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

Not Available
Subclass Title
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)

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Recent Patents

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Recent Publications

Not Available
Publication #TitleFiling DatePub DatePatent Owner
2018/0355,802 GEARED TURBOFAN WITH LOW PRESSURE TURBINE FEATURES Jun 12, 17 Dec 13, 18 , Not available
2018/0355,798 PLENUM FOR COOLING TURBINE FLOWPATH COMPONENTS AND BLADES Jun 08, 17 Dec 13, 18 , General Electric Company
2018/0355,791 AXI-CENTRIFUGAL COMPRESSOR Aug 06, 18 Dec 13, 18 , Honeywell International Inc.
2018/0355,739 FLOW MODULATING AIRFOIL APPARATUS Jun 12, 17 Dec 13, 18 , Not available
2018/0356,093 METHODS OF OPERATING A ROTATING DETONATION COMBUSTOR AT APPROXIMATELY CONSTANT DETONATION CELL SIZE Jun 09, 17 Dec 13, 18 , Not available
2018/0355,764 LOW-POWER BOWED ROTOR PREVENTION SYSTEM Feb 28, 17 Dec 13, 18 , Not available
2018/0355,801 SYSTEM AND METHOD FOR CLEANING COOLING PASSAGES OF A COMBUSTION CHAMBER Feb 14, 17 Dec 13, 18 , Honeywell International Inc.
2018/0356,098 FUEL MANIFOLD Jun 13, 17 Dec 13, 18 , Not available
2018/0355,737 STATOR ASSEMBLY WITH RETENTION CLIP FOR GAS TURBINE ENGINE Jun 09, 17 Dec 13, 18 , Not available
2018/0355,796 FASTENER COVER FOR FLOWPATH FASTENERS Jun 12, 17 Dec 13, 18 , Not available
2018/0355,877 COMPRESSOR BLEED APPARATUS FOR A TURBINE ENGINE Jun 13, 17 Dec 13, 18 , Not available
2018/0355,759 GEARED GAS TURBINE ENGINE WITH OIL DEAERATOR AND AIR REMOVAL Aug 22, 18 Dec 13, 18 , Not available
2018/0355,749 DISTRIBUTED FAN LUBRICATION SYSTEM Dec 21, 16 Dec 13, 18 , Not available
2018/0355,803 GEARED GAS TURBINE ENGINE WITH REDUCED OIL TANK SIZE Aug 20, 18 Dec 13, 18 , Not available
2018/0354,634 A TURBINE ENGINE PROPELLED AIRPLANE HAVING AN ACOUSTIC BAFFLE Nov 21, 16 Dec 13, 18 , SAFRAN AIRCRAFT ENGINES
2018/0354,639 VARIABLE AND ADAPTABLE DIVERTERLESS BUMP INLET May 30, 18 Dec 13, 18 , Not available
2018/0354,635 PROPULSION SYSTEM FOR AN AIRCRAFT Jun 09, 17 Dec 13, 18 , Not available
2018/0355,793 HYBRID COMBUSTOR ASSEMBLY AND METHOD OF OPERATION Jun 09, 17 Dec 13, 18 , Not available
2018/0355,887 CENTRIFUGAL COMPRESSOR COOLING Dec 11, 17 Dec 13, 18 , Not available
2018/0355,758 TURBOCHARGER, NOTABLY FOR A COMBUSTION ENGINE May 18, 18 Dec 13, 18 , Not available

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