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
2024/0149,404 CENTERING A WASHER TO A FASTENER ELEMENT DURING INSTALLATIONNov 09, 22May 09, 24Not available
2024/0151,397 INJECTION TECHNIQUES FOR GAS TURBINE SYSTEMSJan 19, 24May 09, 24Not available
2024/0151,158 BEARING SUPPORT ASSEMBLYJan 11, 24May 09, 24Not available
2024/0151,179 COMPOUNDED TURBO POWER UNIT WITH BOOST COMBUSTORNov 04, 22May 09, 24Not available
2024/0151,182 DEVICE FOR CENTERING AND GUIDING A SHAFT OF AN AIRCRAFT TURBINE ENGINEMar 08, 22May 09, 24Not available
2024/0151,185 GAS TURBINE ENGINE WITH ACOUSTIC SPACING OF THE FAN BLADES AND OUTLET GUIDE VANESNov 03, 22May 09, 24General Electric Company
2024/0151,162 SECTIONED ENGINE STRUCTURE FOR A GAS TURBINE ENGINEAug 21, 23May 09, 24Not available
2024/0151,180 OPTIMIZED CO-GENERATING SYSTEM AND RECOVERY METHOD FOR POWER, WATER AND NITROGENNov 03, 22May 09, 24Saudi Arabian Oil Company
2024/0151,183 SYSTEMS AND METHODS FOR PURGING A FUEL MANIFOLD OF A GAS TURBINE ENGINENov 09, 22May 09, 24Not available
2024/0151,186 DELAY TIME CALCULATION METHOD AND GAS TURBINE CONTROL METHOD, AND DELAY TIME CALCULATION APPARATUS AND CONTROL APPARATUS FOR GAS TURBINEOct 19, 23May 09, 24Not available
2024/0151,181 SUPPORT STRUCTURE FOR BEARING COMPARTMENTOct 27, 23May 09, 24Not available
2024/0151,184 METHOD OF DETERMINING AN OPERATING CONDITION OF A VALVE OF AN AIRCRAFT SYSTEMNov 27, 23May 09, 24Not available
2024/0150,029 INNER COWL ARRANGEMENT FOR GAS TURBINE ENGINEOct 10, 23May 09, 24Rolls Royce plc
2024/0150,033 DIHYDROGEN SUPPLY SYSTEM FOR AN AIRCRAFT ENGINEJul 21, 23May 09, 24Not available
2024/0154,144 SOLID OXIDE FUEL CELL STACK FOR AN AIRCRAFT ENGINEOct 31, 23May 09, 24Airbus Operations GmbH
2024/0154,496 HYDROGEN PRODUCTION USING ELECTRICAL POWER GENERATED BY GAS PRESSURE LETDOWNNov 03, 22May 09, 24Not available
2024/0141,790 METHODS AND APPARATUS FOR PASSIVE FAN BLADE TIP CLEARANCE CONTROLJan 13, 23May 02, 24Not available
2024/0141,792 FAN BLADE FOR A GAS TURBINE ENGINEOct 27, 23May 02, 24Rolls Royce plc
2024/0141,798 GAS TURBINE ENGINE TURBINE SECTION WITH AXIAL SEALOct 31, 22May 02, 24RAYTHEON TECHNOLOGIES CORPORATION
2024/0141,801 TURBINE ENGINE DEVICE WITH POWER SYSTEM GENERATOR, AND VEHICLE COMPRISING SUCH A DEVICEJan 05, 22May 02, 24Not available

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