and tracking
US9952612B2 (en) 2015-03-03 2018-04-24 Caterpillar Inc. Power system having zone-based load sharing
WO2017055975A1 (en) 2015-09-30 2017-04-06 Bombardier Inc. Method of and system for presenting an operating status of an aircraft engine
US10454525B2 (en) 2016-06-20 2019-10-22 Ge Aviation Systems Llc Communication of signals over fuel lines in a vehicle
US10587307B2 (en) 2016-06-20 2020-03-10 Ge Aviation Systems, Llc Transmission of power and communication of signals over fuel and hydraulic lines in a vehicle
US10598095B2 (en) 2016-10-11 2020-03-24 Unison Industries, Llc Integrated starter for aerial vehicle
US10266278B2 (en) 2016-10-11 2019-04-23 Unison Industries, Llc Starter issue detection
US20180209295A1 (en) * 2016-10-11 2018-07-26 General Electric Company Starter controller
US11225915B2 (en) 2017-11-16 2022-01-18 General Electric Company Engine core speed reducing method and system
CN113291488B (zh) * 2021-04-30 2022-01-04 浙江长龙航空有限公司 一种整体驱动发电机性能监控方法及装置
US12061937B2 (en) * 2022-06-22 2024-08-13 Allegro Microsystems, Llc Methods and apparatus for sensor data consistency
CN115577575B (zh) * 2022-12-08 2023-03-14 太仓点石航空动力有限公司 基于压比指标的压气机性能衰退识别方法及系统
KR102713501B1 (ko) * 2024-02-23 2024-10-02 국방과학연구소 군용 무인항공기의 탑재장비 상태 분석방법 및 장치

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4215412A (en) * 1978-07-13 1980-07-29 The Boeing Company Real time performance monitoring of gas turbine engines
GB8729962D0 (en) * 1987-12-23 1988-02-03 Smiths Industries Plc Engine monitoring
US5107674A (en) * 1990-03-30 1992-04-28 General Electric Company Control for a gas turbine engine
US5583420A (en) * 1993-10-01 1996-12-10 Lucas Aerospace Power Equipment Corporation Microprocessor controller for starter/generator
GB2291199A (en) * 1994-07-09 1996-01-17 Rolls Royce Plc Steady state sensor
US5748500A (en) * 1995-11-14 1998-05-05 Electric Power Research Institute, Inc. System to assess the starting performance of a turbine
US5845483A (en) * 1996-04-10 1998-12-08 General Electric Company Windmill engine starting system with fluid driven motor and pump
US6466858B1 (en) * 2000-11-02 2002-10-15 General Electric Company Methods and apparatus for monitoring gas turbine engine operation
US6498978B2 (en) * 2001-05-18 2002-12-24 General Electric Company System and method for monitoring thermal state to normalize engine trending data

Also Published As

Publication number Publication date
EP1260690A2 (en) 2002-11-27
EP1260690B1 (en) 2009-11-11
US6470258B1 (en) 2002-10-22
EP1260690A3 (en) 2004-12-08
DE60234287D1 (de) 2009-12-24
JP2003090232A (ja) 2003-03-28

Similar Documents

Publication Publication Date Title
JP4171610B2 (ja) エンジン始動装置をモニタするシステム及び方法
JP4171609B2 (ja) エンジン性能をモニタする方法、そのシステム及びプログラム記録媒体
US7197430B2 (en) Method and apparatus for determining engine part life usage
US11333077B2 (en) Systems and methods for transferring mechanical power in a turbine engine
Eustace et al. Fault signatures obtained from fault implant tests on an F404 engine
US7584618B2 (en) Controlling air flow to a turbine shroud for thermal control
JP4780870B2 (ja) 可変飛行データ収集方法及びシステム
US11498695B2 (en) System and method for transmission of engine fault data
US20170175646A1 (en) Method and system for stall margin modulation as a function of engine health
WO2008152346A1 (en) Engine health monitoring
US11668248B2 (en) Start-up system and method for rotor bow mitigation
EP3607189A1 (en) Method and system for adjusting an operating parameter as a function of component health
US11702954B1 (en) Monitoring engine operation
CN111720218A (zh) 涡轮发动机的信号响应监测
EP4033420A1 (en) System and method for tracking engine and aircraft component data
EP3772630A1 (en) Heat exchanger blockage detection
US20240060426A1 (en) Systems and methods for determining gas turbine engine operating margins
US12333225B2 (en) System and method for monitoring and diagnosis of engine health using a snapshot-CEOD based approach
Meher-Homji et al. Condition monitoring and diagnostic aspects of gas turbine transient response
EP4318143B1 (en) System and method for addressing redundant sensor mismatch in an engine control system
EP4332708A1 (en) Engine control system and method with artificial intelligence sensor training
EP4556702A1 (en) Aircraft engine starter having an integrated data acquisition system
US12391393B2 (en) Aircraft propulsion system with inlet air monitoring system and method
CN118759893A (zh) 一种发动机的仿真控制方法、系统、设备及存储介质
Eustace et al. Fault signatures obtained from fault implant tests on an F404 engine

Legal Events

Date Code Title Description
A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20050210

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20050210

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20071002

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20071227

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20080715

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20080811

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20110815

Year of fee payment: 3

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20110815

Year of fee payment: 3

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120815

Year of fee payment: 4

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20130815

Year of fee payment: 5

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees