IT1053270B - Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material - Google Patents

Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material

Info

Publication number
IT1053270B
IT1053270B IT5280175A IT5280175A IT1053270B IT 1053270 B IT1053270 B IT 1053270B IT 5280175 A IT5280175 A IT 5280175A IT 5280175 A IT5280175 A IT 5280175A IT 1053270 B IT1053270 B IT 1053270B
Authority
IT
Italy
Prior art keywords
turbine
dimensioned
impellers
manufactured
ceramic material
Prior art date
Application number
IT5280175A
Other languages
Italian (it)
Original Assignee
United Turbine Ab & Co
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 & Co filed Critical United Turbine Ab & Co
Priority to IT5280175A priority Critical patent/IT1053270B/en
Application granted granted Critical
Publication of IT1053270B publication Critical patent/IT1053270B/en

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The compressor rotor (15) is turned by the turbine impeller (16). The turbine impeller is under dimensioned and incapable of producing the required driving force. A second working turbine impeller (17) produces not only working output (18) but also provides the additional energy required to turn the compressor rotor. The additional energy is transferred to the compressor by a first gear train (19) a free wheel coupling (20) and an infinitely variable gear (21). A second gear train (22) connects the variable gear (21) with the compressor rotor shaft. Variable pitch guide vanes (23) are provided between the two turbine impellers (16,17).
IT5280175A 1975-12-19 1975-12-19 Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material IT1053270B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
IT5280175A IT1053270B (en) 1975-12-19 1975-12-19 Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT5280175A IT1053270B (en) 1975-12-19 1975-12-19 Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material

Publications (1)

Publication Number Publication Date
IT1053270B true IT1053270B (en) 1981-08-31

Family

ID=11277562

Family Applications (1)

Application Number Title Priority Date Filing Date
IT5280175A IT1053270B (en) 1975-12-19 1975-12-19 Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material

Country Status (1)

Country Link
IT (1) IT1053270B (en)

Similar Documents

Publication Publication Date Title
GB1487324A (en) Gas turbine engines
SE7610579L (en) GASTURBINE TRANSMISSION FACILITY
GB1500400A (en) Conversion of the dynamic energy of sea waves to motive power
Whitfield et al. Study of incidence loss models in radial and mixed-flow turbomachinery
JPS5353833A (en) Vehicle having at least two driven axles
FR2336553A2 (en) Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material
IT1053270B (en) Gas turbine plant with two turbine impellers - has first turbine wheel under-dimensioned and manufactured from ceramic material
FR2422047A2 (en) Wind driven power generator - has turbine arranged for axial flow with impeller and stator blades which can pivot to form inlet damper
JPS5575502A (en) Radial turbine
GB1504911A (en) Multi-unit wind-operated generator
IT1097218B (en) Wind operated turbine for power generation - has slewing housing tapering from end with fixed guide vanes and vaned rotor
JPS5672300A (en) Device for driving guide vane of multistage centrifugal compressor
GB1119774A (en) Gas turbine engine
FR2360758A1 (en) Gas turbine for aviation propulsion - has differential gear between turbine and compressor and blower drive shafts
SE7610578L (en) GASTURBINE TRANSMISSION FACILITY
GB630164A (en) Improvements relating to gas turbines
GB1524259A (en) Turbines
GB1108069A (en) Two-stage hydraulic reaction turbine
GB1433750A (en) Gas turbine engines building elements
GB611761A (en) Improvements in or relating to hydraulic reversing gears
GB1364465A (en) Hydrodynamic torque converters
FR2281499A1 (en) Turbo generator with central combustion rotor - has expansion zone between normal shock wave and combustion zone
GB191360A (en) Improvements in or relating to fluid pressure turbines
IT1021912B (en) Gas turbine engine for vehicles - has infinitely variable gearing between turbine and compressor
FR2288222A1 (en) Gas turbine engine for vehicles - has infinitely variable gearing between turbine and compressor