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)
07/2003
07/23/2003EP1329617A2 Fluid flow system for a gas turbine engine
07/23/2003EP1329615A2 Compressor stator bleed system
07/23/2003EP1329590A2 Coolant recirculation type gas turbine
07/23/2003EP1329527A2 High strength hot corrosion and oxidation resistant, directionally solidified nickel base superalloy and articles
07/23/2003EP1329382A2 Engine integrated auxiliary power unit
07/23/2003EP1040254B1 A LOW NOx CONDITIONER SYSTEM AND PROCESS FOR A MICROTURBINE POWER GENERATING SYSTEM
07/23/2003CN1115514C Flame disgorging two stream tangential entry nozzle
07/23/2003CN1115474C Method and device for reliable draining liquid fuel from gas turbine fuel system
07/22/2003US6596248 Rotating regenerative absorber, desorber
07/22/2003US6595749 Turbine airfoil and method for manufacture and repair thereof
07/22/2003US6595745 Supplemental seal for the chordal hinge seals in a gas turbine
07/22/2003US6595742 Aircraft engine air filter and method
07/22/2003US6595062 High temperature rake for suspersonic flow
07/17/2003WO2003058141A1 Evaporative cooler
07/17/2003WO2003058047A1 Method for operating a gas turbine group
07/17/2003US20030133796 Compressor stator inner diameter platform bleed system
07/17/2003US20030133793 Cloth seal for an inner compressor discharge case and methods of locating the seal in situ
07/17/2003US20030133786 Gas turbine and turbine rotor for a gas turbine
07/17/2003US20030132342 Method and apparatus for controlling aircraft inlet air flow
07/17/2003US20030131978 Cylinder-type heat exchanger
07/17/2003US20030131608 Turbine will exhaust vortex disrupter and annular recuperator
07/17/2003US20030131607 Tip impingement turbine air starter for turbine engine
07/17/2003US20030131606 Gas turbine engine power boost using micro droplet liquid injection
07/17/2003US20030131605 Adaptive acceleration schedules for gas turbine engine control systems
07/17/2003US20030131602 Turbine power plant having an axially loaded floating brush seal
07/17/2003US20030131601 Sliding steam temperature for combined cycle power plants
07/17/2003US20030131596 Exhaust-gas turbocharger for an internal combustion engine, and method for operating a turbocharged internal combustion engine
07/17/2003US20030131585 Separated core engine type turbofan engine
07/16/2003EP1327758A2 Air intake for an aircraft auxiliary power unit
07/16/2003EP1327748A1 Seal for gas turbine nozzle and shroud interface
07/16/2003EP1327108A1 Thermal shield stone for covering the wall of a combustion chamber, combustion chamber and a gas turbine
07/16/2003EP1327057A1 Device and method for preheating combustibles in combined gas and steam turbine installations
07/16/2003EP1327006A1 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
07/16/2003EP1326699A2 Methods for filtering air for a gas turbine system
07/16/2003EP1253986B1 Method and arrangement for producing casting moulds from metal
07/15/2003US6594533 System and method for performing electronic triage of a turbine part
07/15/2003CA2093712C Apparatus and methods for reducing fuel/air concentration oscillations in gas turbine combustors
07/10/2003WO2003056284A2 Vibration monitoring system for gas turbine engines
07/10/2003WO2003056162A1 Gas turbine engine with offset drive
07/10/2003WO2003056149A1 Turbine noise absorber
07/10/2003WO2003055672A1 Foam wall combustor construction
07/10/2003US20030129338 Integral surface features for cmc components and method therefor
07/10/2003US20030129061 Multi-component hybrid turbine blade
07/10/2003US20030126852 Steam cooled gas turbine system with regenerative heat exchange
07/09/2003EP1326008A1 Method and apparatus for assessing performance of combined cycle power-plants
07/09/2003EP1325276A1 Thermal shielding brick for lining a combustion chamber wall, combustion chamber and a gas turbine
07/09/2003EP0983421B1 Laser segmented thick thermal barrier coatings for turbine shrouds
07/09/2003CN1429316A Recuperator for use with turbine/turbo-alternator
07/08/2003US6589677 Thermal barrier additive which reduces the rate of weight loss and recession of the substrate comprises Ta oxide and an oxide selected from MgO, CaO, SrO, BaO, Al2O3, Y2O3, La2O3, Re2O3 (where Re is a rare earth element)
07/08/2003US6589600 Turbine engine component having enhanced heat transfer characteristics and method for forming same
07/08/2003US6589010 Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same
07/08/2003US6588709 Apparatus for variation of a wall skin
07/08/2003US6588212 Combustion turbine fuel inlet temperature management for maximum power outlet
07/08/2003US6588198 High pressure bypass sliding setpoint for steam-cooled advanced machine
07/08/2003US6588197 Steam control apparatus for turbine
07/08/2003US6588196 Gas and steam turbine system
07/08/2003CA2262050C Steam-cooling type gas turbine
07/03/2003WO2003054360A1 Hot gas path subassembly of a gas turbine
07/03/2003WO2003054359A1 Sealing module for components of a turbo-engine
07/03/2003WO2003054358A1 Gas turbine assembly
07/03/2003US20030125905 Method and apparatus for assessing performance of combined cycle power-plants
07/03/2003US20030124342 Oxidation resistant coatings for niobium-based silicide composites
07/03/2003US20030123982 Supplemental seal for the chordal hinge seal in a gas turbine
07/03/2003US20030123981 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030123980 Supplemental seal for the chordal hinge seal in a gas turbine
07/03/2003US20030123979 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030123978 Composite tubular woven seal for gas turbine nozzle and shroud interface
07/03/2003US20030123976 Methods and apparatus for assembling gas turbine engine struts
07/03/2003US20030122325 Seal for gas turbine nozzle and shroud interface
07/03/2003US20030122320 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030122316 Supplemental seal for the chordal hinge seal in a gas turbine
07/03/2003US20030122312 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030122311 Method of forming and installing a seal
07/03/2003US20030122310 Supplemental seal for the chordal hinge seals in a gas turbine
07/03/2003US20030122309 Supplemental seal for the chordal hinge seals in a gas turbine and methods of installation
07/03/2003US20030121269 Liquid fuel nozzle apparatus with passive protective purge
07/03/2003US20030121268 Combustion engine improvement
07/02/2003EP1323957A2 Composite tubular woven seal for gas turbine nozzle and shroud interface
07/02/2003EP1323910A2 Methods and apparatus for assembling gas turbine engine struts
07/02/2003EP1323901A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323900A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323899A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323898A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323897A2 Supplemental seal for the chordal hinge seals in a gas turbine
07/02/2003EP1323896A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323895A2 Supplemental seal for the chordal hinge seals in a gas turbine
07/02/2003EP1323894A2 Supplemental seal for the chordal hinge seals in a gas turbine
07/02/2003EP1323893A2 A method of forming and installing a seal into a turbomachine
07/02/2003EP1323892A2 Supplemental seal for the chordal hinge seals in a gas turbine and methods of installation
07/02/2003EP1323891A2 Supplemental seal for the chordal hinge seals in a gas turbine
07/02/2003EP1323890A2 Supplemental seal for the chordal hinge seal in a gas turbine
07/02/2003EP1323842A1 Method of restoration of mechanical properties of cast inconel 718 for serviced aircraft components
07/02/2003EP1323691A2 Silicon based substrate with environmental/thermal barrier layer
07/02/2003EP1323633A1 Air intake for turbo-prop engines
07/02/2003EP1322844A2 Assembly and method for fan noise reduction from turbofan engines using dynamically adaptive herschel-quincke tubes
07/02/2003CN1427949A Turbine engine foreign object damage detection system
07/02/2003CN1427922A Method and device for cooling inflow of shaft of steam turbine
07/02/2003CN1427140A Flexibly jointed double casing type bearing seat
07/02/2003CN1426864A Method and equipment for directional solidification casting
07/01/2003US6585483 Stationary roller shaft formed of a material having a low inclusion content and high hardness