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GB1474609A - Gas turbine power plant - Google Patents

Gas turbine power plant

Info

Publication number
GB1474609A
GB1474609A GB2173574A GB2173574A GB1474609A GB 1474609 A GB1474609 A GB 1474609A GB 2173574 A GB2173574 A GB 2173574A GB 2173574 A GB2173574 A GB 2173574A GB 1474609 A GB1474609 A GB 1474609A
Authority
GB
United Kingdom
Prior art keywords
turbine
rotor
plant
gas turbine
compressor
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
GB2173574A
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.)
United Turbine AB and Co KG
Original Assignee
United Turbine AB and Co KG
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 United Turbine AB and Co KG filed Critical United Turbine AB and Co KG
Publication of GB1474609A publication Critical patent/GB1474609A/en
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
    • F02C7/00Features, 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
    • F02C7/36Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Retarders (AREA)

Abstract

1474609 Gas turbine plant UNITED TURBINE AB & CO KB 16 May 1974 [22 May 1973] 21735/74 Heading F1G In a gas turbine plant comprising at least one compressor rotor 15, at least one first turbine rotor 28 and a variable transmission 10 connecting the rotors 15, 28, the power transference path from the transmission 10 to and including the compressor rotor has substantially less moment of inertia than the path from and including the first turbine rotor to the transmission. At least one second turbine rotor 23 connected to a power output shaft 18 can rotate independently of the first turbine rotor 28. Thus the acceleration and deceleration performance of the plant when used in a road vehicle is improved. The plant may include gearing 30, freewheel 11 and a fluid clutch, the variable transmission 10 being of belt type. The compressor rotor 15 may be of light metal and the turbine rotors 23, 28 of similarly light ceramic or of heavier material as appropriate. Figs. 1b and 2 to 4 (not shown) illustrate modified plants incorporating, e.g., two compressor stages (15a, 15b) on the same or separate shafts, and planetary gearing (30).
GB2173574A 1973-05-22 1974-05-16 Gas turbine power plant Expired GB1474609A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7307157 1973-05-22

Publications (1)

Publication Number Publication Date
GB1474609A true GB1474609A (en) 1977-05-25

Family

ID=20317549

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2173574A Expired GB1474609A (en) 1973-05-22 1974-05-16 Gas turbine power plant

Country Status (5)

Country Link
JP (1) JPS5020119A (en)
DE (1) DE2424330C2 (en)
FR (1) FR2230863B1 (en)
GB (1) GB1474609A (en)
IT (1) IT1011479B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2198188A (en) * 1986-11-20 1988-06-08 Mtu Muenchen Gmbh Gas turbine propulsion unit
NL2000190C2 (en) * 2006-08-18 2008-02-19 Macvonk S Postorder B V Drive device.

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE402147B (en) * 1975-12-05 1978-06-19 United Turbine Ab & Co GAS TURBINE SYSTEM WITH THREE IN THE SAME GAS PASSAGE ORGANIZED COAXIAL TURBINE ROTORS
FR2336553A2 (en) * 1975-12-23 1977-07-22 United Turbine Ab & Co Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material
SE401711B (en) * 1976-09-24 1978-05-22 Kronogard Sven Olof GASTURBINE TRANSMISSION FACILITY
EP0104921A3 (en) * 1982-09-27 1985-04-10 The Garrett Corporation Turbine engine system
DE4113247A1 (en) * 1991-04-23 1992-10-29 Bayerische Motoren Werke Ag Gas turbine plant for motor vehicle - has compressor rotor and turbine rotor formed by rotors of mass-produced exhaust gas turbochargers

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1601671A1 (en) * 1962-12-03 1971-01-14 Teves Gmbh Alfred Drive for a hydrostatic transmission
US3280554A (en) * 1964-09-30 1966-10-25 Ford Motor Co Motor vehicle gas turbine drive
US3546879A (en) * 1968-08-19 1970-12-15 Eaton Yale & Towne Two-shaft turbine with means for controlling relative shaft rotation
US3632222A (en) * 1970-10-21 1972-01-04 Avco Corp Damping means for differential gas turbine engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2198188A (en) * 1986-11-20 1988-06-08 Mtu Muenchen Gmbh Gas turbine propulsion unit
GB2198188B (en) * 1986-11-20 1991-05-29 Mtu Muenchen Gmbh Gas turbine engine comprising a gas generator.
NL2000190C2 (en) * 2006-08-18 2008-02-19 Macvonk S Postorder B V Drive device.

Also Published As

Publication number Publication date
IT1011479B (en) 1977-01-20
FR2230863B1 (en) 1979-10-19
FR2230863A1 (en) 1974-12-20
JPS5020119A (en) 1975-03-03
DE2424330C2 (en) 1984-03-15
DE2424330A1 (en) 1974-12-19

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee