IT1088432B - METHOD AND APPARATUS FOR THE DETECTION AND CORRECTION OF FAULTS IN A CONTROL SYSTEM FOR A GAS TURBINE ENGINE - Google Patents

METHOD AND APPARATUS FOR THE DETECTION AND CORRECTION OF FAULTS IN A CONTROL SYSTEM FOR A GAS TURBINE ENGINE

Info

Publication number
IT1088432B
IT1088432B IT3056177A IT3056177A IT1088432B IT 1088432 B IT1088432 B IT 1088432B IT 3056177 A IT3056177 A IT 3056177A IT 3056177 A IT3056177 A IT 3056177A IT 1088432 B IT1088432 B IT 1088432B
Authority
IT
Italy
Prior art keywords
faults
correction
detection
control system
gas turbine
Prior art date
Application number
IT3056177A
Other languages
Italian (it)
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Application granted granted Critical
Publication of IT1088432B publication Critical patent/IT1088432B/en

Links

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/46—Emergency fuel control
    • 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
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • 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
    • F05D2270/00—Control
    • F05D2270/50—Control logic embodiments
    • F05D2270/54—Control logic embodiments by electronic means, e.g. electronic tubes, transistors or IC's within an electronic circuit
    • 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
    • F05D2270/00—Control
    • F05D2270/70—Type of control algorithm
    • 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
    • F05D2270/00—Control
    • F05D2270/70—Type of control algorithm
    • F05D2270/71—Type of control algorithm synthesized, i.e. parameter computed by a mathematical model
IT3056177A 1976-12-20 1977-12-09 METHOD AND APPARATUS FOR THE DETECTION AND CORRECTION OF FAULTS IN A CONTROL SYSTEM FOR A GAS TURBINE ENGINE IT1088432B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US75205076A 1976-12-20 1976-12-20

Publications (1)

Publication Number Publication Date
IT1088432B true IT1088432B (en) 1985-06-10

Family

ID=25024630

Family Applications (1)

Application Number Title Priority Date Filing Date
IT3056177A IT1088432B (en) 1976-12-20 1977-12-09 METHOD AND APPARATUS FOR THE DETECTION AND CORRECTION OF FAULTS IN A CONTROL SYSTEM FOR A GAS TURBINE ENGINE

Country Status (7)

Country Link
JP (1) JPS5395410A (en)
BE (1) BE862071A (en)
CA (1) CA1188775A (en)
DE (1) DE2756681C2 (en)
FR (1) FR2374513A1 (en)
GB (1) GB1597129A (en)
IT (1) IT1088432B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111475889A (en) * 2020-03-30 2020-07-31 西安交通大学 Physical and data-driven aeroengine digital twin modeling method

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4228650A (en) * 1978-05-01 1980-10-21 United Technologies Corporation Simulated parameter control for gas turbine engine
US4212161A (en) * 1978-05-01 1980-07-15 United Technologies Corporation Simulated parameter control for gas turbine engine
DE3101035C2 (en) * 1980-11-11 1983-01-20 Gebrüder Sulzer AG, 8401 Winterthur Control circuit with auxiliary controlled variable
US4504905A (en) * 1981-09-05 1985-03-12 Lucas Industries Plc Digital control system including means for maintaining signals supplied thereby within limiting values
JPS5894004A (en) * 1981-11-30 1983-06-04 Hitachi Ltd Optimum parameter retrieving device for controller of plant control system
JPS6045733A (en) * 1983-08-23 1985-03-12 Toyota Motor Corp Device for controlling moving portion of electronically- regulated gas turbine engine
JPS6047824A (en) * 1983-08-25 1985-03-15 Toyota Motor Corp Movable-part controlling method for electronically controlled gas-turbine engine
JPS6047825A (en) * 1983-08-26 1985-03-15 Toyota Motor Corp Movable-part controlling method for electronically controlled gas-turbine engine
US4845617A (en) * 1987-06-01 1989-07-04 United Technologies Corporation Autofeather state maintenance
US4992946A (en) * 1988-06-20 1991-02-12 General Electric Company Data link for gas turbine engine control
DE19729101A1 (en) * 1997-07-08 1999-01-14 Bosch Gmbh Robert System for operating an internal combustion engine, in particular a motor vehicle
US6568166B2 (en) 2000-12-22 2003-05-27 Pratt & Whitney Canada Corp. Back-up control apparatus for turbo machine
US6687596B2 (en) * 2001-08-31 2004-02-03 General Electric Company Diagnostic method and system for turbine engines
US7216071B2 (en) * 2002-04-23 2007-05-08 United Technologies Corporation Hybrid gas turbine engine state variable model
DE102007025447A1 (en) * 2006-10-09 2008-04-17 Siemens Ag Method for controlling and / or regulating an industrial process
US7630820B2 (en) * 2007-04-24 2009-12-08 Honeywell International Inc. Feedback control system and method that selectively utilizes observer estimates
DE102008041571B4 (en) 2008-08-26 2019-12-05 Robert Bosch Gmbh Method and device for error handling during operation of an internal combustion engine
CN114508421B (en) * 2021-12-14 2023-05-05 泸州懋威科技有限公司 Microminiature aeroengine control system and operation method thereof

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2851855A (en) * 1953-03-27 1958-09-16 Curtiss Wright Corp Fuel control system for jet engines
US3851157A (en) * 1973-07-09 1974-11-26 United Aircraft Corp Self-correcting feedback control system
GB1523275A (en) * 1974-08-20 1978-08-31 Cav Ltd Digital control system for a gas turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111475889A (en) * 2020-03-30 2020-07-31 西安交通大学 Physical and data-driven aeroengine digital twin modeling method
CN111475889B (en) * 2020-03-30 2022-12-06 西安交通大学 Physical and data-driven aeroengine digital twin modeling method

Also Published As

Publication number Publication date
BE862071A (en) 1978-04-14
DE2756681C2 (en) 1986-06-05
FR2374513A1 (en) 1978-07-13
GB1597129A (en) 1981-09-03
DE2756681A1 (en) 1978-06-22
CA1188775A (en) 1985-06-11
FR2374513B1 (en) 1984-10-19
JPS5395410A (en) 1978-08-21

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