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ES2048801T3 - Procedimiento y dispositivo para la regulacion de la alimentacion de combustible de una turbina de gas. - Google Patents

Procedimiento y dispositivo para la regulacion de la alimentacion de combustible de una turbina de gas.

Info

Publication number
ES2048801T3
ES2048801T3 ES89116270T ES89116270T ES2048801T3 ES 2048801 T3 ES2048801 T3 ES 2048801T3 ES 89116270 T ES89116270 T ES 89116270T ES 89116270 T ES89116270 T ES 89116270T ES 2048801 T3 ES2048801 T3 ES 2048801T3
Authority
ES
Spain
Prior art keywords
gas turbine
regulation
procedure
acceleration
fuel feed
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 - Lifetime
Application number
ES89116270T
Other languages
English (en)
Inventor
Friedrich Schwamm
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union 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 Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Application granted granted Critical
Publication of ES2048801T3 publication Critical patent/ES2048801T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02C9/28—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
    • F05D2270/04—Purpose of the control system to control acceleration (u)
    • F05D2270/044—Purpose of the control system to control acceleration (u) by making it as high as possible

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

EL INVENTO SE REFIERE A UN PROCEDIMIENTO PARA LA REGULACION DE LA ENTRADA DE CARBURANTE DE UNA TURBINA DE GAS DEPENDIENDO POR LO MENOS DE UNA TEMPERATURA DE TURBINA DE GAS DEPENDIENDO POR LO MENOS DE UNA TEMPERATURA DE TURBINA Y UNA ACELERACION DE EJE EN LA QUE LA SEÑAL DE VALOR DE LA TEMPERATURA REAL ES DIFERENCIADA Y EL FACTOR DE AMPLIACION DE ESTA SEÑAL SE AJUSTA EN RELACION CON LA ACELERACION DEL EJE. DE ESTA FORMA SE LOGRA EN LA ACELERACION PARTIENDO DE LA MARCHA LIBRE COMO FUERA DE LA ZONA DE CARGA PARCIAL UNA OSCILACION OPTIMA, LO MAS CORTA POSIBLE Y LIBRE DE SOBREOSCILACIONES SOBRE EL ESTADO DE SERVICIO A PLENA CARGA.
ES89116270T 1988-09-09 1989-09-04 Procedimiento y dispositivo para la regulacion de la alimentacion de combustible de una turbina de gas. Expired - Lifetime ES2048801T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3830804A DE3830804A1 (de) 1988-09-09 1988-09-09 Verfahren und anordnung zur regelung der brennstoffzufuhr einer gasturbine

Publications (1)

Publication Number Publication Date
ES2048801T3 true ES2048801T3 (es) 1994-04-01

Family

ID=6362684

Family Applications (1)

Application Number Title Priority Date Filing Date
ES89116270T Expired - Lifetime ES2048801T3 (es) 1988-09-09 1989-09-04 Procedimiento y dispositivo para la regulacion de la alimentacion de combustible de una turbina de gas.

Country Status (3)

Country Link
EP (1) EP0358138B1 (es)
DE (2) DE3830804A1 (es)
ES (1) ES2048801T3 (es)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19523845C2 (de) * 1995-06-30 2002-08-01 Mtu Aero Engines Gmbh Verfahren und Anordnung zur Regelung der Treibstoffzufuhr für Triebwerke
DE19902437C5 (de) * 1999-01-22 2017-01-12 General Electric Technology Gmbh Verfahren und Vorrichtung zum schnellen Anfahren und zur schnellen Leistungssteigerung einer Gasturbinenanlage
EP1870565A1 (de) * 2006-06-23 2007-12-26 Siemens Aktiengesellschaft Vermeidung unzulässig hoher Drehzahlen an Turbosätzen

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4217867A (en) * 1979-05-29 1980-08-19 General Motors Corporation Low overshoot engine speed governor
CA1177936A (en) * 1981-04-24 1984-11-13 Rowland M. Evans Stress limiter apparatus for a gas turbine engine
US4449360A (en) * 1981-04-30 1984-05-22 Aviation Electric Ltd. Stall detector and surge prevention feature for a gas turbine engine
US4423594A (en) * 1981-06-01 1984-01-03 United Technologies Corporation Adaptive self-correcting control system
US4490791A (en) * 1982-04-19 1984-12-25 Chandler Evans Inc. Adaptive gas turbine acceleration control
GB2121986B (en) * 1982-05-21 1986-01-15 Lucas Ind Plc Gas turbine engine fuel control systems

Also Published As

Publication number Publication date
DE58906689D1 (de) 1994-02-24
EP0358138A2 (de) 1990-03-14
EP0358138B1 (de) 1994-01-12
EP0358138A3 (de) 1991-05-08
DE3830804A1 (de) 1990-03-15
DE3830804C2 (es) 1992-05-27

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