CS57391A2 - Two-rotor radial high-pressure gas turbine - Google Patents

Two-rotor radial high-pressure gas turbine Download PDF

Info

Publication number
CS57391A2
CS57391A2 CS91573A CS57391A CS57391A2 CS 57391 A2 CS57391 A2 CS 57391A2 CS 91573 A CS91573 A CS 91573A CS 57391 A CS57391 A CS 57391A CS 57391 A2 CS57391 A2 CS 57391A2
Authority
CS
Czechoslovakia
Prior art keywords
pressure
rotor
turbine
low
compressor
Prior art date
Application number
CS91573A
Other languages
Czech (cs)
English (en)
Inventor
Rolf Jan Mowill
Original Assignee
Rolf Jan Mowill
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 Rolf Jan Mowill filed Critical Rolf Jan Mowill
Publication of CS57391A2 publication Critical patent/CS57391A2/cs

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
    • F02C3/36—Open cycles
    • 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
    • F02C3/09—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 of the centripetal type
    • 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
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • F02C3/103—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor the compressor being of the centrifugal type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00—Engines characterised by fuel-air mixture compression
    • F02B1/02—Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04—Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/02—Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CS91573A 1990-03-05 1991-03-05 Two-rotor radial high-pressure gas turbine CS57391A2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US48813890A 1990-03-05 1990-03-05

Publications (1)

Publication Number Publication Date
CS57391A2 true CS57391A2 (en) 1991-12-17

Family

ID=23938465

Family Applications (1)

Application Number Title Priority Date Filing Date
CS91573A CS57391A2 (en) 1990-03-05 1991-03-05 Two-rotor radial high-pressure gas turbine

Country Status (4)

Country Link
EP (1) EP0452642B1 (fr)
JP (1) JP3200101B2 (fr)
CS (1) CS57391A2 (fr)
DE (1) DE69109173T2 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19854907A1 (de) * 1998-11-27 2000-05-31 Rolls Royce Deutschland Kühlluftführung an einer Axialturbine
US6925809B2 (en) 1999-02-26 2005-08-09 R. Jan Mowill Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
WO2009118471A1 (fr) * 2008-02-29 2009-10-01 Melchior Jean-Frederic Moteur a combustion interne a suralimentation pulsee
FR2950109B1 (fr) * 2009-09-17 2012-07-27 Turbomeca Turbomoteur a arbres paralleles
DE102015204466A1 (de) 2015-03-12 2016-09-15 Siemens Aktiengesellschaft Anordnung mit zwei Verdichtern, Verfahren zum Nachrüsten
CN109404137A (zh) * 2018-09-25 2019-03-01 杭州螺旋新能源科技有限公司 一种燃气轮机及大功率燃气轮机的启动方法
CN112228222B (zh) * 2020-11-06 2024-07-23 中国科学院上海高等研究院 分布式多轴燃气轮机及复合动力系统

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE748208C (de) * 1938-06-15 1944-10-28 Sulzer Ag Gasturbinenanlage
BE434623A (fr) 1938-06-15
DE833739C (de) * 1943-09-04 1952-03-10 Maschf Augsburg Nuernberg Ag Gasturbinenanlage
GB668834A (en) * 1948-11-02 1952-03-26 Power Jets Res & Dev Ltd Improvements in or relating to gas turbine power plant
CH283198A (de) * 1949-03-25 1952-05-31 Limited Centrax Power Units Gasturbinenanlage.
US2625012A (en) * 1950-04-18 1953-01-13 Gen Engineering And Res Corp Gas turbine power plant, including multiple fluid operated turbines
FR1126906A (fr) * 1951-08-08 1956-12-04 Turbine à gaz, plus spécialement pour véhicules
US2663141A (en) * 1952-05-03 1953-12-22 Boeing Co Gas turbine
CH363853A (de) * 1959-01-10 1962-08-15 Sulzer Ag Gasturbinenanlage mit zwei Wellen
US4286430A (en) * 1979-09-17 1981-09-01 Teledyne Industries, Inc. Gas turbine engine
SE453114B (sv) * 1986-04-29 1988-01-11 Asea Stal Ab Sett for drift av ett turbinaggregat

Also Published As

Publication number Publication date
DE69109173D1 (de) 1995-06-01
DE69109173T2 (de) 1995-08-31
JPH0586899A (ja) 1993-04-06
EP0452642A1 (fr) 1991-10-23
EP0452642B1 (fr) 1995-04-26
JP3200101B2 (ja) 2001-08-20

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