ES2127586T3 - Procedimiento para la regulacion de un motor turborreactor. - Google Patents

Procedimiento para la regulacion de un motor turborreactor.

Info

Publication number
ES2127586T3
ES2127586T3 ES96106809T ES96106809T ES2127586T3 ES 2127586 T3 ES2127586 T3 ES 2127586T3 ES 96106809 T ES96106809 T ES 96106809T ES 96106809 T ES96106809 T ES 96106809T ES 2127586 T3 ES2127586 T3 ES 2127586T3
Authority
ES
Spain
Prior art keywords
sub
full load
regulation
soll
procedure
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
ES96106809T
Other languages
English (en)
Inventor
Joachim Dr Kurzke
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 GmbH
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 ES2127586T3 publication Critical patent/ES2127586T3/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
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/112—Purpose of the control system to prolong engine life by limiting temperatures
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)

Abstract

LA INVENCION SE REFIERE A UN PROCEDIMIENTO PARA LA REGULACION DE UN MECANISMO DE TURBOPROPULSION A CHORRO, DONDE SE AJUSTA Y SE ALMACENA UNA TEMPERATURA T{SUB,V SOLL} DE TURBINA DE CARGA COMPLETA CORREGIBLE, QUE SE DA A CONOCER PARA DIFERENTES MAGNITUDES DE LA SITUACION DE ENTRADA DE AIRE Y DEL AVION, POR MEDIO DE UN REGULADOR. PARA LA OBTENCION DE UN VALOR PS{SUB,7 SOLL} TEORICO DE PRESION DE TOBERAS QUE CORRESPONDE A LAS SITUACIONES DE ENTRADA DE AIRE DIFERENTES PARA CARGA COMPLETA SE CORRIGE LA TEMPERATURA T{SUB,V SOLL} DE TURBINA DE CARGA COMPLETA AJUSTADA DEPENDIENDO DEL TIEMPO DE OPERACION EN UN VALOR DE CORRECTURA DT{SUB,K}, QUE RESULTA A PARTIR DE UN CONJUNTO DE MAGNITUDES DE REGULACION Y DE ENTRADA MEDIDAS EN SITUACIONES DE OPERACION DE CARGA COMPLETA O CARGA PARCIAL ESTACIONARIA DEL MECANISMO DE PROPULSION. LA TEMPERATURA T{SUB,V SOLL} DE TURBINA DE CARGA COMPLETA MAXIMA ES IGUAL QUE LA TEMPERATURA T{SUB,V MAX} DE TURBINA MAXIMA ADMISIBLE MAS ALTA.
ES96106809T 1995-05-06 1996-04-30 Procedimiento para la regulacion de un motor turborreactor. Expired - Lifetime ES2127586T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19516693A DE19516693C1 (de) 1995-05-06 1995-05-06 Verfahren zur Regelung eines Turbo-Strahltriebwerks

Publications (1)

Publication Number Publication Date
ES2127586T3 true ES2127586T3 (es) 1999-04-16

Family

ID=7761262

Family Applications (1)

Application Number Title Priority Date Filing Date
ES96106809T Expired - Lifetime ES2127586T3 (es) 1995-05-06 1996-04-30 Procedimiento para la regulacion de un motor turborreactor.

Country Status (3)

Country Link
EP (1) EP0742355B1 (es)
DE (2) DE19516693C1 (es)
ES (1) ES2127586T3 (es)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10801361B2 (en) 2016-09-09 2020-10-13 General Electric Company System and method for HPT disk over speed prevention

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3893291A (en) * 1973-08-29 1975-07-08 Gen Motors Corp Gas turbine fuel control
US3956883A (en) * 1974-08-08 1976-05-18 Westinghouse Electric Corporation Smooth and highly responsive gas turbine temperature limit control especially useful in combined cycle electric power plants
GB2065779B (en) * 1979-12-21 1983-09-21 Rolls Royce Gas turbine fuel system
JPH02267328A (ja) * 1989-03-20 1990-11-01 General Electric Co <Ge> ガスタービンエンジンの制御装置および制御方法
EP0427952A1 (en) * 1989-11-16 1991-05-22 Westinghouse Electric Corporation Apparatus and method for combustion turbine generator overfuel limiting
US5267435A (en) * 1992-08-18 1993-12-07 General Electric Company Thrust droop compensation method and system

Also Published As

Publication number Publication date
EP0742355B1 (de) 1998-12-23
DE19516693C1 (de) 1996-08-22
DE59601031D1 (de) 1999-02-04
EP0742355A1 (de) 1996-11-13

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