GB1353400A - Gas turbine plant - Google Patents

Gas turbine plant

Info

Publication number
GB1353400A
GB1353400A GB3080271A GB3080271A GB1353400A GB 1353400 A GB1353400 A GB 1353400A GB 3080271 A GB3080271 A GB 3080271A GB 3080271 A GB3080271 A GB 3080271A GB 1353400 A GB1353400 A GB 1353400A
Authority
GB
United Kingdom
Prior art keywords
series
turbine
compressor
blades
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
GB3080271A
Other languages
English (en)
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
Publication of GB1353400A publication Critical patent/GB1353400A/en
Expired 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
    • F02C3/06—Gas-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
    • 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
    • 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
    • F02C3/06—Gas-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
    • F02C3/073—Gas-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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/914—Device 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)
GB3080271A 1970-07-03 1971-07-01 Gas turbine plant Expired GB1353400A (en)

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 (1)

Publication Number Publication Date
GB1353400A true GB1353400A (en) 1974-05-15

Family

ID=5775690

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3080271A Expired GB1353400A (en) 1970-07-03 1971-07-01 Gas turbine plant

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
FR2097170B1 (enExample) 1975-06-06
DE2032964B2 (de) 1973-09-20
DE2032964C3 (de) 1974-04-25
US3756019A (en) 1973-09-04

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees