GB1338671A - Control devices for gas turbine power plants - Google Patents

Control devices for gas turbine power plants

Info

Publication number
GB1338671A
GB1338671A GB2055171A GB2055171A GB1338671A GB 1338671 A GB1338671 A GB 1338671A GB 2055171 A GB2055171 A GB 2055171A GB 2055171 A GB2055171 A GB 2055171A GB 1338671 A GB1338671 A GB 1338671A
Authority
GB
United Kingdom
Prior art keywords
nozzle
turbine
pressure
shaft
fuel flow
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
GB2055171A
Other languages
English (en)
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of GB1338671A publication Critical patent/GB1338671A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control
    • F02K1/17—Control or regulation conjointly with another control with control of fuel supply

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
GB2055171A 1970-02-04 1971-04-19 Control devices for gas turbine power plants Expired GB1338671A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7003923A FR2079536A5 (enExample) 1970-02-04 1970-02-04

Publications (1)

Publication Number Publication Date
GB1338671A true GB1338671A (en) 1973-11-28

Family

ID=9050070

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2055171A Expired GB1338671A (en) 1970-02-04 1971-04-19 Control devices for gas turbine power plants

Country Status (3)

Country Link
US (1) US3719047A (enExample)
FR (1) FR2079536A5 (enExample)
GB (1) GB1338671A (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2172006B1 (enExample) * 1972-02-18 1975-06-13 Snecma
US4077203A (en) * 1977-04-13 1978-03-07 Chandler Evans Inc. Emergency metering valve and geometry actuator control device
US4414807A (en) * 1980-12-08 1983-11-15 United Technologies Corporation Method and apparatus for controlling a gas turbine engine
DE363301T1 (de) 1988-09-20 1990-07-05 United Technologies Corp., Hartford, Conn. Steuervorrichtung fuer gasturbinenanlagen.
US7011498B2 (en) 1998-04-03 2006-03-14 Athena Technologies, Inc. Optimization method for power generation systems
US9506405B2 (en) 1998-04-03 2016-11-29 Rockwell Collins Control Technologies, Inc. Apparatus and method for controlling power generation system
US6171055B1 (en) * 1998-04-03 2001-01-09 Aurora Flight Sciences Corporation Single lever power controller for manned and unmanned aircraft
US7069728B2 (en) * 2003-07-29 2006-07-04 Pratt & Whitney Canada Corp. Multi-position BOV actuator
DE102008009604A1 (de) * 2008-02-15 2009-08-20 Rolls-Royce Deutschland Ltd & Co Kg Gehäusestrukturierung zum Stabilisieren der Strömung in einer Strömungsarbeitsmaschine
US11022037B2 (en) * 2018-01-04 2021-06-01 General Electric Company Gas turbine engine thermal management system

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3300979A (en) * 1967-01-31 Apparatus for controlling the afterburner load of a jet engine according to the jet pipe aperture
US2933887A (en) * 1953-07-16 1960-04-26 Rolls Royce Compound gas turbine engine with control for low-pressure rotor
US2874540A (en) * 1955-12-08 1959-02-24 United Aircraft Corp Drive unit
US3023575A (en) * 1957-12-16 1962-03-06 Bendix Corp Normal and emergency fuel control system for gas turbine engines
US3232053A (en) * 1963-09-13 1966-02-01 Bendix Corp Fuel feed and power control apparatus for combustion engines
FR1391769A (fr) * 1963-11-29 1965-03-12 Snecma Dispositif de régulation ou de limitation de températures des turbo machines et turbines à gaz

Also Published As

Publication number Publication date
DE2104782A1 (de) 1971-08-12
US3719047A (en) 1973-03-06
DE2104782B2 (de) 1977-05-12
FR2079536A5 (enExample) 1971-11-12

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee