WO2008089925A3 - Hydrodynamischer antrieb einer hochdruckverdichterwelle eines gasturbinentriebwerks - Google Patents

Hydrodynamischer antrieb einer hochdruckverdichterwelle eines gasturbinentriebwerks Download PDF

Info

Publication number
WO2008089925A3
WO2008089925A3 PCT/EP2008/000402 EP2008000402W WO2008089925A3 WO 2008089925 A3 WO2008089925 A3 WO 2008089925A3 EP 2008000402 W EP2008000402 W EP 2008000402W WO 2008089925 A3 WO2008089925 A3 WO 2008089925A3
Authority
WO
WIPO (PCT)
Prior art keywords
pressure compressor
gas turbine
drive shaft
low
turbine engine
Prior art date
Application number
PCT/EP2008/000402
Other languages
English (en)
French (fr)
Other versions
WO2008089925A2 (de
Inventor
Reinhard Kernchen
Heinz Hoeller
Steffen Kaemmerer
Tillmann Koerner
Original Assignee
Voith Patent Gmbh
Reinhard Kernchen
Heinz Hoeller
Steffen Kaemmerer
Tillmann Koerner
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 Voith Patent Gmbh, Reinhard Kernchen, Heinz Hoeller, Steffen Kaemmerer, Tillmann Koerner filed Critical Voith Patent Gmbh
Publication of WO2008089925A2 publication Critical patent/WO2008089925A2/de
Publication of WO2008089925A3 publication Critical patent/WO2008089925A3/de

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
    • F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
    • F02C3/113—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission with variable power transmission between rotors
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D33/00—Rotary fluid couplings or clutches of the hydrokinetic type
    • F16D33/02—Rotary fluid couplings or clutches of the hydrokinetic type controlled by changing the flow of the liquid in the working circuit, while maintaining a completely filled working circuit
    • F16D33/04—Rotary fluid couplings or clutches of the hydrokinetic type controlled by changing the flow of the liquid in the working circuit, while maintaining a completely filled working circuit by altering the position of blades
    • 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
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • 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
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/406—Transmission of power through hydraulic systems
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

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

Abstract

Die Erfindung betrifft ein Gasturbinentriebwerk, insbesondere Flugtriebwerk, mit einer Brennkammer (1) und einer Gasturbine (2) zur Erzeugung von Antriebsleistung und/oder Schub; mit einem wenigstens zweistufigen Verdichter, umfassend einen Niederdruckverdichter (3) und einen Hochdruckverdichter (4), die wenigstens mittelbar von der Gasturbine antreibbar sind, um Luft oder ein Gasgemisch für die Brennkammer zu verdichten, und welche jeweils eine Antriebswelle (3.1, 4.1) aufweisen, wobei der Hochdruckverdichter über eine drehmomentübertragende Triebverbindung' zwischen der Antriebswelle (3.1) des Niederdruckverdichters und der Antriebswelle (4.1) des Hochdruckverdichters vom Niederdruckverdichter äntreibbar ist und in der Trieb Verbindung eine regelbare. hydrodynamische Maschine zur Übertragung der gesamten Antriebsleistung von der Niederdruckverdichterantriebswelle auf die Hochdruckverdichterantriebswelle oder eines Teils der Antriebsleistung angeordnet ist. Die Erfindung betrifft zudem ein Verfahren zum Regeln des Antriebs der genannten Hochdruckverdichterwelle.
PCT/EP2008/000402 2007-01-23 2008-01-19 Hydrodynamischer antrieb einer hochdruckverdichterwelle eines gasturbinentriebwerks WO2008089925A2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007004274A DE102007004274A1 (de) 2007-01-23 2007-01-23 Gasturbinentriebwerk, insbesondere Flugtriebwerk
DE102007004274.6 2007-01-23

Publications (2)

Publication Number Publication Date
WO2008089925A2 WO2008089925A2 (de) 2008-07-31
WO2008089925A3 true WO2008089925A3 (de) 2008-09-25

Family

ID=39523737

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2008/000402 WO2008089925A2 (de) 2007-01-23 2008-01-19 Hydrodynamischer antrieb einer hochdruckverdichterwelle eines gasturbinentriebwerks

Country Status (2)

Country Link
DE (1) DE102007004274A1 (de)
WO (1) WO2008089925A2 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2457346C1 (ru) * 2010-12-16 2012-07-27 Открытое акционерное общество Авиамоторный научно-технический комплекс "Союз" Газотурбинный привод
DE102014112182A1 (de) 2014-08-26 2016-03-03 Rolls-Royce Deutschland Ltd & Co Kg Flugtriebwerk und Verfahren zum Betreiben eines Flugtriebwerkes
GB2547674A (en) * 2016-02-25 2017-08-30 Rolls Royce Plc Gas turbine engine
GB201619960D0 (en) 2016-11-25 2017-01-11 Rolls Royce Plc Gas turbine engine
US11220960B2 (en) 2019-10-03 2022-01-11 Raytheon Technologies Corporation Superposition gearbox for engine performance
CN114542294B (zh) * 2022-02-16 2024-06-18 中国航发沈阳发动机研究所 一种高马赫数涡轮发动机中央传动系统总体结构

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1030104B (de) * 1956-10-05 1958-05-14 Messerschmitt Boelkow Blohm Ein- oder mehrstufige Brennkraftturbine mit mehrstufigem Verdichter
US2955424A (en) * 1954-11-08 1960-10-11 Parsons C A & Co Ltd Gas turbine plants
US3673797A (en) * 1970-12-08 1972-07-04 Perkins Services Nv Compound power plant
DE2559172A1 (de) * 1975-12-30 1977-07-14 United Turbine Ab & Co Gasturbinenanlage
US4062186A (en) * 1976-05-13 1977-12-13 General Electric Company Apparatus for windmill starts in gas turbine engines
DE2655868A1 (de) * 1976-12-09 1978-06-15 Motoren Turbinen Union Gasturbinenanlage, insbesondere gasturbinentriebwerk fuer ein kraftfahrzeug
WO1995002120A1 (en) * 1993-07-06 1995-01-19 Rolls-Royce Plc Shaft power transfer in gas turbine engines
EP1724455A2 (de) * 2005-05-04 2006-11-22 Rolls-Royce plc Antriebvorrichtung
EP1777392A1 (de) * 2005-10-21 2007-04-25 Hispano Suiza Antriebsvorrichtung für Hilfsantriebe eines Gasturbinenantriebs

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2955424A (en) * 1954-11-08 1960-10-11 Parsons C A & Co Ltd Gas turbine plants
DE1030104B (de) * 1956-10-05 1958-05-14 Messerschmitt Boelkow Blohm Ein- oder mehrstufige Brennkraftturbine mit mehrstufigem Verdichter
US3673797A (en) * 1970-12-08 1972-07-04 Perkins Services Nv Compound power plant
DE2559172A1 (de) * 1975-12-30 1977-07-14 United Turbine Ab & Co Gasturbinenanlage
US4062186A (en) * 1976-05-13 1977-12-13 General Electric Company Apparatus for windmill starts in gas turbine engines
DE2655868A1 (de) * 1976-12-09 1978-06-15 Motoren Turbinen Union Gasturbinenanlage, insbesondere gasturbinentriebwerk fuer ein kraftfahrzeug
WO1995002120A1 (en) * 1993-07-06 1995-01-19 Rolls-Royce Plc Shaft power transfer in gas turbine engines
EP1724455A2 (de) * 2005-05-04 2006-11-22 Rolls-Royce plc Antriebvorrichtung
EP1777392A1 (de) * 2005-10-21 2007-04-25 Hispano Suiza Antriebsvorrichtung für Hilfsantriebe eines Gasturbinenantriebs

Also Published As

Publication number Publication date
DE102007004274A1 (de) 2008-07-31
WO2008089925A2 (de) 2008-07-31

Similar Documents

Publication Publication Date Title
US10738710B2 (en) Multi-shaft gas turbine engine
IN2012DN02042A (de)
GB201316509D0 (en) Method for optimizing the speed of a twin-spool turbojet engine fan, and architecture for implementing same
US8461704B2 (en) Gas turbine engine apparatus
US9951696B2 (en) Twin-shaft gas turbine for multiple frequency power generation
WO2008089925A3 (de) Hydrodynamischer antrieb einer hochdruckverdichterwelle eines gasturbinentriebwerks
RU2017103126A (ru) Гибридизация компрессоров турбореактивного двигателя
EP1939430A3 (de) Turbofantriebwerksanordnung und Montageverfahren dafür
EP1916390A3 (de) Gasturbinentriebwerksanordnung und Verfahren zu deren Zusammenbau
US20130139518A1 (en) Multiple turboshaft engine control method and system for helicopters
EP2728140A3 (de) Boostervorrichtung für eine Gasturbine mit einem Getriebe
WO2008088660A3 (en) Multi-stage compressor/driver system and method of operation
EP2472084A3 (de) Verfahren und System zum Antreiben eines Fahrzeuges
AU2013273476B2 (en) Combination of two gas turbines to drive a load
EP2048330A3 (de) Systeme und Verfahren mit mehreren Drehmomentpfaden für Gasturbinenmotoren
EP2177735A3 (de) Turbofan
EP4276295A3 (de) Getriebeturbolüfter mit überdrehzahlschutz
WO2011009455A3 (de) Axialkolbenmotor, verfahren zum betrieb eines axialkolbenmotors sowie verfahren zur herstellung eines wärmeübertragers eines axialkolbenmotors
WO2010111357A3 (en) High-flow-capacity centrifugal hydrogen gas compression systems, methods and components therefor
GB2411437A (en) Aircraft gas turbine engine
WO2013001361A3 (en) Apparatus and method for reducing air mass flow for extended range low emissions combustion for single shaft gas turbines
WO2012007638A3 (en) A solution for controlling a turbo compressor
EP2522817A3 (de) Systeme und Verfahren für ein optimiertes Abschalten einer Gasturbine
WO2006096796A3 (en) Torque drive mechanism for gas compressor
EP2592235A3 (de) Verdichteranordnungen für einen Gasturbinenmotor

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 08707135

Country of ref document: EP

Kind code of ref document: A2

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 08707135

Country of ref document: EP

Kind code of ref document: A2