IT1106135B - Incrementatore di spinta per motori a turbina - Google Patents

Incrementatore di spinta per motori a turbina

Info

Publication number
IT1106135B
IT1106135B IT51369/78A IT5136978A IT1106135B IT 1106135 B IT1106135 B IT 1106135B IT 51369/78 A IT51369/78 A IT 51369/78A IT 5136978 A IT5136978 A IT 5136978A IT 1106135 B IT1106135 B IT 1106135B
Authority
IT
Italy
Prior art keywords
turbine engines
thrust increase
thrust
increase
engines
Prior art date
Application number
IT51369/78A
Other languages
English (en)
Other versions
IT7851369A0 (it
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 IT7851369A0 publication Critical patent/IT7851369A0/it
Application granted granted Critical
Publication of IT1106135B publication Critical patent/IT1106135B/it

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 Eletrric Generators (AREA)
  • Control Of Turbines (AREA)
IT51369/78A 1977-10-17 1978-10-04 Incrementatore di spinta per motori a turbina IT1106135B (it)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
IT7851369A0 IT7851369A0 (it) 1978-10-04
IT1106135B true IT1106135B (it) 1985-11-11

Family

ID=25288171

Family Applications (1)

Application Number Title Priority Date Filing Date
IT51369/78A IT1106135B (it) 1977-10-17 1978-10-04 Incrementatore di spinta per motori a turbina

Country Status (8)

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

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.
US8200413B2 (en) 2008-09-23 2012-06-12 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
ES474267A1 (es) 1979-04-16
IT7851369A0 (it) 1978-10-04
JPS5467114A (en) 1979-05-30
GB1591217A (en) 1981-06-17
SE7810755L (sv) 1979-04-18
SE439038B (sv) 1985-05-28
JPS5851137B2 (ja) 1983-11-15
DE2843043A1 (de) 1979-04-19
DE2843043C2 (de) 1986-05-15
CA1139113A (en) 1983-01-11
FR2406078B1 (it) 1983-08-26
FR2406078A1 (fr) 1979-05-11

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