ES390841A1 - Control apparatus for a gas turbine engine - Google Patents

Control apparatus for a gas turbine engine

Info

Publication number
ES390841A1
ES390841A1 ES390841A ES390841A ES390841A1 ES 390841 A1 ES390841 A1 ES 390841A1 ES 390841 A ES390841 A ES 390841A ES 390841 A ES390841 A ES 390841A ES 390841 A1 ES390841 A1 ES 390841A1
Authority
ES
Spain
Prior art keywords
signals
nozzles
gas turbine
control apparatus
turbine engine
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
ES390841A
Other languages
Spanish (es)
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
Joseph Lucas Industries Ltd
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 Lucas Industries Ltd, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Publication of ES390841A1 publication Critical patent/ES390841A1/en
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
    • F02C9/32—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)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Improvements in control devices for heat engines and, more particularly, for gas turbine heat engines, including a gas generator, a drive turbine and nozzles to control the passage of gases from the generator to the drive turbine, characterized by that the apparatus comprises means responsive to servo pressure signals and operable to move the nozzles, means to generate a fluid pressure, valve means operable by electrical signals to derive said servo pressure signals from said fluid pressure, means that respond to other signals to modify the position of the nozzles and means to generate said electrical signals in response to the operating conditions of the heat engine. (Machine-translation by Google Translate, not legally binding)
ES390841A 1970-04-25 1971-04-23 Control apparatus for a gas turbine engine Expired ES390841A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1998870 1970-04-25

Publications (1)

Publication Number Publication Date
ES390841A1 true ES390841A1 (en) 1973-06-01

Family

ID=10138466

Family Applications (1)

Application Number Title Priority Date Filing Date
ES390841A Expired ES390841A1 (en) 1970-04-25 1971-04-23 Control apparatus for a gas turbine engine

Country Status (6)

Country Link
BR (1) BR7102485D0 (en)
CA (1) CA947094A (en)
DE (1) DE2120103A1 (en)
ES (1) ES390841A1 (en)
FR (1) FR2086362B1 (en)
GB (1) GB1331983A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3999373A (en) * 1975-07-11 1976-12-28 General Motors Corporation Automotive gas turbine control
US4266401A (en) * 1977-12-22 1981-05-12 The Garrett Corporation Gas turbine engine fuel control

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2667228A (en) * 1949-02-24 1954-01-26 Cyrus F Wood Aircraft fuel and propeller pitch control
US3199293A (en) * 1963-08-15 1965-08-10 Gen Electric Two shaft gas turbine control system
US3243596A (en) * 1963-11-21 1966-03-29 Gen Electric Gas turbine power system stabilizer

Also Published As

Publication number Publication date
FR2086362B1 (en) 1974-09-27
BR7102485D0 (en) 1973-04-12
DE2120103A1 (en) 1971-11-11
GB1331983A (en) 1973-09-26
CA947094A (en) 1974-05-14
FR2086362A1 (en) 1971-12-31

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