| 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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| 01/20/1994 | DE4223528A1 Verfahren zum Betreiben einer Gasturbine A method of operating a gas turbine |
| 01/20/1994 | DE4223495A1 Gas turbine with small blade clearance - consists of two=part pendulum housing with carrier plates and elastic membranes |
| 01/20/1994 | DE4223413A1 Intake system for super- and hypersonic aircraft - has articulated members, associated with swivel elements, actuated by toggle lever joints |
| 01/19/1994 | EP0578639A1 Turbine casing. |
| 01/18/1994 | US5279760 Blend of solvent and surfactant |
| 01/18/1994 | US5279111 Gas turbine cooling |
| 01/18/1994 | US5279109 Gas turbine engine variable bleed pivotal flow splitter |
| 01/12/1994 | EP0578461A1 Turbine nozzle support arrangement |
| 01/12/1994 | EP0578460A1 Turbine nozzle seal arrangement |
| 01/12/1994 | EP0460105B1 Bypass valve and visual indicator for a fuel system |
| 01/11/1994 | US5277023 For a combustor of a gas turbine engine |
| 01/11/1994 | US5277021 Very high altitude turbine combustor |
| 01/11/1994 | CA1325890C Gas turbine plant system and gas pressure stabilizer thereof in emergency |
| 01/05/1994 | EP0576859A1 Turbo machine with axial dry gas seal |
| 01/05/1994 | EP0401342B1 Segmented seal plate for a turbine engine |
| 01/05/1994 | DE4221805A1 Starting control for gas turbine engine - has electronic control for progressive start=up with intermediate speed and final operating speed |
| 01/05/1994 | DE4221804A1 Fuel supply control system for gas turbine engine - has two piston pumps with variable pulse length drive with opposing phase |
| 01/04/1994 | US5275534 Turbine disk forward seal assembly |
| 01/04/1994 | US5275529 Sandwich panel joint |
| 01/04/1994 | US5275000 Reducing thermal deposits in endothermic fuel reactors of propulsion systems |
| 01/04/1994 | US5274997 Gas turbine engine |
| 01/04/1994 | US5274996 Closed loop fuel control system |
| 01/04/1994 | US5274992 Integrated power unit combustion apparatus and method |
| 12/29/1993 | EP0576355A1 Changeover valve for a combi jet engine having two operational configurations |
| 12/29/1993 | EP0576316A1 Flexible sealing with cover jacket |
| 12/29/1993 | CN1080023A Turbulated cooling passages in gas turbine buckets |
| 12/29/1993 | CN1080022A Process for cleaning gas tubbine inlet air |
| 12/28/1993 | US5273249 Slide joint bracket |
| 12/28/1993 | US5272870 Cooling arrangement for jet engines |
| 12/28/1993 | US5272868 Gas turbine engine lubrication system |
| 12/22/1993 | EP0575302A1 Pneumatic turbine with particle separator |
| 12/22/1993 | EP0574754A1 Gas turbine using a pressure wave machine as energy exchanger |
| 12/22/1993 | EP0379525B1 Fabric expansion joints for exhaust systems of gas turbines |
| 12/21/1993 | US5271714 Turbine nozzle support arrangement |
| 12/21/1993 | US5271712 Turbine geometry to reduce damage from hard particles |
| 12/21/1993 | US5271218 Off-engine mounting system for steam and gaseous fuel manifolds of marine and industrial gas turbine engines |
| 12/21/1993 | US5271215 Natural gas stream turbine system operating with a semi-open cycle |
| 12/15/1993 | EP0539580A4 Very high altitude turbine combustor |
| 12/15/1993 | CN1023143C Valve device of power plant for burning a fuel at high pressure |
| 12/14/1993 | US5270081 Iron-base alloy structural component having a corrosion-inhibiting coating, and method of producing the coating |
| 12/14/1993 | US5269135 Gas turbine engine fan cooled heat exchanger |
| 12/14/1993 | US5269133 Heat exchanger for cooling a gas turbine |
| 12/09/1993 | WO1993024754A2 A gas compressor |
| 12/09/1993 | WO1993024735A1 Support casing with integrated bearing housing for a turbo-charger |
| 12/09/1993 | CA2136716A1 A gas compressor |
| 12/08/1993 | EP0572725A1 Sound attenuating liner |
| 12/08/1993 | EP0572402A1 An improved turbine cooling system. |
| 12/07/1993 | US5267608 Heat exchanger and reactor for aircraft and propulsion systems |
| 12/07/1993 | US5267433 Air turbine starter having a dual clutch |
| 12/07/1993 | CA1324999C Bodies with reduced surface drag |
| 12/01/1993 | EP0572312A1 Sealing arrangement between stator blade rows and a rotating rotor drum |
| 12/01/1993 | EP0572202A1 Apparatus and methods for reducing fuel/air concentration oscillations in gas turbine combustors |
| 12/01/1993 | EP0571791A1 Dry gas seal |
| 11/30/1993 | US5266360 Inhibiting coke formation by coating gas turbine elements with silica |
| 11/30/1993 | US5265409 Uniform cooling film replenishment thermal liner assembly |
| 11/30/1993 | US5265407 Oxidant blow down heater |
| 11/24/1993 | EP0571244A1 Sealing structure for a pivoting blade of a turbomachine |
| 11/23/1993 | US5264244 Inhibiting coke formation by coating gas turbine elements with alumina |
| 11/23/1993 | US5263315 Starting of a small turbojet |
| 11/23/1993 | US5263314 Fuel leakage protection system for gas turbine engine |
| 11/23/1993 | US5263312 Tube fitting for a gas turbine engine |
| 11/18/1993 | EP0570217A1 Intercooled gas turbine engine |
| 11/18/1993 | EP0493481B1 Integrated power unit control apparatus and method |
| 11/16/1993 | US5261608 Multi-line fluid supply manifold assembly |
| 11/16/1993 | US5261226 Topping combustor for an indirect fired gas turbine |
| 11/16/1993 | US5261222 For reducing temperature transients during start-up |
| 11/16/1993 | CA1324367C Fuel transfer system for aircraft |
| 11/11/1993 | WO1993022548A1 Exhaust vent for de-icing system of aircraft nacelle |
| 11/11/1993 | WO1993022547A1 Method for conversion of heat energy into mechanical energy in a gas-turbine engine, and gas-turbine engine |
| 11/10/1993 | EP0568748A1 Heat recovering thrust turbine having rotational flow path |
| 11/10/1993 | EP0568576A1 Noise attenuation panel |
| 11/10/1993 | EP0568573A1 Structural cellular component |
| 11/10/1993 | EP0568570A1 Noise attenuation panel |
| 11/09/1993 | US5259185 Fuel drainage connector system for aircraft gas turbine |
| 11/09/1993 | US5259183 Turbojet engine exhaust casing with integral suspension lugs |
| 11/03/1993 | EP0568226A1 Airfoil having multi-passage baffle |
| 11/02/1993 | US5257906 Exhaust system for a turbomachine |
| 11/02/1993 | US5257502 Fuel delivery system for dual annular combustor |
| 11/02/1993 | US5257500 Aircraft engine ignition system |
| 11/02/1993 | US5257498 Efficient anti-ice exhaust vent |
| 10/28/1993 | DE4213678A1 Turbine for exhaust turbocharger - uses compressed air as cooling medium for adjusting elements of guide blades |
| 10/27/1993 | EP0566868A1 Method of operating a gas turbine plant |
| 10/26/1993 | US5255849 Cooling air transfer apparatus for aircraft gas turbine engine exhaust nozzles |
| 10/26/1993 | US5255505 System for capturing heat transferred from compressed cooling air in a gas turbine |
| 10/25/1993 | CA2067064A1 Heat-recovering-thrust-turbine having rotational flow path |
| 10/22/1993 | CA2093185A1 Method of operating a gas turbine group |
| 10/19/1993 | US5253976 Integrated steam and air cooling for combined cycle gas turbines |
| 10/19/1993 | US5253875 Method for sealing a high pressure section of a gas turbine casing |
| 10/19/1993 | US5253472 Small gas turbine having enhanced fuel economy |
| 10/19/1993 | US5253471 Gas turbine engine combustor |
| 10/19/1993 | US5253470 Heat exchange with electric motor starter unit to increase temperature |
| 10/19/1993 | CA1323433C Engine monitoring apparatus |
| 10/14/1993 | WO1993020335A1 A method and a device in a rotating machine |
| 10/14/1993 | WO1993020334A1 Mounting of axial turbo-machinery |
| 10/13/1993 | CN1022433C Axisymmetric vectoring exhaust nozzle seal |
| 10/12/1993 | US5251691 Device for the indirect heating of air |
| 10/12/1993 | US5251435 For use in an aircraft turbofan engine |
| 10/12/1993 | US5251434 Pressurized fluidized-bed boiler power plant |
| 10/06/1993 | EP0564135A2 Gas turbine engine cooling system |
| 10/06/1993 | EP0563553A1 Air cooling of turbines in compressed air storage driven by gas turbine |