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)
11/2000
11/07/2000US6141957 Flame detector for combustor
11/07/2000US6141955 Gas turbine generator with dual steam-injected turbines
11/07/2000US6141954 Premixing fuel injector with improved flame disgorgement capacity
11/02/2000WO2000065213A1 A thermodynamic apparatus
11/02/2000WO2000065201A1 High pressure turbine cooling of gas turbine engine
11/02/2000EP1048901A1 High temperature gas heater
11/02/2000EP1048862A2 Combined hydraulic system
11/02/2000EP1048842A2 Fuel control system and valve therefor
11/02/2000EP1048393A1 Method for identification and repair of indications in hardware
11/02/2000EP1047896A1 Direct control fuel valve for fuel flow injecting circuit
10/2000
10/31/2000US6141087 System and method for measuring engine rotor thrust using Fabry-Perot fiber sensor
10/31/2000US6139303 Fixture for disposing a laser blocking material in an airfoil
10/31/2000US6139263 Flow machine with rotor and stator
10/31/2000US6139261 Bushing assembly with removable wear sleeve
10/31/2000US6139259 Low noise permeable airfoil
10/31/2000US6139257 Shroud cooling assembly for gas turbine engine
10/31/2000US6139019 Seal assembly and rotary machine containing such seal
10/31/2000US6138950 Aircraft engine air intake system
10/31/2000US6138654 Piezoelectric ignition and sensing device
10/26/2000WO2000062936A1 Arrangement and method for purification of flowing gas
10/26/2000WO2000025067A8 Fuel air mixer for a radial dome in a gas turbine engine combustor
10/25/2000EP1046787A2 Turbine inner shell heating and cooling flow circuit
10/25/2000EP1046010A1 Fuel injection assembly for gas turbine engine combustor
10/25/2000CN1271404A Gas turbine power generation equipment and air humidifying apparatus
10/24/2000US6135712 Turbomachine with mutual braking of concentric shafts
10/24/2000US6135238 Extended reaction acoustic liner for jet engines and the like
10/24/2000US6135135 Force balanced proportional bypass valve
10/24/2000US6134880 Turbine engine with intercooler in bypass air passage
10/24/2000US6134878 Cooling arrangement for a gas turbine driven power system
10/24/2000US6134876 Gas turbine engine with exhaust expander and compressor
10/24/2000US6134875 Turbine aircraft engine starting system controller
10/24/2000US6134874 Integral inertial particle separator for radial inlet gas turbine engine
10/24/2000US6134873 Method of operating a combustion turbine power plant at full power at high ambient temperature or at low air density using supplemental compressed air
10/19/2000WO2000008326A3 Methods and apparatus for water injection in a turbine engine
10/19/2000DE19922012C1 Rotor unit machining takes measurements of the actual surfaces at the fused joint for the flash to be removed and a nominal surface structure is machined from stored data to give the required flow characteristics
10/18/2000EP1045219A1 Method for reducing frost formation on a heat exchanger
10/18/2000EP1045218A1 Method for improving the performance of a cryogenic heat exchanger under frosting conditions
10/18/2000EP1045156A2 Bushing assembly with removable wear sleeve
10/18/2000EP1045114A2 Cooling supply system for stage 3 bucket of a gas turbine
10/18/2000CN1270656A Gas and turbine installation and method for operating an installation of this type
10/17/2000US6132520 Removal of thermal barrier coatings
10/17/2000US6132173 Cooled platform for a gas turbine moving blade
10/17/2000US6132168 Balancing a pressure drop across ring seals in gas turbine engines
10/17/2000US6131914 Gas turbine engine bearing compartment seal
10/17/2000US6131855 Device for removing hot air for a jet engine air inlet cowl with a de-icing circuit
10/17/2000US6131449 Velocity adaptive control test system
10/12/2000WO2000060239A2 Load sharing valve and system for operating centrifugal pumps in parallel
10/12/2000WO2000060226A1 Brayton or brayton-rankine combined cycle with hot-gas recirculation and inverse mixing ejector
10/12/2000WO2000060225A1 Biomass combustion chamber for gas turbine
10/12/2000WO2000060219A1 Turbo-engine with an array of wall elements that can be cooled and method for cooling an array of wall elements
10/12/2000CA2369361A1 Biomass combustion chamber for gas turbine
10/11/2000EP1043480A2 Film cooling of hot walls
10/11/2000EP1042541A1 Method for producing abrasive tips for gas turbine blades
10/11/2000CN1269459A Heat-insulating screen for gas turbine
10/10/2000US6130405 Laser drilling holes in a cylindrical workpiece
10/10/2000US6129973 Microchannel laminated mass exchanger and method of making
10/10/2000US6129509 Particle traps for turbo-prop engine
10/10/2000US6129309 Aircraft engine apparatus with reduced inlet vortex
10/10/2000US6128896 Aircraft air conditioner energy recovery device
10/06/2000CA2267818A1 Brayton or brayton-rankine combined cycle with hot-gas recirculation and inverse mixing ejector
10/05/2000WO2000058608A1 Method for producing electrical energy in a gas turbine process
10/05/2000DE19915049A1 Hitzeschild für eine Gasturbine Heat shield for a gas turbine
10/05/2000DE19913681A1 Verfahren zur Erzeugung elektrischer Energie in einem Gasturbinenprozeß A method for generating electrical energy in a gas turbine process
10/04/2000EP1041290A2 Gas turbine starting method
10/04/2000EP1041250A2 Heat shield for a gas turbine
10/04/2000EP1040291A1 Noise attenuating device for butterfly valves
10/04/2000EP1040261A2 Nozzles for water injection in a turbine engine
10/04/2000EP1040254A1 A LOW NOx CONDITIONER SYSTEM AND PROCESS FOR A MICROTURBINE POWER GENERATING SYSTEM
10/04/2000EP1040253A1 Cooling arrangement for turbine rotor
10/03/2000US6126723 Microcomponent assembly for efficient contacting of fluid
10/03/2000US6126549 Coupling device
10/03/2000US6125625 Low NOx conditioner system for a microturbine power generating system
10/03/2000US6125624 Anti-coking fuel injector purging device
09/2000
09/28/2000WO2000057033A1 Covering element and arrangement with a covering element and a support structure
09/28/2000WO2000057029A1 Turbine blade
09/28/2000WO2000056602A1 Modular air intake duct for aircraft
09/28/2000DE19913269A1 Turbinenschaufel Turbine blade
09/28/2000CA2366357A1 Covering element and arrangement with a covering element and with a carrying structure
09/27/2000EP1039183A2 Seal assembly and rotary machine containing such seal
09/27/2000EP1039115A2 Gas turbine system
09/27/2000EP1039097A2 Transport of high viscosity fuel to a power generation plant
09/27/2000CN1056909C Axial-flow gas turbine
09/26/2000US6123751 Filter construction resistant to the passage of water soluble materials; and method
09/26/2000US6123273 Dual-fuel nozzle for inhibiting carbon deposition onto combustor surfaces in a gas turbine
09/26/2000US6123170 Noise reducing connection assembly for aircraft turbine housings
09/26/2000US6123112 Fluid line with integrated unpressurized return flow
09/26/2000US6122892 Ventilated honeycomb cell sandwich panel and ventilation process for such a panel
09/21/2000WO2000055485A2 Control of the inlet of an auxiliary power unit
09/21/2000WO2000055036A2 Tangentially directed acoustic jet controlling boundary layers
09/21/2000WO2000039442A3 Turbine engine control system providing electronic power turbine governor and temperature/torque limiting
09/20/2000EP1036988A2 Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
09/20/2000EP1036924A2 Gas turbine generator having reserve capacity controller
09/20/2000EP0647291B1 A gas compressor
09/20/2000CN1056667C Method of operation of gas turbine using additive feed
09/20/2000CN1056666C Device for cooling gas-turbine coolant in combined gas and steam turbine installation
09/19/2000US6120245 Cooling structure around L shaped vertical type gas turbine output shaft
09/19/2000US6120244 Structure and method for inserting inserts in stationary blade of gas turbine
09/19/2000US6119445 Method of and apparatus for augmenting power produced from gas turbines
09/14/2000WO2000053908A1 Gas turbine engine
09/14/2000WO2000053907A1 Method of operation of a gas turbine engine power plant and a gas turbine engine power plant