F02C

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Description

GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; combustion apparatus in which combustion takes place in a fluidised bed of fuel or other particles F23C 10/00; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B 11/00; using gas-turbine plants in vehicles, see the relevant vehicle classes)

Subclasses

SubclassTitle
1/00 Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid (by the use of combustion products F02C 3/00, F02C 5/00)
1/02 Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid (by the use of combustion products F02C 3/00, F02C 5/00) the working fluid being an unheated pressurised gas
1/04 Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid (by the use of combustion products F02C 3/00, F02C 5/00) the working fluid being heated indirectly
1/05 Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid (by the use of combustion products F02C 3/00, F02C 5/00) the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy
1/06 Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid (by the use of combustion products F02C 3/00, F02C 5/00) the working fluid being heated indirectly characterised by the type or source of heat, e.g. using nuclear or solar energy using reheated exhaust gas (F02C 1/08 takes precedence)
1/08 Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid (by the use of combustion products F02C 3/00, F02C 5/00) the working fluid being heated indirectly Semi-closed cycles
1/10 Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid (by the use of combustion products F02C 3/00, F02C 5/00) the working fluid being heated indirectly Closed cycles
3/00 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00)
3/02 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) using exhaust-gas pressure in a pressure exchanger to compress combustion-air (pressure exchangers per seF04F 13/00)
3/04 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16)
3/045 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) having compressor and turbine passages in a single rotor (F02C 3/073 takes precedence)
3/05 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) having compressor and turbine passages in a single rotor (F02C 3/073 takes precedence) the compressor and the turbine being of the radial flow type
3/055 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) the compressor being of the positive-displacement type
3/06 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) the compressor comprising only axial stages (F02C 3/1 takes precedence)
3/067 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) the compressor comprising only axial stages (F02C 3/1 takes precedence) having counter-rotating rotors (F02C 3/073 takes precedence)
3/073 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) the compressor comprising only axial stages (F02C 3/1 takes precedence) the compressor and turbine stages being concentric
3/08 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) the compressor comprising at least one radial stage (F02C 3/1 takes precedence)
3/09 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) the compressor comprising at least one radial stage (F02C 3/1 takes precedence) of the centripetal type
3/10 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) with another turbine driving an output shaft but not driving the compressor
3/107 Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C 5/00) having a turbine driving a compressor (power transmission arrangements F02C 7/36; control of working fluid flow F02C 9/16) with two or more rotors connected by power transmission

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Recent Patents

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Recent Publications

Publication #TitleFiling DatePub DatePatent Owner
2024/0167,681 AIRCRAFT ENGINE FOR NITROGEN OXIDE REDUCTIONFeb 27, 23May 23, 24Not available
2024/0167,887 ELECTRICAL CONNECTIVITY TO HIGH TEMPERATURE FILM SENSOR DEVICESNov 22, 22May 23, 24Not available
2024/0167,416 RECONFIGURABLE HYBRID SOLAR GAS TURBINE SYSTEM OPERATING IN A SEMI-OPEN CYCLEMay 25, 21May 23, 24Not available
2024/0167,418 Electrically Powered Supersonic and Hypersonic PropulsorNov 23, 23May 23, 24Not available
2024/0167,420 AIRCRAFT COMPRISING AT LEAST ONE AIR INTAKE DEVICE CONFIGURED TO LIMIT THE ONSET OF AERODYNAMIC NOISENov 17, 23May 23, 24Not available
2024/0167,422 GAS TURBINE ENGINES INCLUDING EMBEDDED ELECTRICAL MACHINES AND ASSOCIATED COOLING SYSTEMSOct 11, 23May 23, 24General Electric Company Polska sp. z o.o.; General Electric Company;
2024/0167,424 ENGINE POWER EXTRACTION SYSTEM AND METHOD FOR USING SAMENov 18, 22May 23, 24Not available
2024/0167,426 CONTRAIL DETECTION, DISCRIMINATION, AND CONTROLNov 21, 22May 23, 24Rosemount Aerospace Inc.
2024/0167,385 Turbine Engine AirfoilOct 16, 23May 23, 24Not available
2024/0167,417 POWER GENERATION SYSTEM, METHOD FOR DYNAMICALLY ADJUSTING A POWER GENERATION SYSTEM, AND METHOD FOR CONTROLLING A POWER GENERATION SYSTEMNov 28, 22May 23, 24Not available
2024/0167,419 PROCESS FOR USING WASTE HEAT FROM THE UTILIZATION OF LOW, NEUTRAL AND/OR NEGATIVE CARBON INTENSITY HYDROGENSep 22, 23May 23, 24Not available
2024/0167,421 FAN MODULE EQUIPPED WITH AN OIL TRANSFER DEVICEMar 09, 22May 23, 24SAFRAN AIRCRAFT ENGINES
2024/0167,423 AIRFOIL LAST CHANCE SCREEN UTILIZING EDM AND AFMNov 18, 22May 23, 24Not available
2024/0167,425 SYSTEMS AND METHODS FOR MODEL-BASED CONTROL OF GAS TURBINE SYSTEM CONSIDERING FLUID INJECTIONNov 21, 22May 23, 24Not available
2024/0167,427 INTER-COOLED PREHEAT OF STEAM INJECTED TURBINE ENGINEJan 29, 24May 23, 24Not available
2024/0167,433 DUAL COMPRESSION-EXPANSION PUMPS AND RELATED METHODSJan 03, 23May 23, 24Not available
2024/0167,571 DYNAMIC SEALING IN AN AIRCRAFT TURBINE ENGINE CONTROL VALVEMar 23, 22May 23, 24SAFRAN AEROSYSTEMS
2024/0157,183 SACRIFICIAL FIRE SHIELD FOR SHIELDING AN AIRCRAFT PARTNov 16, 22May 16, 24Not available
2024/0157,336 SYSTEMS AND METHODS FOR IN-SITU COKE REMOVAL FROM HOT-GAS PATH SURFACESMay 18, 23May 16, 24Not available
2024/0159,157 GAS TURBINE ENGINE BLEED AIR FLOW CONTROLJan 24, 23May 16, 24Not available

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