| 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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| 01/17/1996 | EP0691881A1 Pulse combusted acoustic agglomeration process |
| 01/17/1996 | EP0605546B1 Method and apparatus to install and remove heavy components |
| 01/16/1996 | US5484261 System for regulating air supply conditions of a turbo shaft machine |
| 01/16/1996 | US5483791 In a gas turbine engine |
| 01/10/1996 | CN1114732A Method for cooling self-burning combustion chamber |
| 01/09/1996 | US5482429 Fan blade containment assembly |
| 01/09/1996 | US5481866 Single stage premixed constant fuel/air ratio combustor |
| 01/04/1996 | WO1996000364A1 Pilot injector for gas turbine engines |
| 01/04/1996 | WO1996000345A1 Pressure vessel fuel nozzle support for an industrial gas turbine engine |
| 01/03/1996 | EP0515613B1 Diaphragm seal plate |
| 01/03/1996 | CN2216595Y Air rotary starter |
| 01/02/1996 | US5481145 Power recovery plant |
| 01/02/1996 | US5480232 Oil seal for gas turbine |
| 01/02/1996 | US5480110 Transport plane with stub tail |
| 01/02/1996 | US5479818 Process for detecting fouling of an axial compressor |
| 01/02/1996 | US5479773 Tangential air entry fuel nozzle |
| 01/02/1996 | US5479772 For a combustor of a gas turbine engine |
| 12/28/1995 | CA2152550A1 Oxidation resistant cobalt-based alloy |
| 12/27/1995 | EP0689007A1 Cooling the take-off injector in a combustion chamber with two burner heads |
| 12/27/1995 | EP0689006A1 Method and device for supplying fuel and for cooling the take-off injector in a combustion chamber with two burner heads |
| 12/26/1995 | US5478199 Active low noise fan assembly |
| 12/26/1995 | US5477672 High-temperature, high-pressure gas generation apparatus for turbine drive |
| 12/26/1995 | US5477671 For mixing air and fuel for delivery for a gas turbine engine module |
| 12/21/1995 | WO1995034751A1 Redundant engine starting system |
| 12/21/1995 | DE4420973A1 Axial gas turbine shaft seal for turbo engine |
| 12/20/1995 | EP0687864A2 A gas turbine engine combustion chamber |
| 12/13/1995 | EP0686231A1 New power process |
| 12/06/1995 | CN1112985A Cooling of hot unit of gas turbine |
| 12/05/1995 | US5471832 Combined cycle power plant |
| 12/05/1995 | US5471743 Method of disassembling a gas turbine engine power plant |
| 12/05/1995 | CA2084176C Gas turbine combustor |
| 11/30/1995 | DE4418680A1 Brennstoffversorgungseinrichtung für Turbo-Strahltriebwerke mit Nachbrenner The fuel supply device for turbo-jet engines with afterburner |
| 11/29/1995 | EP0684369A1 Steam cooling of gas turbine with backup air cooling |
| 11/29/1995 | EP0684367A1 Coal burner combined power plant having a fuel reformer |
| 11/29/1995 | EP0684364A1 Gas turbine rotor blade tip cooling device |
| 11/29/1995 | EP0684182A1 Flame-out resistant fuel pumping system |
| 11/29/1995 | CN1112645A Power apparatus |
| 11/28/1995 | US5470198 Sealing structures for gas turbine engines |
| 11/28/1995 | US5469706 Liquid fuel atomizing unit for miniature jet engine |
| 11/26/1995 | CA2150088A1 Method and apparatus for reducing noise generated by combustion |
| 11/23/1995 | WO1995031715A1 Method for measuring and extending the service life of fatigue-limited metal components |
| 11/23/1995 | WO1995031685A1 Rotary heat exchanger for gas turbine associated therewith |
| 11/23/1995 | WO1995031684A1 Rotary heat exchanger for gas turbine associated therewith |
| 11/23/1995 | WO1995031683A1 Rotary heat exchanger for gas turbine |
| 11/23/1995 | WO1995031632A1 Annular bearing compartment |
| 11/23/1995 | DE4432685C1 Starting cover for turbo=machine casing |
| 11/23/1995 | CA2190481A1 Rotary heat exchanger for gas turbine associated therewith |
| 11/23/1995 | CA2190480A1 Rotary heat exchanger for gas turbine associated therewith |
| 11/23/1995 | CA2190479A1 Rotary heat exchanger for gas turbine |
| 11/22/1995 | CA2148978A1 Gas turbine engine combustion chamber |
| 11/21/1995 | US5468123 System for ventilating the turbine disks and stator of a turbo jet engine |
| 11/21/1995 | US5467815 Apparatus for impingement cooling |
| 11/21/1995 | CA2056567C High energy ignition generator in particular for a gas turbine |
| 11/16/1995 | WO1995030822A1 Bearing support housing |
| 11/16/1995 | WO1995030779A1 Method for improving oxidation and spalling resistance of diffusion aluminide coatings |
| 11/15/1995 | EP0681647A1 Laser initiated non-linear fuel droplet ignition |
| 11/14/1995 | US5466198 Geared drive system for a bladed propulsor |
| 11/14/1995 | US5465570 Fuel control system for a staged combustor |
| 11/09/1995 | WO1995030115A1 Bulkhead and fuel nozzle guide assembly for an annular combustion chamber |
| 11/09/1995 | WO1995030077A1 Turbofan containment structure |
| 11/09/1995 | WO1995030076A1 Fan blade containment assembly |
| 11/09/1995 | WO1995030075A1 Variable thickness isogrid case |
| 11/09/1995 | WO1995030074A1 Aircraft fan containment structure restraint |
| 11/09/1995 | WO1995030073A1 Aircraft fan containment structure |
| 11/09/1995 | WO1995030072A1 Shroud segment having a cut-back retaining hook |
| 11/09/1995 | WO1995030071A1 Brush seal support and vane assembly windage cover |
| 11/09/1995 | WO1995030032A1 Effective cleaning method for turbine airfoils |
| 11/08/1995 | EP0681099A2 Gasturbine power station |
| 11/08/1995 | EP0172224B2 Steam-injected free-turbine-type gas turbine |
| 11/07/1995 | US5464322 Cooling circuit for turbine stator vane trailing edge |
| 11/07/1995 | US5463873 Method and apparatus for evaporative cooling of air leading to a gas turbine engine |
| 11/07/1995 | US5463865 Starter air valve position pressure transducer |
| 11/07/1995 | US5463863 To combustion equipment of a gas turbine engine |
| 11/02/1995 | WO1995029371A1 Sorption cooling of compressor inlet air |
| 11/02/1995 | WO1995029331A2 Stator vane arrangement for successive turbine stages |
| 11/02/1995 | EP0679800A2 Gaseous fuel compression and control system for gas turbine engine |
| 11/01/1995 | CN1110993A Gas turbine blade alloy |
| 10/31/1995 | US5462403 Compressor stator vane assembly |
| 10/31/1995 | US5461866 Gas turbine engine combustion liner float wall cooling arrangement |
| 10/31/1995 | US5461854 Combustor cooling for gas turbine engines |
| 10/31/1995 | CA2002121C Apparatus and method for providing ignition to a turbine engine |
| 10/29/1995 | CA2148060A1 Ducting for an external gas turbine topping combustor |
| 10/26/1995 | WO1995028243A1 Cooled gas turbine blade |
| 10/26/1995 | DE4414232A1 Vorrichtung zur Dämpfung von thermoakustischen Schwingungen in einer Brennkammer Device for damping thermoacoustic oscillations in a combustion chamber |
| 10/26/1995 | DE19518634A1 System for distributing aircraft fuel delivered by pump |
| 10/24/1995 | US5459994 Gas turbine-air separation plant combination |
| 10/19/1995 | WO1995027655A1 Integrated power and cooling environmental control system |
| 10/19/1995 | CA2185924A1 Integrated power and cooling environmental control system |
| 10/18/1995 | EP0677650A1 Fuel supply system for fuel injectors |
| 10/18/1995 | EP0677145A1 Separable fan strut for a gas turbofan powerplant. |
| 10/18/1995 | EP0578639B1 Turbine casing |
| 10/17/1995 | CA1337343C Staged turbo compressor with flanged and air cooled drive shaft |
| 10/15/1995 | CA2147019A1 Fuel injector and igniter assembly |
| 10/12/1995 | WO1995027126A1 Turbine shroud segment with serpentine cooling channels |
| 10/12/1995 | WO1995027087A1 Highly heat-resistant nickel-based alloy and its use |
| 10/12/1995 | DE4412314A1 Oil discharge pipe for axially=flowing gas turbine |
| 10/12/1995 | CA2186842A1 Highly heat-resistant nickel-based alloy and its use |
| 10/11/1995 | EP0489894B1 A composite structural component |
| 10/10/1995 | US5456578 Turbine housing of turbocharger |
| 10/10/1995 | US5456574 Centrifugal pump with starting stage |