ES2085298T3 - Mecanismo de turbina de gas con compresor diagonal - Google Patents

Mecanismo de turbina de gas con compresor diagonal

Info

Publication number
ES2085298T3
ES2085298T3 ES90110164T ES90110164T ES2085298T3 ES 2085298 T3 ES2085298 T3 ES 2085298T3 ES 90110164 T ES90110164 T ES 90110164T ES 90110164 T ES90110164 T ES 90110164T ES 2085298 T3 ES2085298 T3 ES 2085298T3
Authority
ES
Spain
Prior art keywords
diagonal
gas turbine
compressor
turbine mechanism
drive mechanisms
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
ES90110164T
Other languages
English (en)
Inventor
Marc Boffo
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 ES2085298T3 publication Critical patent/ES2085298T3/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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

EL INVENTO SE REFIERE A UN MECANISMO PROPULSOR POR TURBINAS A GAS CON COMPRESOR DIAGONAL (1) Y UN DIFUSOR DIAGONAL QUE SE LE AÑADE A ESTE (2). CON ELLO, EL DIFUSOR DIAGONAL (2) SE SITUA DENTRO DE LA CAMARA DE COMBUSTION CIRCULAR (6) Y ESTA SE ALIMENTA DESDE LA PARTE INTERIOR RADIAL, EN CONTRACORRIENTE, CON AIRE COMPRIMIDO. TALES MECANISMOS PROPULSORES SON MAS COMPACTOS Y POSEEN UN GRADO DE EFECTIVIDAD MAYOR QUE LOS MECANISMO PROPULSORES DE TURBINAS CON UN COMPRESOR RADIAL.
ES90110164T 1989-06-10 1990-05-29 Mecanismo de turbina de gas con compresor diagonal Expired - Lifetime ES2085298T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3919097 1989-06-10

Publications (1)

Publication Number Publication Date
ES2085298T3 true ES2085298T3 (es) 1996-06-01

Family

ID=6382561

Family Applications (1)

Application Number Title Priority Date Filing Date
ES90110164T Expired - Lifetime ES2085298T3 (es) 1989-06-10 1990-05-29 Mecanismo de turbina de gas con compresor diagonal

Country Status (6)

Country Link
US (1) US5094069A (es)
EP (1) EP0402693B1 (es)
JP (1) JPH03164529A (es)
CA (1) CA2018576A1 (es)
DE (1) DE59010207D1 (es)
ES (1) ES2085298T3 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5490388A (en) * 1992-09-28 1996-02-13 Asea Brown Boveri Ltd. Gas turbine combustion chamber having a diffuser
US5279126A (en) * 1992-12-18 1994-01-18 United Technologies Corporation Diffuser-combustor
DE4419338A1 (de) * 1994-06-03 1995-12-07 Abb Research Ltd Gasturbine und Verfahren zu ihrem Betrieb
US6363706B1 (en) 1998-12-24 2002-04-02 Alliedsignal Apparatus and method to increase turbine power
US7080515B2 (en) * 2002-12-23 2006-07-25 Siemens Westinghouse Power Corporation Gas turbine can annular combustor
US7010921B2 (en) * 2004-06-01 2006-03-14 General Electric Company Method and apparatus for cooling combustor liner and transition piece of a gas turbine
US7451600B2 (en) * 2005-07-06 2008-11-18 Pratt & Whitney Canada Corp. Gas turbine engine combustor with improved cooling
EP1892378A1 (de) * 2006-08-22 2008-02-27 Siemens Aktiengesellschaft Gasturbine
FR2927950B1 (fr) * 2008-02-27 2011-12-23 Snecma Ensemble diffuseur-redresseur pour une turbomachine
DE102011108887A1 (de) * 2011-07-28 2013-01-31 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenzentripetalringbrennkammer sowie Verfahren zur Strömungsführung
GB2503495B (en) * 2012-06-29 2014-12-03 Rolls Royce Plc Spool for turbo machinery
WO2016183588A2 (en) * 2015-05-14 2016-11-17 University Of Central Florida Research Foundation, Inc. Compressor flow extraction apparatus and methods for supercritical co2 oxy-combustion power generation system
US10465907B2 (en) 2015-09-09 2019-11-05 General Electric Company System and method having annular flow path architecture
US10598380B2 (en) 2017-09-21 2020-03-24 General Electric Company Canted combustor for gas turbine engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1002314A (fr) * 1946-09-06 1952-03-05 Turbo-moteur
US2640319A (en) * 1949-02-12 1953-06-02 Packard Motor Car Co Cooling of gas turbines
GB783448A (en) * 1955-01-26 1957-09-25 Rudolph Birmann Improvements in or relating to elastic fluid mechanism such as compressors, turbines, or diffusers
US3365892A (en) * 1965-08-10 1968-01-30 Derderian George Turbomachine
US3404853A (en) * 1966-12-12 1968-10-08 George B. Miller Radial turbine engines and applications thereof
US3546880A (en) * 1969-08-04 1970-12-15 Avco Corp Compressors for gas turbine engines
GB2123136A (en) * 1982-06-22 1984-01-25 Curtiss Wright Corp A fuel burner and combustor assembly for a gas turbine engine
FR2576358A1 (fr) * 1985-01-24 1986-07-25 Wieczorek Julien Module haute-pression et haute-temperature pour turboreacteurs

Also Published As

Publication number Publication date
EP0402693B1 (de) 1996-03-20
US5094069A (en) 1992-03-10
DE59010207D1 (de) 1996-04-25
EP0402693A1 (de) 1990-12-19
CA2018576A1 (en) 1990-12-10
JPH03164529A (ja) 1991-07-16

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