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)
12/2002
12/12/2002US20020184885 Device and process for controlling the pressure and delivery of a fuel feed to a servovalve unit
12/12/2002US20020184884 Rapid shutdown and ecology system
12/12/2002US20020184862 High-performance filter for intake air for gas turbine, and filter unit using such filter for intake air for gas turbine
12/12/2002DE10127196A1 Verfahren zur Brennstoffversorgung sowie Brennstoffversorgungssystem für ein mit zumindest einer Fluggasturbine versehenes Flugzeug A method for fuel supply and fuel supply system equipped with at least one aircraft gas turbine aircraft
12/12/2002DE10123874A1 Flight propulsion system with safety gearbox has electrical gearbox with first magnetic pole wheel on turbine stage, second on fixed parts of system and wheel with phase windings on fan
12/12/2002CA2390341A1 Method and apparatus for managing maintenance operations
12/11/2002EP1265037A1 Fixation of turbine ceramic matrix composite combustion chamber using dilution holes
12/11/2002EP1265036A1 Elastic mounting of a ceramic matrix composite combustion chamber inside a metallic casing
12/11/2002EP1265035A1 Double mounting of a ceramic matrix composite combustion chamber
12/11/2002EP1265033A1 Combustion chamber with a system for mounting the chamber end wall
12/11/2002EP1265032A1 Ceramic matrix composite material gas turbine combustion chamber
12/11/2002EP1265031A1 Fixing of metallic cowls on turbomachine combustion chamber liners made of CMC materials
12/11/2002EP1264975A2 Fuel system for an aircraft gas turbine
12/11/2002EP1264091A1 Method and arrangement for cleaning the intake air of a gas turbine
12/11/2002EP1263997A1 Casting systems and methods with auxiliary cooling onto a liquidus portion of a casting
12/11/2002CN1384794A Supersonic external-compression diffuser and method for designing same
12/11/2002CN1095805C Method for combined generation of synthesis gas and power
12/10/2002US6492789 Method and apparatus for controlling a high-speed AC permanent magnet synchronous motor coupled to an industrial turbo engine
12/10/2002US6492034 Heat shield
12/10/2002US6491495 Closed circuit blade-cooled turbine
12/10/2002US6491048 Manifold for use in cleaning combustion turbines
12/10/2002US6490899 Method and apparatus for peening tops of cooled blades
12/10/2002US6490791 Method for repairing cracks in a turbine blade root trailing edge
12/10/2002CA2349154C Rotary-turbine internal combustion engine
12/10/2002CA2284493C Combined cycle electric power generating plant
12/10/2002CA2232897C Gas turbine cooling moving blade
12/10/2002CA2118557C A cooled turbine nozzle assembly and a method of calculating the diameters of cooling holes for use in such an assembly
12/05/2002WO2002097332A1 Heat shield arrangement for a hot-gas conducting component, in particular for structural pieces of gas turbines and method for production of said arrangement
12/05/2002WO2002097252A1 Lng regasification process and system
12/05/2002WO2002097242A1 Device for cooling coolant in a gas turbine and gas and steam turbine with said device
12/05/2002US20020182362 Method for repairing a thermal barrier coating and repaiied coating formed thereby
12/05/2002US20020182062 Aircraft engine air filter and method
12/05/2002US20020182061 Air inlet and outlet silencer structures for turbine
12/05/2002US20020182059 Centripetal air-bleed system
12/05/2002US20020182058 Methods and apparatus for minimizing gas turbine engine thermal stress
12/05/2002US20020179773 Method and apparatus for aircraft inlet ice protection
12/05/2002US20020179731 Ultrasonically enhanced continuous flow fuel injection apparatus and method
12/05/2002US20020178735 Combustion system for a gas turbine engine with variable airflow pressure actuated premix injector
12/05/2002US20020178731 Gas turbine plant and process for limiting a critical process value
12/05/2002US20020178728 Methods for reducing heat load in combustor panels
12/05/2002US20020178727 Methods and apparatus for injecting fuel into gas turbine engines
12/05/2002US20020178726 Combustor for gas turbine engines with low air flow swirlers
12/05/2002US20020178725 Nested core gas turbine engine
12/04/2002EP1262666A2 Air inlet and outlet silencer structures for turbine
12/04/2002EP1262638A1 Device for cooling of the cooling fluid of a gas turbine and gas and steam turbine plant with such a device
12/04/2002EP1262636A2 Gas turbine engine exhaust frame for minimizing the thermal stress and method for assembling it
12/04/2002EP1262632A1 Turbine airfoil with separately formed tip and method for manufacture and repair thereof
12/04/2002EP1262630A1 Centripetal air bleed device
12/04/2002EP1141522A4 Low drag ducted ram air turbine generator and cooling system
12/04/2002EP0855022B1 Methods for the design, quality control, and management of fatigue-limited metal components
12/04/2002CN1382897A High thrust turbosupercharger rotor with ball bearing
12/04/2002CN1382837A Fin stripping system with feedback control of water treatment and acid reusing system
12/03/2002US6489582 Non-submersion electrodischarge machining using conditioned water as a medium
12/03/2002US6488017 Piezoelectric ignition device for increasing spark energy
12/03/2002US6487863 Method and apparatus for cooling high temperature components in a gas turbine
12/03/2002US6487862 Low cost jet engine
12/03/2002US6487861 Combustor for gas turbine engines with low air flow swirlers
12/03/2002US6487860 Turbine engine fuel supply system
12/03/2002US6487848 Gas turbine engine jet noise suppressor
12/03/2002US6487847 Gas turbine engine fuel control system
12/03/2002US6487843 Turbomachine and method for operating
11/2002
11/28/2002WO2002095929A1 Gas turbine generator
11/28/2002WO2002095768A1 A brayton cycle nuclear power plant and a method of starting the brayton cycle
11/28/2002WO2002095310A1 Method and installation for feeding an air separation plant with a gas turbine
11/28/2002WO2002095293A1 Burner apparatus for burning fuel and air
11/28/2002WO2002020134A3 Methods for filtering air for a gas turbine system
11/28/2002US20020174647 Fuel metering unit with two integrated outlet ports
11/28/2002DE10221418A1 Imprägnierter Kern auf Aluminiumoxidbasis und Verfahren zu seiner Herstellung Impregnated alumina-based core and process for its preparation
11/28/2002CA2440701A1 A brayton cycle nuclear power plant and a method of starting the brayton cycle
11/27/2002EP1260767A1 Heat shield assembly for a high temperature gas conveying component, in particular for structural components of gas turbines, as well as process for producing such an assembly
11/27/2002EP1260690A2 System and method for monitoring gas turbine engine starting systems
11/27/2002EP1260689A1 Fuel metering device with two integrated exit ports
11/27/2002EP1260673A2 Turbine cooling circuit
11/27/2002EP1260608A1 Method of depositing a MCrAIY bond coating
11/27/2002EP1260602A1 Process for producing a thermally insulating coating system on a metallic substrate
11/27/2002EP1260261A1 Turbine air filter media
11/27/2002EP1259348A1 Clean melt nucleated casting systems and methods with cooling of the casting
11/27/2002CN2522630Y Turbo supercharger lubricating-oil sealing apparatus
11/27/2002CN1381670A Combustion turbine with axial relative movel guide unit
11/26/2002US6487491 System and method of controlling clearance between turbine engine blades and case based on engine components thermal growth model
11/26/2002US6485655 Method and apparatus for retaining an internal coating during article repair
11/26/2002US6485262 Methods and apparatus for extending gas turbine engine airfoils useful life
11/26/2002US6485025 Metallic cellular structure
11/26/2002US6484510 Fuel divider and ecology system for a gas turbine engine
11/26/2002US6484508 Methods for operating gas turbine engines
11/26/2002US6484507 Method and apparatus for controlling liquid droplet size and quantity in a stream of gas
11/26/2002US6484505 Combustor liner cooling thimbles and related method
11/26/2002US6484490 Gas turbine system and method
11/26/2002CA2107429C Gas turbine engine cooling systems
11/23/2002CA2373591A1 A process for applying a heat shielding coating system on a metallic substrate
11/21/2002WO2002093506A1 Improved fluid metering device
11/21/2002WO2002080189A8 A nuclear power plant and a method of conditioning its power generation circuit
11/21/2002US20020173897 System and method for monitoring thermal state to normalize engine trending data
11/21/2002US20020172591 Turbine cooling circuit
11/21/2002US20020171007 Aircraft engine mounting
11/21/2002US20020170698 System for casting a metal article
11/21/2002US20020170294 Thermal turbomachine and process for igniting the thermal turbomachine
11/21/2002DE10123708A1 Scavenging method for fuel pipe in gas turbine plant with scavenging material, especially air mixed with liquid and/or gaseous water
11/21/2002DE10122695A1 Verfahren zur Kühlung einer Gasturbine und Gasturbinenanlage Method for cooling a gas turbine and gas turbine plant
11/20/2002EP1258681A2 Methods and apparatus for cooling gas turbine engine combustors