DE3666966D1 - Dual entry radial turbine gas generator - Google Patents

Dual entry radial turbine gas generator

Info

Publication number
DE3666966D1
DE3666966D1 DE8686901145T DE3666966T DE3666966D1 DE 3666966 D1 DE3666966 D1 DE 3666966D1 DE 8686901145 T DE8686901145 T DE 8686901145T DE 3666966 T DE3666966 T DE 3666966T DE 3666966 D1 DE3666966 D1 DE 3666966D1
Authority
DE
Germany
Prior art keywords
gas generator
radial turbine
turbine gas
dual entry
entry radial
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
DE8686901145T
Other languages
English (en)
Inventor
Rolf Mowill
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.)
Ulstein Turbine AS
Original Assignee
Ulstein Turbine AS
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 Ulstein Turbine AS filed Critical Ulstein Turbine AS
Priority claimed from PCT/NO1986/000012 external-priority patent/WO1986004643A1/en
Application granted granted Critical
Publication of DE3666966D1 publication Critical patent/DE3666966D1/de
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
    • F02C3/10—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
    • 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
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)

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)
DE8686901145T 1985-02-05 1986-02-05 Dual entry radial turbine gas generator Expired DE3666966D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/698,586 US4641495A (en) 1985-02-05 1985-02-05 Dual entry radial turbine gas generator
PCT/NO1986/000012 WO1986004643A1 (en) 1985-02-05 1986-02-05 Dual entry radial turbine gas generator

Publications (1)

Publication Number Publication Date
DE3666966D1 true DE3666966D1 (de) 1989-12-21

Family

ID=24805863

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8686901145T Expired DE3666966D1 (de) 1985-02-05 1986-02-05 Dual entry radial turbine gas generator

Country Status (4)

Country Link
US (1) US4641495A (de)
EP (1) EP0210249B1 (de)
CA (1) CA1262638A (de)
DE (1) DE3666966D1 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5081832A (en) * 1990-03-05 1992-01-21 Rolf Jan Mowill High efficiency, twin spool, radial-high pressure, gas turbine engine
US5628182A (en) * 1993-07-07 1997-05-13 Mowill; R. Jan Star combustor with dilution ports in can portions
US5377483A (en) * 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
US5613357A (en) * 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
US5638674A (en) * 1993-07-07 1997-06-17 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor
US5572862A (en) * 1993-07-07 1996-11-12 Mowill Rolf Jan Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
US5924276A (en) * 1996-07-17 1999-07-20 Mowill; R. Jan Premixer with dilution air bypass valve assembly
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
US6397576B1 (en) * 1999-10-12 2002-06-04 Alm Development, Inc. Gas turbine engine with exhaust compressor having outlet tap control
US6460324B1 (en) * 1999-10-12 2002-10-08 Alm Development, Inc. Gas turbine engine
US6363708B1 (en) * 1999-10-12 2002-04-02 Alm Development, Inc. Gas turbine engine
US7603841B2 (en) * 2001-07-23 2009-10-20 Ramgen Power Systems, Llc Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel
US6694743B2 (en) 2001-07-23 2004-02-24 Ramgen Power Systems, Inc. Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall
US7003961B2 (en) * 2001-07-23 2006-02-28 Ramgen Power Systems, Inc. Trapped vortex combustor
US7104068B2 (en) * 2003-08-28 2006-09-12 Siemens Power Generation, Inc. Turbine component with enhanced stagnation prevention and corner heat distribution
US6968697B2 (en) * 2003-09-17 2005-11-29 Honeywell International Inc. Integral compressor housing of gas turbine engines
US7628018B2 (en) * 2008-03-12 2009-12-08 Mowill R Jan Single stage dual-entry centriafugal compressor, radial turbine gas generator
JP5629321B2 (ja) 2009-09-13 2014-11-19 リーン フレイム インコーポレイテッド 燃焼装置用の入口予混合器
US20120067054A1 (en) * 2010-09-21 2012-03-22 Palmer Labs, Llc High efficiency power production methods, assemblies, and systems
US9651138B2 (en) 2011-09-30 2017-05-16 Mtd Products Inc. Speed control assembly for a self-propelled walk-behind lawn mower
US9033670B2 (en) 2012-04-11 2015-05-19 Honeywell International Inc. Axially-split radial turbines and methods for the manufacture thereof
US9115586B2 (en) 2012-04-19 2015-08-25 Honeywell International Inc. Axially-split radial turbine
WO2014109788A1 (en) * 2013-01-10 2014-07-17 United Technologies Corporation Gas generator with mount having air passages
US9476305B2 (en) 2013-05-13 2016-10-25 Honeywell International Inc. Impingement-cooled turbine rotor
US10202856B2 (en) * 2014-09-02 2019-02-12 United Technologies Corporation Decoupled gas turbine engine
US11788464B2 (en) 2019-05-30 2023-10-17 Joseph Michael Teets Advanced 2-spool turboprop engine
GB201915309D0 (en) * 2019-10-23 2019-12-04 Rolls Royce Plc Turboshaft

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2405919A (en) * 1940-03-02 1946-08-13 Power Jets Res & Dev Ltd Fluid flow energy transformer
US2435836A (en) * 1944-12-13 1948-02-10 Gen Electric Centrifugal compressor
US2470565A (en) * 1945-10-09 1949-05-17 Ingersoll Rand Co Surge preventing device for centrifugal compressors
GB609926A (en) * 1946-03-25 1948-10-08 Adrian Albert Lombard Improvements in or relating to internal-combustion turbines
US2695499A (en) * 1949-08-22 1954-11-30 Power Jets Res & Dev Ltd Gas turbine power unit
US3625003A (en) * 1970-09-08 1971-12-07 Gen Motors Corp Split compressor gas turbine
US4251985A (en) * 1979-07-17 1981-02-24 General Motors Corporation Bleed valve control circuit

Also Published As

Publication number Publication date
EP0210249A1 (de) 1987-02-04
US4641495A (en) 1987-02-10
CA1262638A (en) 1989-11-07
EP0210249B1 (de) 1989-11-15

Similar Documents

Publication Publication Date Title
DE3666966D1 (de) Dual entry radial turbine gas generator
IT1197110B (it) Turbina a gas
ES545169A0 (es) Generador de gas
DK547786D0 (da) Vindturbine
DE3675290D1 (de) Gasturbinengehaeuseaufbau.
ES2022438B3 (es) Gondola motriz de turbina de gas
FR2582876B1 (fr) Groupe generateur hydro-electrique portatif
DE3688967D1 (de) Solargenerator.
DE68908698D1 (de) Gasgenerator.
NO850046L (no) Gassturbin
DE3861239D1 (de) Gaserzeuger.
DE3661224D1 (en) Gas turbine combustor
NO860062L (no) Fremgangsmaate for utvikling av mekanisk energi.
DK160953C (da) Udstoedsgasturboladerturbine
DE3770135D1 (de) Gasturbinenanlage.
DE3585231D1 (de) Gasturbinenmotor.
EP0224429A3 (en) Gas turbine engine augmentor
DK0378085T3 (da) Udstødningsgasturbinegeneratoranlæg
GB8520202D0 (en) Gas turbine aero-engine
FR2585408B1 (fr) Turbine a gaz axiale
KR880009854U (ko) 메탄가스 발생장치
KR870008051U (ko) 산소 가스 발생기
GB8530984D0 (en) Gas turbines
IT8548402A0 (it) Turbina assiale a gas
ATA33685A (de) Windkraftmaschine

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee