DE2843043C2 - Einrichtung zur Bereitstellung einer Leistungsreserve bei Flugzeug-Gasturbinentriebwerken - Google Patents

Einrichtung zur Bereitstellung einer Leistungsreserve bei Flugzeug-Gasturbinentriebwerken

Info

Publication number
DE2843043C2
DE2843043C2 DE2843043A DE2843043A DE2843043C2 DE 2843043 C2 DE2843043 C2 DE 2843043C2 DE 2843043 A DE2843043 A DE 2843043A DE 2843043 A DE2843043 A DE 2843043A DE 2843043 C2 DE2843043 C2 DE 2843043C2
Authority
DE
Germany
Prior art keywords
signal
engine
power
relay
trimming
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
Application number
DE2843043A
Other languages
German (de)
English (en)
Other versions
DE2843043A1 (de
Inventor
Leon D. Rancho Palos Verdes Calif. Lewis
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.)
Garrett Corp
Original Assignee
Garrett Corp
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 Garrett Corp filed Critical Garrett Corp
Publication of DE2843043A1 publication Critical patent/DE2843043A1/de
Application granted granted Critical
Publication of DE2843043C2 publication Critical patent/DE2843043C2/de
Expired legal-status Critical Current

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
    • 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
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/051—Thrust
    • 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
    • F05D2270/01—Purpose of the control system
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • 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
    • F05D2270/01—Purpose of the control system
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • F05D2270/093—Purpose of the control system to cope with emergencies of one engine in a multi-engine system

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Control Of Turbines (AREA)
  • Control Of Eletrric Generators (AREA)
DE2843043A 1977-10-17 1978-10-03 Einrichtung zur Bereitstellung einer Leistungsreserve bei Flugzeug-Gasturbinentriebwerken Expired DE2843043C2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US84275177A 1977-10-17 1977-10-17

Publications (2)

Publication Number Publication Date
DE2843043A1 DE2843043A1 (de) 1979-04-19
DE2843043C2 true DE2843043C2 (de) 1986-05-15

Family

ID=25288171

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2843043A Expired DE2843043C2 (de) 1977-10-17 1978-10-03 Einrichtung zur Bereitstellung einer Leistungsreserve bei Flugzeug-Gasturbinentriebwerken

Country Status (8)

Country Link
JP (1) JPS5851137B2 (sv)
CA (1) CA1139113A (sv)
DE (1) DE2843043C2 (sv)
ES (1) ES474267A1 (sv)
FR (1) FR2406078A1 (sv)
GB (1) GB1591217A (sv)
IT (1) IT1106135B (sv)
SE (1) SE439038B (sv)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4500966A (en) * 1982-05-26 1985-02-19 Chandler Evans Inc. Super contingency aircraft engine control
FR2665927B1 (fr) * 1990-08-16 1992-10-30 Snecma Dispositif compensateur de temperature devant la turbine d'une turbomachine d'aviation.
WO2010039197A1 (en) 2008-09-23 2010-04-08 Aerovironment Inc. Powerplant and related control system and method
FR2990002B1 (fr) * 2012-04-27 2016-01-22 Snecma Turbomachine comportant un systeme de surveillance comprenant un module d'engagement d'une fonction de protection de la turbomachine et procede de surveillance
US10233756B2 (en) 2013-08-27 2019-03-19 Garrett Transportation I Inc. Two-sided turbocharger wheel with differing blade parameters

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB680290A (en) * 1949-10-10 1952-10-01 Lucas Ltd Joseph Means for synchronising air-craft engines
GB1006654A (en) * 1961-01-27 1965-10-06 Dowty Fuel Syst Ltd Improved fuel system for internal combustion engines
GB1012941A (en) * 1961-03-10 1965-12-15 Plessey Co Ltd Improvements in or relating to fuel control devices for internal combustion engines
US3771314A (en) * 1971-10-04 1973-11-13 Gen Electric Gas turbine engine emergency speed control system
US3811273A (en) * 1973-03-08 1974-05-21 United Aircraft Corp Slaved fuel control for multi-engined aircraft
US3971208A (en) * 1974-04-01 1976-07-27 The Garrett Corporation Gas turbine fuel control
US3987279A (en) * 1975-04-22 1976-10-19 The Boeing Company Automatic performance reserve (APR) system

Also Published As

Publication number Publication date
SE439038B (sv) 1985-05-28
CA1139113A (en) 1983-01-11
FR2406078B1 (sv) 1983-08-26
SE7810755L (sv) 1979-04-18
DE2843043A1 (de) 1979-04-19
IT1106135B (it) 1985-11-11
JPS5467114A (en) 1979-05-30
GB1591217A (en) 1981-06-17
IT7851369A0 (it) 1978-10-04
FR2406078A1 (fr) 1979-05-11
ES474267A1 (es) 1979-04-16
JPS5851137B2 (ja) 1983-11-15

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Legal Events

Date Code Title Description
OAP Request for examination filed
OD Request for examination
8125 Change of the main classification

Ipc: F02C 9/32

D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee