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)
06/2004
06/24/2004US20040118105 Normally open reverse flow flapper valve
06/24/2004US20040118102 Wide-angle concentric diffuser
06/24/2004US20040118101 Recuperator configuration
06/24/2004DE10348413A1 Verfahren zum Erzeugen einer Wirbelströmung auf der Innenseite von Löchern in einem Gegenstand und dazugehörige Gegenstände A method for generating a swirl flow on the inside of holes in an object and associated objects
06/23/2004EP1431663A2 Test model for a gas turbine combustor dome and method of fabricating
06/23/2004EP1431662A1 Turbine combustor with closed circuit cooling
06/23/2004EP1431661A1 Flow guiding body
06/23/2004EP1431521A2 Methods and apparatus for sealing gas turbine engine variable vane assemblies
06/23/2004EP1431518A2 Turbine engine shroud segment assembly with a surface-recessed seal bridging adjacent shroud segments
06/23/2004EP1431515A2 Turbine engine shroud segment and assembly with circumferential seal on a planar segment surface
06/23/2004EP1431513A2 Methods and apparatus for assembling gas turbine nozzles
06/23/2004EP1431421A1 Procees and compositions for removing aluminosilicate material from a substrate
06/23/2004EP1430593A1 System and method for providing ballast loading for a turbo-generator
06/23/2004EP1430244A1 Dual actuator air turbine starter valve
06/23/2004CN1507547A Burner apparatus for burning fuel and air
06/23/2004CN1507534A Method for cooling a gas turbing and gas turbing installation
06/23/2004CN1506617A Combustion chamber for firing one kind of combustable liquid mixed fuel
06/23/2004CN1506612A Fluid sprayer and spraying method
06/23/2004CN1506588A Method and apparatus for mounting bearing assembly
06/23/2004CN1506560A Combustion gas turbine
06/23/2004CN1154791C Thermodynamic apparatus
06/23/2004CN1154787C Combined circulation generating apparatus and steam supply method for its cooling use
06/23/2004CA2452990A1 Cooled turbine integrated fuel cell hybrid power plant
06/22/2004US6752592 Supplemental seal for the chordal hinge seals in a gas turbine
06/22/2004US6751961 Bulkhead panel for use in a combustion chamber of a gas turbine engine
06/22/2004US6751941 Foil bearing rotary flow compressor with control valve
06/22/2004US6751939 Flow divider and ecology valve
06/17/2004WO2004051062A1 Method for controlling the injection of liquid into an inflow channel of a prime mover or a machine-tool
06/17/2004WO2004051061A1 Separating device, method and turbine unit for the removal of foreign components from a medium flow
06/17/2004US20040117148 System and method for displaying real-time turbine corrected output and heat rate
06/17/2004US20040115469 Thermal barrier coating protected by alumina and method for preparing same
06/17/2004US20040115462 Article including a substrate with a metallic coating and a protective coating thereon, and its preparation and use in component restoration
06/17/2004US20040115395 Assembly containing a composite article and assembly method therefor
06/17/2004US20040115054 Blade for a turbine comprising a cooling air deflector
06/17/2004US20040115051 Methods and apparatus for sealing gas turbine engine variable vane assemblies
06/17/2004US20040115041 Methods and apparatus for assembling a bearing assembly
06/17/2004US20040115040 Torque tube bearing assembly
06/17/2004US20040114666 Temperature sensing structure, method of making the structure, gas turbine engine and method of controlling temperature
06/17/2004US20040113014 Rotatable scarf inlet for an aircraft engine and method of using the same
06/17/2004US20040112287 Method and device for gas phase diffusion coating of metal components
06/17/2004US20040112280 Method for producing monocrystalline structures
06/17/2004US20040112220 Low power nitrogen enriched air generation system
06/17/2004US20040112064 Gas turbine with device for extracting work from disk cooling air
06/17/2004US20040112041 Coated journals
06/17/2004US20040112039 Gas turbine combustor
06/17/2004US20040112038 Dual fuel type combined turbine plant and method for operating the same
06/17/2004US20040112037 Gas turbine power generator
06/16/2004EP1429043A2 Methods and apparatus for assembling a bearing assembly
06/16/2004EP1429005A2 Coated journals of a geartrain in a turbofan engine
06/16/2004EP1429001A2 Intake silencer for gas turbines
06/16/2004EP1428986A2 Torque tube bearing assembly
06/16/2004EP1428985A1 Gas turbine
06/16/2004EP1428984A2 Air-cooled gas turbine
06/16/2004EP1428983A1 Exhaust gas turbine casing
06/16/2004EP1428982A1 A method of depositing a local MCrAIY-coating
06/16/2004EP1428909A1 Thermal barrier coating protected by alumina and method for preparing same
06/16/2004EP1428903A2 Article including a substrate with a metallic coating and a protective coating thereon, and its preparation and use in component restoration
06/16/2004EP1428001A1 Methods and apparatus for model based shrouded bellows stiffness determinations
06/16/2004EP1427928A1 Method for gas turbine light-off
06/16/2004EP1427915A2 Turbine no-load speed limiter
06/16/2004EP1427507A1 Air filter system
06/16/2004EP1137866B1 Impeller containment system
06/16/2004CN1504638A Exhaust-gas-turbine casing
06/15/2004US6750557 Redundant prime mover system
06/15/2004US6749726 Lasers/fiber optics are used for fuel ignition; propulsion engines
06/15/2004US6749400 Gas turbine engine disk rim with axially cutback and circumferentially skewed cooling air slots
06/15/2004US6749396 Failsafe film cooled wall
06/10/2004US20040109786 Nickel-base superalloy composition and its use in single-crystal articles
06/10/2004US20040109767 Metallic article with integral end band under compression
06/10/2004US20040109764 Turbine, in particular a gas turbine, and a blade
06/10/2004US20040109758 Insulation system for a turbine and method
06/10/2004US20040109756 Gas turbine
06/10/2004US20040109755 Exhaust-gas-turbine casing
06/10/2004US20040108413 Mounting arrangement
06/10/2004US20040107703 Electric starter motor with integral clutch
06/10/2004US20040107691 Fuel system utilizing dual mixing pump
06/10/2004US20040107575 Methods for replacing a portion of a combustor liner
06/10/2004US20040107574 Methods for replacing combustor liners
06/09/2004EP1426687A1 Methods for replacing a portion of a combustor liner
06/09/2004EP1426685A2 Fuel system utilizing dual mixing pump
06/09/2004EP1426588A1 Separating device, method and turbine installation for removing foreign particles from the flow of a fluid
06/09/2004EP1426587A1 Soundproof aircraft engine nacelle
06/09/2004EP1426561A2 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion
06/09/2004EP1426558A2 Gas turbine transition piece with dimpled surface and cooling method for such a transition piece
06/09/2004EP1426555A2 Method and apparatus for reducing flow across compressor airfoil tips
06/09/2004EP1426457A2 Nickel-base superalloy composition and its use in single-crystal articles
06/09/2004EP1426141A1 Method and apparatus for removing a predetermined amount of material from a bottom portion of a dovetail slot in gas turbine engine disk
06/09/2004EP1426136A1 Methods for replacing combustor liners
06/09/2004EP1425502A1 Sealing method and device for a gas turbine shaft
06/09/2004DE10256418A1 Abgasturbinengehäuse Exhaust turbine housing
06/09/2004DE10256193A1 Verfahren zur Steuerung der Flüssigkeitseinspritzung in einen Zuströmkanal einer Kraft- oder Arbeitsmaschine Method for controlling the fluid injection into an inflow of power engine or machine
06/09/2004DE10254824A1 Ansaugschalldämpfer für Gasturbinen Intake silencers for gas turbines
06/09/2004CN1153005C Method and apparatus for electric power generation
06/09/2004CA2432608A1 Gas turbine
06/08/2004US6746783 High-temperature articles and method for making
06/08/2004US6746209 Methods and apparatus for cooling gas turbine engine nozzle assemblies
06/08/2004US6746208 Closed circuit blade-cooled turbine
06/08/2004US6746207 Turboprop aircraft engine
06/08/2004US6745622 Apparatus and method for inspecting dovetail slot width for gas turbine engine disk
06/08/2004US6745571 Method of combustor cycle airflow adjustment