Patents
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)
07/2004
07/15/2004US20040134284 Combustion chamber dynamic pressure transducer tee probe holder and related method
07/15/2004US20040134199 Methods and apparatus for controlling engine clearance closures
07/15/2004US20040134196 Reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process using cooled air injection to the turbines
07/15/2004US20040134126 method and device for plasmacatalytic conversion of liquid hydrocarbons, such as engine fuels, into a synthesis gas by employing a pulse-periodic pseudocorona streamer microwave discharge in the presence of of air, and in certain cases, water
07/15/2004DE10361499A1 Dichtungseinrichtung für eine umlaufende Maschine Sealing device for a rotary machine
07/15/2004CA2448502A1 Methods and apparatus for controlling engine clearance closures
07/14/2004EP1437785A2 Cooled turbine integrated fuel cell hybrid power plant
07/14/2004EP1437483A1 Trailing edge cooling of a turbine airfoil
07/14/2004EP1437199A1 Manufacturing cell using tooling apparatus
07/14/2004EP1437194A2 Process of removing a ceramic coating deposit in a surface hole of a component
07/14/2004EP1436491A1 Method for conditioning a compressor airflow and device therefor
07/14/2004CN1512048A System and method for display real-time turbine correction output and heat comsunption rate
07/14/2004CN1512047A Fuel metering device with compensation regulator valve in turbine engine
07/14/2004CN1512046A 燃气轮机 Gas turbine
07/14/2004CN1512038A Mounting method and device for gas turbine jet nozzle
07/13/2004US6762512 Methods for starting a combustion turbine and combustion turbine generator configured to implement same methods
07/13/2004US6761807 Molded tooling for use in airfoil stripping processes
07/13/2004US6761538 Continual radial loading device for steam turbine reaction type buckets and related method
07/13/2004US6761245 Tubular acoustic attenuation piece for an aircraft jet engine air intake
07/13/2004US6761035 Thermally free fuel nozzle
07/13/2004US6761034 Structural cover for gas turbine engine bolted flanges
07/13/2004US6761031 Double wall combustor liner segment with enhanced cooling
07/13/2004CA2357492C Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system, and fuel nozzle wash system
07/08/2004WO2004057170A1 Gas turbine power plant
07/08/2004US20040133396 Appliance for reading identification connectors
07/08/2004US20040131877 Article having turbulation and method of providing turbulation on an article
07/08/2004US20040131138 Brayton cycle nuclear power plant and a method of starting the brayton cycle
07/08/2004US20040129241 System and method for generating and sustaining a corona electric discharge for igniting a combustible gaseous mixture
07/08/2004US20040129000 Valve for dynamic control of fuel flow rate in gas turbine power plant, power plant and components thereof employing such valve, and method of constructing such valve
07/08/2004US20040128978 Bearing journals
07/08/2004DE10259963A1 Wabendichtung Honeycomb seal
07/07/2004EP1435492A2 High temperature turbine nozzle and process for manufacturing
07/07/2004EP1435491A2 Improved high temperature splash plate
07/07/2004EP1435490A2 High temperature centerbody and process for manufacturing
07/07/2004EP1435489A2 High temperature combustor wall and process for manufacturing
07/07/2004EP1435475A2 Planet gear journal for an epicyclic gear system
07/07/2004EP1435433A2 Turbo recuperator device
07/07/2004EP1435431A1 SEALING STRUCTURE OF SPINDLE BOLT, AND GAS TURBINE
07/07/2004EP1435276A1 Modular metal working tooling apparatus
07/07/2004EP1062409B1 High efficiency low pollution hybrid brayton cycle combustor
07/07/2004CN1511242A Heat shield arrangement for hot-gas conducting component, in particular for structural pieces for gas turbines and method for production of said arrangement
07/07/2004CN1511220A Sole plate for turbine and power generating plant equipment
07/07/2004CN1510415A Method for selecting adhesive, product and system thereof
07/07/2004CN1510251A Closed cooled combustion chamber for turbomachine
07/07/2004CN1509840A Method and device for removing materials from bottom of gas turbine disc dovetail grooves
07/06/2004US6758985 Method of removing a ceramic coating
07/06/2004US6758651 Gas turbine
07/06/2004US6758477 Aspirating face seal with axially biasing one piece annular spring
07/06/2004US6758259 Method and arangement for producing casting moulds from metal
07/06/2004US6758044 Control system for positioning compressor inlet guide vanes
07/06/2004CA2273944C Electrical system for turbine/alternator on common shaft
07/01/2004WO2004055960A1 Gas turbine engine starter generator with multiple windings on each exciter stator pole
07/01/2004WO2004055352A1 A method of utilizing low temperature heat
07/01/2004WO2004055339A1 An improved mounting system for installing a starter-generator to an accessory housing on a gas turbine engine
07/01/2004WO2004055338A1 Fluid flow actuated flapper valve
07/01/2004US20040126486 Method of repairing a Ni-base alloy part
07/01/2004US20040126229 High temperature turbine nozzle for temperature reduction by optical reflection and process for manufacturing
07/01/2004US20040126225 Rotary machine sealing assembly
07/01/2004US20040124573 Modular metalworking tooling apparatus
07/01/2004US20040124308 Hybrid solid oxide fuel cell aircraft auxiliary power unit
07/01/2004US20040124273 Fuel nozzle assembly
07/01/2004US20040124231 Method for coating a substrate
07/01/2004US20040124229 Methods for replacing portions of turbine shroud supports
07/01/2004US20040123603 Electrical machine
07/01/2004US20040123602 Turbo recuperator device
07/01/2004US20040123599 High temperature centerbody for temperature reduction by optical reflection and process for manufacturing
07/01/2004US20040123598 High temperature combustor wall for temperature reduction by optical reflection and process for manufacturing
07/01/2004US20040123597 Secondary fuel nozzle with readily customizable pilot fuel flow rate
07/01/2004US20040123447 Manufacturing cell using tooling apparatus
07/01/2004US20040123445 Method of producing polygonal ring-shaped machine parts having complex cross-section
07/01/2004DE19858702B4 Verfahren zum Verbinden von Schaufelteilen einer Gasturbine, sowie Schaufel und Rotor für eine Gasturbine A method of joining blade parts of a gas turbine, as well as the blade and rotor for a gas turbine
06/2004
06/30/2004EP1433924A2 Gas turbine combustor
06/30/2004EP1433865A1 High-strength Ni-base superalloy and gas turbine blades
06/30/2004EP1433704A1 Low power nitrogen enriched air generation system
06/30/2004EP1433703A1 Auxiliary power unit passive cooling system
06/30/2004EP1433565A1 Methods for replacing portions of turbine shroud supports
06/30/2004EP1432894A1 Method for preparing clean intake air for gas turbine
06/30/2004EP1432893A1 Articulated heat recovery heat exchanger
06/30/2004EP1432888A1 Spring mounted recuperator
06/30/2004EP1432549A1 A method for manufacturing a stator or rotor component
06/30/2004EP1073828B1 Containment system for containing blade burst
06/30/2004CN2622405Y Filter
06/30/2004CN2622404Y Air inlet device for gas turbine
06/30/2004CN1509392A Combustion chamber in particulary of gas turbine
06/30/2004CN1508396A Structure for connecting or space sealing members with different thermal expansion coefficients
06/30/2004CN1508395A Method and mechanism for assembling variable blade of sealed gas turbine engine
06/30/2004CA2453634A1 Turbo recuperator device
06/29/2004US6755924 Heat treatment; dimensional stability
06/29/2004US6755280 Method for producing a panel comprising an adapted acoustically resistive layer and panel so obtained
06/24/2004WO2004053311A1 Hermetic motor and gas booster
06/24/2004US20040121207 Cooled turbine integrated fuel cell hybrid power plant
06/24/2004US20040120810 Methods and apparatus for assembling gas turbine nozzles
06/24/2004US20040120808 Shroud segment and assembly with surface recessed seal bridging adjacent members
06/24/2004US20040120806 Shroud segment and assembly with circumferential seal at a planar segment surface
06/24/2004US20040118363 Common radial plane motor cooling
06/24/2004US20040118341 Introducing a stream of air into the turbine's interior and a fog of the corrosion inhibitor into the stream of air entering the turbine so that the corrosion inhibitor is drawn into and through the interior of the turbine
06/24/2004US20040118128 Compact quick attach starter-generator installation
06/24/2004US20040118125 Turbine inlet air-cooling system and method
06/24/2004US20040118124 Flow control body
06/24/2004US20040118123 Combustion chamber with a closed cooling system for a turbine