IT971435B - Apparato regolatore per un impian to a turbine a gas a titolo di esempio di un apparato motore di autoveicolo o di aeromobile - Google Patents

Apparato regolatore per un impian to a turbine a gas a titolo di esempio di un apparato motore di autoveicolo o di aeromobile

Info

Publication number
IT971435B
IT971435B IT32367/72A IT3236772A IT971435B IT 971435 B IT971435 B IT 971435B IT 32367/72 A IT32367/72 A IT 32367/72A IT 3236772 A IT3236772 A IT 3236772A IT 971435 B IT971435 B IT 971435B
Authority
IT
Italy
Prior art keywords
motor vehicle
gas turbine
aircraft engine
engine system
turbine system
Prior art date
Application number
IT32367/72A
Other languages
English (en)
Original Assignee
Mtu Muenchen Gmbh
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 Mtu Muenchen Gmbh filed Critical Mtu Muenchen Gmbh
Application granted granted Critical
Publication of IT971435B publication Critical patent/IT971435B/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
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F02C9/32—Control of fuel supply characterised by throttling of fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Velocity Or Acceleration (AREA)
  • Feedback Control In General (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
IT32367/72A 1971-12-21 1972-11-30 Apparato regolatore per un impian to a turbine a gas a titolo di esempio di un apparato motore di autoveicolo o di aeromobile IT971435B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2163344A DE2163344C3 (de) 1971-12-21 1971-12-21 Regeleinrichtung für eine Gasturbinenanlage, z. B. ein Kraftfahrzeug- oder Flugtriebwerk

Publications (1)

Publication Number Publication Date
IT971435B true IT971435B (it) 1974-04-30

Family

ID=5828610

Family Applications (1)

Application Number Title Priority Date Filing Date
IT32367/72A IT971435B (it) 1971-12-21 1972-11-30 Apparato regolatore per un impian to a turbine a gas a titolo di esempio di un apparato motore di autoveicolo o di aeromobile

Country Status (7)

Country Link
US (1) US3886730A (it)
JP (1) JPS5740333B2 (it)
DE (1) DE2163344C3 (it)
FR (1) FR2164840B1 (it)
GB (1) GB1414468A (it)
IT (1) IT971435B (it)
SE (1) SE376947B (it)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4397148A (en) * 1980-07-02 1983-08-09 General Electric Company Control system for an augmented turbofan engine
GB2217477B (en) * 1988-04-05 1992-04-15 Rolls Royce Plc An engine control unit for a turbomachine
GB2218537B (en) * 1988-05-11 1993-02-17 Rolls Royce Plc Engine control
US7437871B2 (en) * 2002-05-31 2008-10-21 General Electric Company Automatic engine protection system for use when electronic parts of a control system are exposed to overtemperature conditions

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB675368A (en) * 1949-03-31 1952-07-09 Franklin Faller Offner Improved device for controlling engine acceleration and/or speed
US2948114A (en) * 1956-03-17 1960-08-09 Hispano Suiza Sa Engine fuel control including acceleration-biased control signal selector
US3007307A (en) * 1956-05-14 1961-11-07 Napier & Son Ltd Speed selector with delayed temperature datum adjustment
GB892514A (en) * 1957-10-23 1962-03-28 United Aircraft Corp Improvements relating to control apparatus for turbine-type power plants
US3158996A (en) * 1959-01-08 1964-12-01 Power Jets Res & Dev Ltd Control systems for gas turbine engines
US3019604A (en) * 1959-01-19 1962-02-06 Gen Motors Corp Turbojet thrust computer
US3098356A (en) * 1960-10-20 1963-07-23 Sperry Rand Corp Fuel control system for gas turbine engines
FR1291954A (fr) * 1961-06-02 1962-04-27 United Aircraft Corp Dispositif de réglage de l'alimentation en combustible d'une turbine à gaz
US3691405A (en) * 1971-08-10 1972-09-12 Ultra Electronics Ltd Thermocouple response time compensation circuit arrangement

Also Published As

Publication number Publication date
DE2163344B2 (de) 1973-11-29
FR2164840B1 (it) 1975-11-07
GB1414468A (en) 1975-11-19
SE376947B (it) 1975-06-16
US3886730A (en) 1975-06-03
DE2163344C3 (de) 1974-07-04
JPS4872507A (it) 1973-09-29
JPS5740333B2 (it) 1982-08-26
FR2164840A1 (it) 1973-08-03
DE2163344A1 (de) 1973-09-06

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