| Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889) |
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| 04/01/1997 | US5615547 System for regulating oil and fuel temperatures of a turbojet engine |
| 03/26/1997 | EP0764767A2 Combined cycle power plant |
| 03/26/1997 | EP0764267A1 Method for measuring and extending the service life of fatigue-limited metal components |
| 03/25/1997 | US5613829 Gas turbine subassembly having a brush seal |
| 03/25/1997 | US5613356 Method of cooling thermally loaded components of a gas turbine group |
| 03/20/1997 | DE19533945A1 Internally cooled gas turbine component |
| 03/19/1997 | EP0763164A1 Turbofan containment structure |
| 03/19/1997 | EP0763163A1 Aircraft fan containment structure |
| 03/19/1997 | EP0712466B1 Centrifugal fuel pump with starting stage |
| 03/18/1997 | US5611214 Microcomponent sheet architecture |
| 03/18/1997 | US5611197 Closed-circuit air cooled turbine |
| 03/13/1997 | WO1997009578A2 Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers |
| 03/13/1997 | WO1997009524A1 Gas-turbine engine |
| 03/13/1997 | CA2230226A1 Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers |
| 03/12/1997 | EP0761977A1 High temperature composite material impellor, particularly of small diameter, and its manufacturing method |
| 03/12/1997 | EP0761947A1 Noise reduction kit for turbofan engine |
| 03/12/1997 | EP0761946A1 Staged fuel injection system with shuttle valve and fuel injector therefor |
| 03/12/1997 | EP0761945A1 Suspension device for a turboprop |
| 03/12/1997 | EP0761944A1 Method of operation for a gas turbine power plant |
| 03/12/1997 | EP0761943A1 Method of and apparatus for generating power |
| 03/12/1997 | CN1034237C Transportable electrical power generating system fueled by organic waste |
| 03/11/1997 | US5609779 Laser drilling of non-circular apertures |
| 03/11/1997 | US5609019 Apparatus for operating a gas turbine in a simple cycle and in a cycle combined with a steam turbine |
| 03/05/1997 | EP0760081A1 Rotary heat exchanger for gas turbine associated therewith |
| 03/05/1997 | EP0760080A1 Rotary heat exchanger for gas turbine associated therewith |
| 03/05/1997 | EP0760079A1 Rotary heat exchanger for gas turbine |
| 03/05/1997 | EP0760053A1 Annular bearing compartment |
| 03/05/1997 | EP0760052A1 Variable thickness isogrid case |
| 03/05/1997 | EP0708877B1 Method for repairing a combustion chamber assembly |
| 03/05/1997 | EP0616679B1 Cooling-air cooling unit for gas turbines |
| 03/05/1997 | CN1144301A Method of operating sequentially fired gas-turbine group |
| 03/04/1997 | US5606853 Gaseous fuel compression and control system for gas turbine engine |
| 03/01/1997 | CA2181963A1 Turbofan engine with reduced noise |
| 03/01/1997 | CA2181647A1 Method of operating a power station plant |
| 02/27/1997 | DE19633579A1 Process for starting combined cycle power plant |
| 02/26/1997 | EP0759098A1 Effective cleaning method for turbine airfoils |
| 02/26/1997 | EP0758932A1 Cooled gas turbine blade |
| 02/20/1997 | WO1997006361A1 A process and installation for cooling air |
| 02/20/1997 | CA2228634A1 A process and installation for cooling air |
| 02/19/1997 | EP0758406A1 A technique to prevent or divert cracks |
| 02/18/1997 | US5603604 Method and apparatus for enhancing gas turbo machinery flow |
| 02/18/1997 | US5603602 Pressurized ball bearing assemblies |
| 02/12/1997 | EP0758045A1 Starting process for a combined power plant |
| 02/12/1997 | EP0757775A1 Bulkhead and fuel nozzle guide assembly for an annular combustion chamber |
| 02/12/1997 | EP0757752A1 Aircraft fan containment structure restraint |
| 02/12/1997 | EP0757751A1 Shroud segment having a cut-back retaining hook |
| 02/12/1997 | EP0757750A1 Brush seal support and vane assembly windage cover |
| 02/05/1997 | EP0757164A1 Fuel supply for gas turbine with annular combustor |
| 02/05/1997 | EP0756667A1 Gas turbine airfoil clocking |
| 02/05/1997 | EP0667008B1 Partial engine and driveshaft failure detection monitor for a multi-engine aircraft |
| 02/04/1997 | US5598699 Laser initiated non-linear fuel droplet ignition apparatus |
| 02/04/1997 | US5598698 Fuel control system for a staged combustor |
| 02/04/1997 | US5598696 Clip attached heat shield |
| 01/30/1997 | WO1997003281A1 Preheating of gas turbine fuel with compressed cooling air |
| 01/30/1997 | WO1997002985A1 Turboprop engine with an air-oil cooler |
| 01/30/1997 | WO1997002984A1 Aircraft gas turbine engine with a liquid-air heat exchanger |
| 01/23/1997 | WO1997002421A1 Pumping device |
| 01/23/1997 | WO1997002408A1 Non-polluting, open brayton cycle automotive power unit |
| 01/22/1997 | EP0754142A1 Integrated power and cooling environmental control system |
| 01/22/1997 | EP0539580B1 Very high altitude turbine combustor |
| 01/21/1997 | US5595474 Pitch variation control device for the blades of a turbomachine rotor and method of operating the device |
| 01/21/1997 | US5595059 Combined cycle power plant with thermochemical recuperation and flue gas recirculation |
| 01/17/1997 | EP0764267A4 Method for measuring and extending the service life of fatigue-limited metal components |
| 01/16/1997 | WO1997001708A1 Gas turbine starter |
| 01/15/1997 | EP0753376A1 Method of repairing an abradable seal |
| 01/14/1997 | US5594665 Process and device for monitoring and for controlling of a compressor |
| 01/14/1997 | US5594216 Jet engine sound-insulation structure |
| 01/14/1997 | US5593274 Closed or open circuit cooling of turbine rotor components |
| 01/14/1997 | US5593165 Circumferential flow channel for carbon seal runner cooling |
| 01/09/1997 | DE19524733A1 Fluggasturbinen-Triebwerk mit einem Flüssigkeits-Luft-Wärmetauscher Aircraft gas turbine engine with a liquid-air heat exchanger |
| 01/09/1997 | DE19524731A1 Turboprop-Triebwerk mit einem Luft-Ölkühler Turboprop with an air-oil cooler |
| 01/08/1997 | EP0752056A1 Compressor stator vane assembly |
| 01/08/1997 | EP0752054A1 Bearing support housing |
| 01/08/1997 | EP0751849A1 Repair coating for superalloy articles, such as gas turbine engine components |
| 01/08/1997 | CN1139736A Method for controlling gas turbine burning heavy oil |
| 01/08/1997 | CN1139735A Fuel inlet pipe for gas turbine with circular combustion chamber |
| 01/07/1997 | US5591904 Apparatus for diminishing intake vortexes in jet engines |
| 01/07/1997 | US5590849 Active noise control using an array of plate radiators and acoustic resonators |
| 01/07/1997 | US5590531 Perforated wall for a gas turbine engine |
| 01/07/1997 | US5590518 Hydrogen-rich fuel, closed-loop cooled, and reheat enhanced gas turbine powerplants |
| 01/03/1997 | WO1997000381A1 Compressor stall and surge control using airflow asymmetry measurement |
| 01/02/1997 | EP0751282A2 Bypass air valve |
| 01/02/1997 | EP0751281A2 Bypass air valve |
| 01/02/1997 | EP0751280A1 Flow aligned plenum endwall treatment for compressor blades |
| 01/02/1997 | EP0701669B1 Geared drive system for a bladed propulsor |
| 01/02/1997 | DE19523935A1 Pumpvorrichtung Pumping device |
| 01/02/1997 | DE19523062A1 Combined-cycle power plant |
| 12/27/1996 | WO1996041992A1 Catalytic combustion chamber for a gas turbine |
| 12/25/1996 | CN1033660C Turbine geometry to reduce damage from hard particles |
| 12/24/1996 | US5586866 Baffle-cooled wall part |
| 12/24/1996 | US5586859 Flow aligned plenum endwall treatment for compressor blades |
| 12/24/1996 | US5586735 Two-dimensional supersonic and hypersonic air intake, with three movable ramps, for the combustion air of an aircraft engine |
| 12/24/1996 | US5586430 Balanced dual flow regenerator heat exchanger system and core driving system |
| 12/19/1996 | DE19521356A1 Gasturbine, umfassend einen Verdichterteil, einen Brennerteil und einen Turbinenteil Gas turbine comprising a compressor part, a burner part and a turbine part |
| 12/18/1996 | EP0748667A1 Removal of inserts from the interior of turbine airfoils |
| 12/18/1996 | EP0650554B1 Process for operating a gas turbine |
| 12/17/1996 | US5584173 Nozzle seal assembly with removable baseplate |
| 12/12/1996 | WO1996039578A1 Torch assembly |
| 12/12/1996 | CA2222604A1 Torch assembly |
| 12/11/1996 | EP0747573A1 Gas turbine rotor with remote support rings |