| 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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| 09/21/2004 | CA2133185C Vertical gas turbine system |
| 09/16/2004 | WO2004079892A1 Electric start for a prime mover |
| 09/16/2004 | US20040181330 Method and apparatus for managing maintenance operations |
| 09/16/2004 | US20040179936 Tube-type vortex reducer with retaining ring |
| 09/16/2004 | US20040178640 Gas turbine generator |
| 09/16/2004 | US20040177901 High-strength ni-base superalloy and gas turbine blades |
| 09/16/2004 | US20040177619 Fluid injector and injection method |
| 09/16/2004 | US20040177618 Methods for operating gas turbine engines |
| 09/15/2004 | EP1457910A2 On-line system and method for processing information relating to the wear of turbine components |
| 09/15/2004 | EP1457855A1 Methods and apparatus for assessing gas turbine damage |
| 09/15/2004 | EP1457640A2 Tubular vortex streamer for gas turbine and their support ring |
| 09/15/2004 | EP1456510A1 Turbine noise absorber |
| 09/15/2004 | EP1456508A1 Hot gas path subassembly of a gas turbine |
| 09/15/2004 | EP1456507A1 Sealing module for components of a turbo-engine |
| 09/15/2004 | EP1456506A1 Gas turbine assembly |
| 09/15/2004 | EP1129273B1 Gas microturbine power generating system including a battery source for supplying startup power |
| 09/15/2004 | CN1529040A Combined circulation generator and steam supply method for cooling |
| 09/14/2004 | US6791204 Torque generation for salient-pole synchronous machine for start-up of a prime mover |
| 09/14/2004 | US6789616 Cylinder-type heat exchanger |
| 09/10/2004 | WO2004077400A2 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 09/09/2004 | US20040175597 Turbine components with thermal barrier coatings |
| 09/09/2004 | US20040175271 Airfoil shape for a turbine nozzle |
| 09/09/2004 | US20040175264 Method for cooling a turbo machine and turbo machine |
| 09/09/2004 | US20040172952 Coated crossfire tube assembly |
| 09/09/2004 | US20040172951 Method for operating a burner of a gas turbine and a power plant |
| 09/09/2004 | US20040172947 Turbine equipment and combined cycle power generation equipment and turbine operating method |
| 09/09/2004 | US20040172827 Fan and compressor blade dovetail restoration process |
| 09/09/2004 | US20040172826 Turbine element repair |
| 09/09/2004 | US20040172825 Turbine element repair |
| 09/08/2004 | EP1455067A2 Stall detection and recovery system for a gas turbine engine |
| 09/08/2004 | EP1455066A1 Cooling of a turbine and method therefore |
| 09/08/2004 | EP1455055A1 Turbomachine with cooled shroud segments |
| 09/08/2004 | EP1455053A2 Airfoil shape for a turbine nozzle |
| 09/08/2004 | EP1454707A1 Fan and compressor blade dovetail restoration process |
| 09/08/2004 | EP1454082A1 Zero twist carrier |
| 09/08/2004 | EP1454047A1 Gas turbine air starter gear assembly comprising a stationary roller shaft and method of manufacturing said roller shaft |
| 09/08/2004 | EP1454046A1 Method of starting a gas turbine engine |
| 09/08/2004 | EP1454045A1 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 09/08/2004 | EP1454044A1 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 09/08/2004 | CN1527922A Coolable segment for a turbomachinery and combustion turbine |
| 09/08/2004 | CN1526928A Method for cooling turbomachine and turbomachine for applicating the same method |
| 09/08/2004 | CN1526927A Cooled flushing fuel injector |
| 09/08/2004 | CN1526918A Gas-turbine engine turbon-nozzle arc section with single-branch open cavity hollow blade |
| 09/08/2004 | CN1526917A Method for providing turbulence structure on internal surface of middle hole of workpiece and relative workpiece |
| 09/08/2004 | CN1526510A Production and repairing method for wing surface of integrated blade rotor |
| 09/08/2004 | CN1165698C Sealing system, esp for sealing device of rotary machine |
| 09/07/2004 | US6787947 Cooling the upstream end plate of a high pressure turbine by means of a system of dual injectors at the end of the combustion chamber |
| 09/07/2004 | US6787740 Metal alloy hub section welded to a metal alloy airfoil, solution treating the hub at 1620-1655 degrees f to 1-4 hours, and oil quenching |
| 09/07/2004 | US6786694 Gas turbine and method of operating a gas turbine |
| 09/07/2004 | US6786635 Turbine blade (bucket) health monitoring and prognosis using neural network based diagnostic techniques in conjunction with pyrometer signals |
| 09/07/2004 | US6786488 Seal structure, turbine having the same, and leak-preventing seal system for rotating shaft |
| 09/07/2004 | US6786430 Liquid atomizing nozzle |
| 09/07/2004 | US6786052 Insulation system for a turbine and method |
| 09/07/2004 | US6786050 System and method for oil fuel burning integrated combined cycle power generation |
| 09/07/2004 | US6786049 Fuel supply control for a gas turbine including multiple solenoid valves |
| 09/07/2004 | US6786048 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
| 09/07/2004 | US6786040 Ejector based engines |
| 09/07/2004 | US6785961 Turbine nozzle segment and method of repairing same |
| 09/07/2004 | CA2300606C Gas turbine starting method |
| 09/07/2004 | CA2200253C Fuel supply system for decontaminating injected fuel |
| 09/07/2004 | CA2087761C High pressure turbine component interference fit up |
| 09/02/2004 | WO2004074654A1 Integral cooling system for rotary engine |
| 09/02/2004 | WO2004074653A1 Compact compound engine package |
| 09/02/2004 | WO2004074640A1 Sealing arrangement, particularly for the blade segments of gas turbines |
| 09/02/2004 | WO2004074638A1 Device for effecting heat transfer to rotating equipment, in particular gas turbines |
| 09/02/2004 | US20040172187 Methods and apparatus for assessing gas turbine engine damage |
| 09/02/2004 | US20040171330 Apparatus and method for consistently retaining a gas turbine engine blade in a predetermined position and orientation |
| 09/02/2004 | US20040170935 Power generator with low co2 emissions and associated method |
| 09/02/2004 | US20040170499 Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity |
| 09/02/2004 | US20040170498 Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 09/02/2004 | US20040170496 Turbine nozzle segment cantilevered mount |
| 09/02/2004 | US20040170494 Closed circuit blade-cooled turbine |
| 09/02/2004 | US20040169022 Method of closing working hole in gas turbine blade top |
| 09/02/2004 | US20040168786 Method of manufacturing gas turbine part using porous metal |
| 09/02/2004 | US20040168468 Intake of air into separation unit; extracting gas stream consisting of air gas, in particular oxygen or nitrogen; directing towards combustion chamber; controlling a parameter by acting on a compressor; assigning a variable set point value |
| 09/02/2004 | US20040168443 Methods and apparatus for assembling gas turbine engines |
| 09/02/2004 | US20040168427 Methods and apparatus for operating gas turbine engines |
| 09/02/2004 | DE10307552A1 Mounting for connecting inner and outer casings of gas turbine consists of radial rings forming bayonet fittings with annular U-shaped fittings on casings which allow them to tip |
| 09/02/2004 | DE10307374A1 Verfahren zum Betrieb eines teilgeschlossenen, aufgeladenen Gasturbinenkreislaufs sowie Gasturbinensystem zur Durchführung des Verfahrens Method for operating a partially closed, charged gas turbine cycle gas turbine system and for performing the method |
| 09/02/2004 | DE10306820A1 Anordnung zur Beeinflussung des Wärmeübergangs in rotierenden Einrichtungen, insbesondere in Gasturbinen Arrangement for influencing the heat transfer in rotating devices, in particular in gas turbines |
| 09/02/2004 | CA2516717A1 Integral cooling system for rotary engine |
| 09/02/2004 | CA2516470A1 System for affecting the heat transfer in rotating equipment, in gas turbines in particular |
| 09/01/2004 | EP1452802A1 Methods and apparatus for washing gas turbine engine combustors |
| 09/01/2004 | EP1452707A1 Protective device for the air intake of a jet engine |
| 09/01/2004 | EP1452695A1 Cooled turbine blade having reduced cooling air leakage |
| 09/01/2004 | EP1452693A2 Turbine nozzle segment cantilevered mount |
| 09/01/2004 | EP1452692A2 Turbine bucket damper pin |
| 09/01/2004 | EP1452691A1 Annular stator blade platform for low pressure turbine in a gas turbine engine |
| 09/01/2004 | EP1452690A2 Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 09/01/2004 | EP1452689A1 Gas turbine vane segment having a bifurcated cavity |
| 09/01/2004 | EP1452275A1 Apparatus and method for consistently retaining a gas turbine engine blade in predetermined position and orientation |
| 09/01/2004 | EP1452264A1 Method of manufacturing gas turbine part using porous metal |
| 09/01/2004 | EP1451459A1 High energy particle arrestor for air turbine starters |
| 09/01/2004 | EP1451458A1 Arrangement at gas turbine |
| 09/01/2004 | EP1451450A1 Gas turbo group |
| 09/01/2004 | EP1450984A1 A method for manufacturing a stator or rotor component |
| 09/01/2004 | EP1007832B1 Device for compressing a gaseous medium and systems comprising such device |
| 09/01/2004 | EP0928880B1 Tip shroud for moving blades of gas turbine |
| 09/01/2004 | EP0921278B1 Sealing structure for first stage stator blade of gas turbine |
| 09/01/2004 | EP0919700B1 Device for sealing gas turbine stator blades |