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)
04/2000
04/13/2000WO2000020740A2 Gas turbine engine
04/13/2000WO2000020738A2 Gas turbine engine
04/13/2000WO2000020272A1 Aircraft engine air intake system
04/13/2000CA2345312A1 Gas turbine engine
04/13/2000CA2345293A1 Gas turbine engine
04/12/2000EP0992661A1 Ignition burner for a combustion chamber
04/12/2000EP0992310A2 Step milling process
04/12/2000CN1250504A Cooling supply manifold assembly for cooling combustion turbine components
04/12/2000CN1250487A Method of forming internal passages within articles and articles formed by same
04/11/2000US6047552 Heat-shield component with cooling-fluid return and heat-shield configuration for a component directing hot gas
04/11/2000US6047540 Small gas turbine engine having enhanced fuel economy
04/06/2000WO2000019124A1 Planetary gear
04/06/2000WO2000018972A1 Device and process for cooling metal components which were subjected to high temperatures
04/06/2000DE19941892A1 Turbinensystem und Energieerzeugungsverfahren Turbine system and power generation method
04/06/2000DE19845375A1 Indirect cooling process for flow in gap between turbine rotor and stator, involving use of water to cool stator part adjacent to gap
04/05/2000EP0990780A1 Gas turbine equipment
04/05/2000EP0990771A1 Trapped insert turbine airfoil
04/05/2000EP0990716A1 Thermal barrier coating
04/05/2000EP0990481A1 Co-machined bonded airfoil
04/04/2000US6045325 Apparatus for minimizing inlet airflow turbulence in a gas turbine engine
04/04/2000US6044640 Process and installation for cooling air
03/2000
03/30/2000WO2000017577A1 Dynamic control system and method for catalytic combustion process and gas turbine engine utilizing same
03/30/2000WO2000017533A1 Retaining arrangement for a bearing, in particular for a high pressure compressor shaft
03/30/2000WO2000017504A1 Fuel preheating in a gas turbine
03/30/2000WO2000017417A1 Method for processing the interior of a hollow part
03/30/2000WO2000017049A1 Multi-linkage suspension system including outboard isolators
03/29/2000EP0989287A2 Turbine seal and turbine assembly containing such spline seal
03/29/2000EP0988441A1 Combustion turbine cooling panel
03/29/2000EP0954688A4 Torch assembly
03/29/2000CN1249016A Coal fuel gas turbine system
03/29/2000CN1050893C Apparatus and methods for reducing fuel/air concentration oscillations in gas turbine combustors
03/28/2000US6042898 Cleaning oxides from a deposited m(ni,co,fe)craly bond coat on a superalloy substrate using an electric current; forming an adherent aluminum oxide scale and then a ceramic layer; blades, vanes of aircraft gas turbine engines
03/28/2000US6041588 Gas and steam turbine system and operating method
03/23/2000WO2000015383A1 Laser drilling holes in a cylindrical workpiece
03/22/2000EP0987457A1 Bearing retaining device in particular for a high pressure compressor shaft
03/22/2000EP0846220A4 Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers
03/21/2000US6039531 Gas turbine blade
03/21/2000US6038863 Burner arrangement for a gas turbine for preventing the ingress of fluids into a fuel passage
03/21/2000US6038851 Exhaust re-combustion type combined cycle power generation plant
03/21/2000US6038850 Combined cycle power plant
03/21/2000US6038849 Method of operating a combustion turbine power plant using supplemental compressed air
03/16/2000DE19932479A1 Gas turbine rotor cooling system uses cooled space outlets linked to flowed turbine space and arranged in blade flange parts in flowed nozzle area.
03/15/2000EP0985083A1 A method in or relating to the start of a power turbine and arrangement in power turbine in order to avoid start damage on turbine wheel/housing
03/15/2000EP0984839A1 Metal-ceramic graded-index material, product produced from said material, and method for producing the material
03/14/2000US6036440 Gas turbine cooled moving blade
03/14/2000US6036436 Gas turbine cooling stationary vane
03/14/2000US6035929 Apparatus for heating or cooling a circular housing
03/14/2000US6035645 Aerodynamic fuel injection system for a gas turbine engine
03/14/2000US6035644 Turbine control valve
03/14/2000US6035627 Turbine engine with cooled P3 air to impeller rear cavity
03/14/2000US6035626 Gas turbine starter assist torque control system
03/09/2000WO2000012939A1 Burner assembly
03/09/2000WO2000000772A3 DRY, LOW NOx CATALYTIC PILOT
03/09/2000WO1999061316A3 Biplanar scarfed nacelle inlet
03/08/2000EP0983421A1 Laser segmented thick thermal barrier coatings for turbine shrouds
03/08/2000EP0717813B1 Method of operating a gas turbine using an additive feed
03/07/2000US6033207 Flameless combustion and utilization of fuel gases
03/07/2000US6032959 Shingle damper brush seal
03/07/2000US6032459 Turbine exhaust cooling in a microturbine power generating system
03/07/2000US6032457 Fuel nozzle guide
03/07/2000US6032361 Gas turbine multi-hole film cooled combustor liner and method of manufacturing
03/02/2000DE19940763A1 Energy generator with integrated coal gasification operating in combined cycle
03/01/2000EP0982546A2 Combustor baffle
03/01/2000EP0982476A2 Apparatus for generating power
03/01/2000EP0981703A1 Brush-hair seal
03/01/2000EP0981681A1 Gas and steam turbine system, and refrigeration of the coolant intended for the gas turbine in such a system
03/01/2000EP0944767A4 Abradable seal
02/2000
02/29/2000US6029347 Method of manufacturing a turbine of thermostructural composite material, in particular of small diameter
02/24/2000WO2000009875A2 Nozzles for water injection in a turbine engine
02/24/2000WO2000009863A1 Mismatch proof variable stator vane
02/24/2000WO2000009862A1 Microturbine power generating system including variable-speed gas compressor
02/24/2000WO2000009778A1 Multilayer thermal barrier coating systems
02/24/2000CA2340431A1 Microturbine power generating system including variable-speed gas compressor
02/23/2000EP0980960A2 Bowed nozzle vane with selective thermal barrier coating
02/23/2000EP0958452A4 Ramjet engine for power generation
02/22/2000US6027305 Method and apparatus for reducing high-cycle fatigue and suppressing noise in rotating machinery
02/22/2000US6027304 High pressure inlet bleed heat system for the compressor of a turbine
02/17/2000WO2000008327A2 Control systems and methods for water injection in a turbine engine
02/17/2000WO2000008326A2 Methods and apparatus for water injection in a turbine engine
02/17/2000CA2336584A1 Control systems and methods for water injection in a turbine engine
02/17/2000CA2306487A1 Methods and apparatus for water injection in a turbine engine
02/16/2000EP0979962A2 Seal assembly and rotary machine containing such seal assembly
02/16/2000EP0979961A1 Seal apparatus for rotary machines
02/16/2000EP0979881A1 Thermal barrier and overlay coating systems comprising composite metal/metal oxide bond coating layers
02/15/2000CA2196764C Ultra-high efficiency turbine and fuel cell combination
02/10/2000WO2000006876A1 Quasi-isothermal brayton cycle engine
02/10/2000WO2000006380A1 Removal of thermal barrier coatings
02/09/2000EP0978635A1 Process for cooling the thermally stressed structures of a power plant
02/09/2000EP0977940A1 Air intake system for a gas turbine engine
02/09/2000CN1243913A Electric power generation by combined plant with one gas turbine and one steam turbine
02/08/2000US6023135 Turbogenerator/motor control system
02/08/2000US6023134 Power conversion system for bi-directional conversion between hydraulic power and electrical power
02/08/2000US6022197 Aircraft pump system with internal pressure control, comprising a regenerative pump and a centrifugal pump
02/03/2000WO2000005494A1 Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same
02/03/2000WO2000005489A1 Device and method for reducing the noise emissions of internal combustion engines and for diagnosing the same
02/03/2000WO2000005011A1 Ceramic shell mold provided with reinforcement, and related processes
02/03/2000DE19834376A1 Cooling system for gas turbine vanes passes the gas through an axial cyclone dust separator to give cleaned gas for cooling to prevent clogging
02/03/2000CA2338232A1 Apparatus and method for active reduction of the noise emission from je t engines and for their diagnosis
02/02/2000EP0976982A1 Method of operating the combustion chamber of a liquid-fuel gas turbine
02/02/2000EP0975862A1 Improved integrated environmental and secondary power system