| 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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| 03/03/1993 | EP0529900A1 Gas turbine apparatus and method of control thereof |
| 03/03/1993 | EP0529310A1 Topping combustor for an indirect fired gas turbine |
| 03/03/1993 | EP0368990B1 Reducing carbon buildup in a turbine engine |
| 03/03/1993 | EP0348500B1 Annular combustor with tangential cooling air injection |
| 03/03/1993 | CN1069561A Fuel delivery system for dual annular combustor |
| 03/02/1993 | US5190245 Turbojet engine exhaust casing with integral suspension lugs |
| 03/02/1993 | US5189874 Axial-flow gas turbine cooling arrangement |
| 03/01/1993 | CA2072417A1 Aircraft engine nacelle having circular arc profile |
| 03/01/1993 | CA2072386A1 Turbine blade impingement baffle |
| 02/24/1993 | EP0528297A1 Single vortex combustor arrangement |
| 02/24/1993 | EP0528138A1 Blade shroud for axial turbine |
| 02/24/1993 | EP0380632B1 Assuring reliable starting of turbine engines |
| 02/24/1993 | CN1069318A System and method for integration of combustor-tubine units and compressors |
| 02/24/1993 | CA2076563A1 Topping combustor for an indirect fired gas turbine |
| 02/23/1993 | US5188510 Method and apparatus for enhancing gas turbo machinery flow |
| 02/23/1993 | US5188507 Low-pressure turbine shroud |
| 02/23/1993 | US5187936 Continuous flow fuel circulation system |
| 02/23/1993 | US5187931 Combustor inner passage with forward bleed openings |
| 02/17/1993 | EP0527629A1 Fuel delivery system for dual annular combustor |
| 02/16/1993 | US5186006 Mounting for ceramic scroll |
| 02/16/1993 | US5185997 Gas turbine system |
| 02/13/1993 | CA2072275A1 Fuel delivery system for dual annular combustor |
| 02/09/1993 | US5184526 Automatic speed changing system for two-shaft type gas turbine engine |
| 02/09/1993 | US5184461 Method and apparatus for automatic bypass operation |
| 02/09/1993 | US5184458 Power unit fuel pressurization system |
| 02/09/1993 | US5184457 Valve assembly and method |
| 02/09/1993 | US5184456 Gas turbine motor drive |
| 02/09/1993 | CA2074326A1 Shroud ring for an axial flow turbine |
| 02/03/1993 | EP0526058A1 Turbine Nozzle Support |
| 02/02/1993 | US5183223 Load sharing support system |
| 02/02/1993 | US5182906 Hybrid spinner nose configuration in a gas turbine engine having a bypass duct |
| 02/02/1993 | US5182905 Method for automatic bypass operation |
| 02/02/1993 | US5182904 Gas turbine engine power unit |
| 01/26/1993 | US5181826 Attenuating shroud support |
| 01/26/1993 | US5181728 Trenched brush seal |
| 01/26/1993 | US5181376 Process and system for producing power |
| 01/26/1993 | US5181308 Method for installing annular seals |
| 01/23/1993 | CA2074284A1 Method for installing annular seals |
| 01/20/1993 | EP0523932A1 Compressor stall recovery method and apparatus |
| 01/20/1993 | EP0523899A1 Fluid bearing face seal for gas turbine engines |
| 01/19/1993 | US5180285 Protective coating |
| 01/19/1993 | US5180282 Gas turbine engine structural frame with multi-yoke attachment of struts to outer casing |
| 01/19/1993 | CA1312888C Seal assembly |
| 01/14/1993 | DE4121340A1 Isolierung von thermischen maschinen Isolation of thermal machines |
| 01/13/1993 | EP0522834A1 Heat shield mechanism for turbine engines |
| 01/13/1993 | EP0522833A1 Heat shield for a compressor stator structure |
| 01/13/1993 | EP0522832A1 Staged fuel delivery system with secondary distribution valve |
| 01/13/1993 | EP0522795A1 Heat shield |
| 01/12/1993 | US5177957 Propfan turbine engine |
| 01/12/1993 | US5177954 Gas turbine engine with cooled turbine blades |
| 01/12/1993 | US5177951 Method for management of heat generated by aircraft gas turbine installations |
| 01/10/1993 | CA2070521A1 Heat shield for a compressor/stator structure |
| 01/07/1993 | EP0521687A1 Combustor dome assembly |
| 01/07/1993 | EP0521325A1 Combustion chamber |
| 01/05/1993 | US5176814 Method of cooling with an endothermic fuel |
| 01/05/1993 | US5176495 Thermal shielding apparatus or radiositor for a gas turbine engine |
| 12/29/1992 | US5174714 Heat shield mechanism for turbine engines |
| 12/29/1992 | US5174584 Fluid bearing face seal for gas turbine engines |
| 12/29/1992 | US5174525 Structure for eliminating lift load bending in engine core of turbofan |
| 12/29/1992 | US5174524 Cooling system for high speed aircraft |
| 12/29/1992 | US5174110 Utility conduit enclosure for turbine engine |
| 12/29/1992 | US5174109 For an aircraft auxiliary power unit |
| 12/29/1992 | US5174106 For initiating combustion of a pyrotechnic charge |
| 12/26/1992 | WO1993000506A1 Thermal machine insulation |
| 12/23/1992 | EP0519823A1 Rear suspension structure for a turbine engine |
| 12/23/1992 | EP0519822A1 Suspension structure for a turbo engine exhaust casing |
| 12/23/1992 | EP0519304A1 Method and device to improve a gas turbine system |
| 12/22/1992 | US5172545 Apparatus for attaching a pre-atomization bowl to a gas turbine engine combustion chamber |
| 12/22/1992 | US5172543 Starting system for a gas turbine and method of starting a gas turbine |
| 12/16/1992 | EP0518594A1 Droop compensated bypass valve |
| 12/16/1992 | EP0518592A1 Vortex suppression for an eductor |
| 12/16/1992 | EP0518498A1 Thermal shield for axisymmetric vectoring nozzle |
| 12/14/1992 | CA2068110A1 Vortex suppression for an eductor |
| 12/10/1992 | DE4118284A1 Automotive gas turbine starter - delivers fuel in cone from coaxial nozzle inside trumpet shaped flame holder |
| 12/09/1992 | EP0517461A1 Aircraft gas turbine engine particle separator |
| 12/09/1992 | EP0516995A1 Combined gas-steam power plant |
| 12/08/1992 | US5169288 Low noise fan assembly |
| 12/08/1992 | US5169287 Shroud cooling assembly for gas turbine engine |
| 12/08/1992 | US5169159 For separating a high pressure fluid from a low pressure fluid |
| 12/08/1992 | US5168704 Gas turbine engine fuel and actuation pressure pumping system |
| 12/08/1992 | US5168699 Apparatus for ignition diagnosis in a combustion turbine |
| 12/08/1992 | US5168698 Fuel manifold system for gas turbine engines |
| 12/02/1992 | EP0516389A2 Apparatus for emovably attaching a core frame to a vane frame with a stable mid ring |
| 12/02/1992 | EP0516322A1 Shroud cooling assembly for gas turbine engine |
| 12/02/1992 | CA2069593A1 Combined gas/steam power station plant |
| 12/01/1992 | WO1992022053A1 Noise attenuation panel |
| 12/01/1992 | US5167487 Cooled shroud support |
| 12/01/1992 | US5167485 Self-cooling joint connection for abutting segments in a gas turbine engine |
| 12/01/1992 | US5167249 Inlet system for a missile |
| 12/01/1992 | US5167122 Fuel system for a turbo machine |
| 12/01/1992 | US5167117 Method and apparatus for cooling an airplane engine |
| 12/01/1992 | CA2095919A1 Noise attenuation panel |
| 12/01/1992 | CA1310877C Cleaning gas turbine compressors |
| 11/26/1992 | WO1992020971A1 Very high altitude turbine combustor |
| 11/26/1992 | WO1992020913A1 Plasma ignition apparatus and method for enhanced combustion and flameholding in engine combustion chambers |
| 11/25/1992 | EP0515130A1 Tapered metering channel for cooling of gas turbine shroud |
| 11/25/1992 | EP0515124A1 Method and apparatus for the production of a hot fluid stream for energy recovery |
| 11/24/1992 | US5165848 Vane liner with axially positioned heat shields |
| 11/24/1992 | US5165847 Tapered enlargement metering inlet channel for a shroud cooling assembly of gas turbine engines |
| 11/24/1992 | US5165606 Method for operating a pressure atomization nozzle |