| 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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| 08/11/2004 | EP1144141A4 Multipiece core assembly |
| 08/11/2004 | CN1519507A 燃烧室 Combustor |
| 08/11/2004 | CN1519466A Fuel injection appts. triggered flushing by differential pressure |
| 08/11/2004 | CN1519464A Gas turbine tail tube seal and gas turbine using same |
| 08/11/2004 | CN1519458A 涡轮叶片 Turbine blades |
| 08/11/2004 | CN1161540C Gas turbine having sequential combustion |
| 08/10/2004 | US6773229 Turbine nozzle having angel wing seal lands and associated welding method |
| 08/10/2004 | US6773228 Methods and apparatus for turbine nozzle locks |
| 08/10/2004 | US6773225 Gas turbine and method of bleeding gas therefrom |
| 08/10/2004 | US6772857 Acoustically resistive layer for an acoustical attenuation panel, panel using such a layer |
| 08/10/2004 | US6772596 Gas turbine installation |
| 08/10/2004 | US6772581 Gas turbine cooling passages for blade rings, combustor transition piece connecting portions and stationary blades |
| 08/10/2004 | CA2299815C Gas turbine split ring |
| 08/10/2004 | CA2227551C Control for cooling flow for high temperature cumbustion chamber |
| 08/05/2004 | WO2004065770A1 Control of a gas turbine with hot-air reactor |
| 08/05/2004 | WO2003098019A3 Fuel vaporization systems for vaporizing liquid fuel |
| 08/05/2004 | US20040151587 Microcircuit cooling for a turbine blade tip |
| 08/05/2004 | US20040151586 Turbine blade |
| 08/05/2004 | US20040148943 Gas turbine and bleeding method thereof |
| 08/05/2004 | US20040148938 Differential pressure induced purging fuel injectors |
| 08/05/2004 | US20040148937 Cooled purging fuel injectors |
| 08/05/2004 | US20040148922 Thermal and compressed air storage system |
| 08/05/2004 | DE10261869A1 Bearing for fast rotating shaft has runner which for forming of crowned running surface has radius continuously decreasing or increasing from both axial ends up to common apex |
| 08/05/2004 | DE102004002712A1 Fatigue life evaluation method for turbine blade, involves determining existence of turbine blade within fatigue-life limit, when creep elongation strain is less than specific percentage of initial length of blade |
| 08/05/2004 | CA2456628A1 Microcircuit cooling for a turbine blade tip |
| 08/04/2004 | EP1443275A1 Combustion chamber |
| 08/04/2004 | EP1443274A2 Methods for replacing a portion of a combustor dome assembly |
| 08/04/2004 | EP1443190A1 Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner |
| 08/04/2004 | EP1443178A2 Turbine blade |
| 08/04/2004 | EP1442829A2 Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
| 08/04/2004 | EP1442817A2 Apparatus and method for rejuvenating cooling passages within a turbine airfoil |
| 08/04/2004 | EP1442203A1 Method for controlling the cooling air mass flows of a gas turbine group |
| 08/04/2004 | EP1441874A1 Method for removing coating material from a cooling hole of a gas turbine engine component |
| 08/04/2004 | EP1343950B1 System to feed cooling air into a gas turbine rotor |
| 08/04/2004 | CN1517691A Estimating method for fatigue life of turbine blade, turbine blade creep elongation strain measurement device and turbine blade |
| 08/04/2004 | CN1517533A Method and device of heat exchanging |
| 08/04/2004 | CN1517513A Turbo-blade and gas turbine |
| 08/04/2004 | CN1160509C Sealing device for axial flow turbine |
| 08/03/2004 | US6769870 Structure for separating the high and low pressure turboexpanders of a gas turbine |
| 08/03/2004 | US6769868 Stator vane actuator in gas turbine engine |
| 08/03/2004 | US6769867 Joint structure of coolant passage, tube seal, and gas turbine |
| 08/03/2004 | US6769266 Heat and electric power supply system and operation method thereof |
| 08/03/2004 | US6769259 Gas turbine having a cooling air system and a spray air system |
| 08/03/2004 | US6769258 System for staged chilling of inlet air for gas turbines |
| 08/03/2004 | US6769257 Transition piece outlet structure enabling to reduce the temperature, and a transition piece, a combustor and a gas turbine providing the above output structure |
| 07/30/2004 | CA2456403A1 An active cooling panel of thermostructural composite material and method for its manufacture |
| 07/29/2004 | WO2004063560A1 System and method for generating and sustaining a corona electric discharge for igniting a combustible gaseous mixture |
| 07/29/2004 | US20040148129 Method and system for diagnosing state of gas turbine |
| 07/29/2004 | US20040146741 Thermal barrier coating |
| 07/29/2004 | US20040146657 Using three plasma torches ; concurrent spraying, heating |
| 07/29/2004 | US20040146402 Turbine moving blade and gas turbine |
| 07/29/2004 | US20040146399 Coolable segment for a turbomachinery and combustion turbine |
| 07/29/2004 | US20040144113 Heat extraction system for cooling power transformer |
| 07/29/2004 | US20040144099 Coleman regenerative engine with exhaust gas water extraction |
| 07/29/2004 | US20040144098 Multi-stage multi-plane combustion method for a gas turbine engine |
| 07/29/2004 | US20040144097 Apparatus and methods for reducing foreign object debris ingestion into aircraft engines |
| 07/29/2004 | US20040144078 Sole plate for turbine and power generating plant equipment |
| 07/29/2004 | US20040144077 Air intake and method for breathing air using an air intake |
| 07/29/2004 | US20040143967 Methods for replacing a portion of a combustor dome assembly |
| 07/29/2004 | DE10358431A1 Temperaturabtaststruktur, Verfahren zu ihrer Herstellung, Gasturbinen-Triebwerk und Temperatursteuerverfahren Temperaturabtaststruktur, to processes for their preparation, to gas turbine engine and temperature control method |
| 07/29/2004 | DE10353005A1 Verfahren und Einrichtung zum Steuern Triebwerks-Spielraumverschlüssen Method and apparatus for controlling engine compartment latches game |
| 07/28/2004 | EP1441408A1 Hybrid solid oxide fuel cell aircraft auxiliary power unit |
| 07/28/2004 | EP1441116A1 Air intake and method for breathing air using an air intake |
| 07/28/2004 | EP1441110A2 Combined cycle power plant and cooling steam supply method for gas turbine therein |
| 07/28/2004 | EP1440223A1 Gas turbine group |
| 07/28/2004 | EP1440004A1 Passive cooling system for auxiliary power unit installation |
| 07/28/2004 | EP1115967A4 Fan noise reduction from turbofan engines using adaptive herschel-quincke tubes |
| 07/28/2004 | EP1084372B1 Film cooling strip for gas turbine engine combustion chamber |
| 07/28/2004 | EP0911489B1 Gas turbine cooling stationary blade |
| 07/28/2004 | CN1516994A Method for plasma-catalytic conversion of fuels that can be used in internal combustion engine or gas turbine into synthetic gas and plasma-catalytic converter used for same |
| 07/28/2004 | CN1516756A Method for producing mono-crystalline structures |
| 07/28/2004 | CN1515811A Sealed assembly of rotary machine |
| 07/27/2004 | US6768278 Gas turbine engine starter generator with switchable exciter stator windings |
| 07/27/2004 | US6767659 Ceramic matrix composite component of a gas turbine engine such as a combustion liner adapted for backside radiative cooling |
| 07/27/2004 | US6767649 Crack-free welded joint to join two rotor sections; layers joined by powder metallurgy |
| 07/27/2004 | US6767182 Device for controlling the cooling flows of gas turbines |
| 07/27/2004 | US6766647 Method for ignition and start up of a turbogenerator |
| 07/27/2004 | US6766639 Acoustic-structural LPC splitter |
| 07/27/2004 | US6766636 Gas turbine intake air filter unit |
| 07/22/2004 | WO2004061340A1 Honeycomb seal |
| 07/22/2004 | US20040142112 superalloy parts exposed to high temperatures and frequent thermal cycles |
| 07/22/2004 | US20040141838 Turbine stage one shroud configuration and method for service enhancement |
| 07/22/2004 | US20040141836 Self-actuated bearing cooling flow shut-off valve |
| 07/22/2004 | US20040141835 Dust collecting filter, dust collecting device, and intake device of gas turbine |
| 07/22/2004 | US20040140079 Device and method for casting a workpiece, and workpiece |
| 07/22/2004 | US20040139750 Air assist fuel nozzle |
| 07/22/2004 | US20040139746 Gas turbine tail tube seal and gas turbine using the same |
| 07/22/2004 | US20040139722 Methods and apparatus for exchanging heat |
| 07/22/2004 | CA2509573A1 Honeycomb seals and methods of manufacturing same |
| 07/21/2004 | EP1438486A1 Device for filtering particles out of a coolant flow in a turbo machine |
| 07/21/2004 | CN1514507A Mixed type power generating equipment of cooling type turbine integrated fuel battery |
| 07/21/2004 | CN1514168A Flow quiding body |
| 07/20/2004 | US6764276 Guide vane assembly |
| 07/20/2004 | US6764081 Supplemental seal for the chordal hinge seals in a gas turbine and methods of installation |
| 07/20/2004 | US6764043 Rotatable scarf inlet for an aircraft engine and method of using the same |
| 07/20/2004 | US6763664 Fuel ratio control method and device in a gas turbine combustor |
| 07/20/2004 | US6763662 Installation for the generation of energy |
| 07/20/2004 | US6763651 Active system for wide area suppression of engine vortex |
| 07/15/2004 | US20040136824 Trailing edge cooling |
| 07/15/2004 | US20040134897 Process of removing a ceramic coating deposit in a surface hole of a component |