DE2032964C3 - Gasturbinenanlage mit gegenläufigen Laufrädern - Google Patents

Gasturbinenanlage mit gegenläufigen Laufrädern

Info

Publication number
DE2032964C3
DE2032964C3 DE2032964A DE2032964A DE2032964C3 DE 2032964 C3 DE2032964 C3 DE 2032964C3 DE 2032964 A DE2032964 A DE 2032964A DE 2032964 A DE2032964 A DE 2032964A DE 2032964 C3 DE2032964 C3 DE 2032964C3
Authority
DE
Germany
Prior art keywords
turbine
compressor
pressure
blade
gas turbine
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
DE2032964A
Other languages
German (de)
English (en)
Other versions
DE2032964A1 (de
DE2032964B2 (de
Inventor
Heinrich 4200 Oberhausen-Sterkrade Holzapfel
Jan-Albert Vilp Konings (Niederlande)
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.)
Gutehoffnungshutte Sterkrade AG
Original Assignee
Gutehoffnungshutte Sterkrade AG
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 Gutehoffnungshutte Sterkrade AG filed Critical Gutehoffnungshutte Sterkrade AG
Priority to DE2032964A priority Critical patent/DE2032964C3/de
Priority to GB3080271A priority patent/GB1353400A/en
Priority to FR7124250A priority patent/FR2097170B1/fr
Priority to US00159449A priority patent/US3756019A/en
Publication of DE2032964A1 publication Critical patent/DE2032964A1/de
Publication of DE2032964B2 publication Critical patent/DE2032964B2/de
Application granted granted Critical
Publication of DE2032964C3 publication Critical patent/DE2032964C3/de
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00Rotary kinetic fluid motors or pumps
    • Y10S415/914Device to control boundary layer

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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
DE2032964A 1970-07-03 1970-07-03 Gasturbinenanlage mit gegenläufigen Laufrädern Expired DE2032964C3 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE2032964A DE2032964C3 (de) 1970-07-03 1970-07-03 Gasturbinenanlage mit gegenläufigen Laufrädern
GB3080271A GB1353400A (en) 1970-07-03 1971-07-01 Gas turbine plant
FR7124250A FR2097170B1 (enExample) 1970-07-03 1971-07-02
US00159449A US3756019A (en) 1970-07-03 1971-07-02 Gas turbine blade arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2032964A DE2032964C3 (de) 1970-07-03 1970-07-03 Gasturbinenanlage mit gegenläufigen Laufrädern

Publications (3)

Publication Number Publication Date
DE2032964A1 DE2032964A1 (de) 1972-01-05
DE2032964B2 DE2032964B2 (de) 1973-09-20
DE2032964C3 true DE2032964C3 (de) 1974-04-25

Family

ID=5775690

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2032964A Expired DE2032964C3 (de) 1970-07-03 1970-07-03 Gasturbinenanlage mit gegenläufigen Laufrädern

Country Status (4)

Country Link
US (1) US3756019A (enExample)
DE (1) DE2032964C3 (enExample)
FR (1) FR2097170B1 (enExample)
GB (1) GB1353400A (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4301649A (en) * 1979-08-24 1981-11-24 General Motors Corporation Single rotor engine with turbine exhausting to subatmospheric pressure
DE3004980C2 (de) * 1980-02-11 1984-10-11 Rudolf E. New York N.Y. Fengler Propeller-Überschall-Strahltriebwerk für Flugzeuge und Flugkörper
US4693075A (en) * 1984-10-31 1987-09-15 Andrew Sabatiuk Gas turbine engines employing fixed volume combustion
US4757682A (en) * 1985-05-20 1988-07-19 Eugene Bahniuk Axial flow turbine
DE3542541A1 (de) * 1985-12-02 1987-06-04 Ingelheim Peter Graf Von Vorrichtung zur erzeugung einer vortriebskraft
US5224339A (en) * 1990-12-19 1993-07-06 Allied-Signal Inc. Counterflow single rotor turbojet and method
BG99154A (en) * 1994-11-01 1996-06-28 Givechev Gas turbine engine
RU2306424C1 (ru) * 2006-03-17 2007-09-20 Закрытое акционерное общество "ЭНТЭК" Проточная часть паровой турбины
US8192141B1 (en) * 2007-04-05 2012-06-05 The United States Of America As Represented By The Secretary Of The Air Force Dual compression rotor
FR2951226B1 (fr) * 2009-10-14 2013-01-04 Turbomeca Dispositif de filtrage d'air en entree de moteur a combustion interne avec moyen de ventilation
US20110146289A1 (en) * 2009-12-21 2011-06-23 John Lewis Baughman Power extraction method
US20110146228A1 (en) * 2009-12-21 2011-06-23 John Lewis Baughman Power extraction system
US20120110976A1 (en) * 2010-11-08 2012-05-10 Marius Angelo Paul Universal aero space , naval eternal technology systems
US20220333611A1 (en) * 2021-04-14 2022-10-20 Stokes Technology Development Ltd. Counter-rotating axial air moving device

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE892046C (de) * 1953-08-20 Maschinenfabrik Augsburg-Nürnlberg A. G., Augsburg Leitapparat für axial durchströmte Kreiselradmaschinen
DE735392C (de) * 1941-06-26 1943-05-13 Aeg Einrichtung zur Kuehlung von Gasturbinenschaufeln
US2702985A (en) * 1944-01-31 1955-03-01 Power Jets Res & Dev Ltd Gas turbine power plant with power take-off from rotatable guide blading
DE1085718B (de) * 1958-11-26 1960-07-21 Daimler Benz Ag Gasturbinentriebwerk
FR1455278A (fr) * 1965-08-05 1966-04-01 Snecma Turboréacteur à double flux

Also Published As

Publication number Publication date
DE2032964A1 (de) 1972-01-05
FR2097170A1 (enExample) 1972-03-03
GB1353400A (en) 1974-05-15
FR2097170B1 (enExample) 1975-06-06
DE2032964B2 (de) 1973-09-20
US3756019A (en) 1973-09-04

Similar Documents

Publication Publication Date Title
DE2032964C3 (de) Gasturbinenanlage mit gegenläufigen Laufrädern
DE1951356C3 (de) Gasturbinentriebwerk für Flugzeuge
DE1626130A1 (de) Gasturbinentriebwerksanlage
DE2831802A1 (de) Gasturbinentriebwerk und verfahren zu dessen betrieb
DE2141265A1 (de) Gasturbine
WO2005045203A2 (de) Verfahren zum betreiben einer turbomaschine, und turbomaschine
DE2454054A1 (de) Innentriebwerk bzw. gasgenerator fuer gasturbinentriebwerke
DE112007001870T5 (de) Dampfturbinen
DE19814627C2 (de) Kühlluftentnahme aus dem Diffusorteil eines Kompressors einer Gasturbine
DE2128217B2 (de) Mehrstufiger Verdichter
DE1628261B2 (de) Luftentnahmevorrichtung an axialverdichtern
DE1428106B2 (de) Verstellvorrichtung zum gemeinsamen verstellen der leit schaufeln der axialstufen eines mehrstufigen kreiselver dichters
DE1428216A1 (de) Mehrstufen-Axialkompressor
DE700618C (de) Gasturbinenanlage
DE925984C (de) Teilbeaufschlagte Gasturbine
DE1948363A1 (de) Gasturbinen-Strahltriebwerksanlage
EP0296440A1 (de) Dampfturbine für Teillastbetrieb
EP2886806A1 (de) Strömungsmaschine
CH277112A (de) Abgasturbine zum Antrieb eines Ladegebläses.
DE102006010863B4 (de) Turbomaschine, insbesondere Verdichter
DE940950C (de) Mechanisch zeitweilig in einem ihrer normalen Laufrichtung entgegengesetzten Sinn angetriebene Gasturbine
DE655698C (de) Verdichteranlage fuer Druckfeuerung von Dampferzeugern oder Aufladung von Brennkraftmaschinen
DE2033756C (de) Siedewasserreaktoranlage
AT147696B (de) Brennkraftturbine.
EP3172407B1 (de) Gasturbine mit einer kühlung der letzten turbinenstufe

Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)