Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
11/2003
11/18/2003US6647729 Combustion chamber provided with a system for fixing the chamber end wall
11/18/2003US6647708 Multi-spool by-pass turbofan engine
11/18/2003US6647707 Nested core gas turbine engine
11/18/2003CA2117240C Sealing structures for gas turbine engines
11/13/2003WO2003094265A1 A gas turbine engine and fuel cell stack combination
11/13/2003WO2003093666A1 Flow divider and purge air system for a gas turbine engine
11/13/2003WO2003042928A3 Fault management system for gas turbine engines
11/13/2003US20030209910 Methods for starting a combustion turbine and combustion turbine generator configured to implement same methods
11/13/2003US20030209589 Method of forming a channel on the surface of a metal substrate, and related articles
11/13/2003US20030209256 Jet wet suit cover system for gaspath cleaning
11/13/2003US20030209142 Device for removing carbon dioxide from exhaust gas
11/12/2003EP1361351A2 Method to extend the life of a gas turbine engine
11/12/2003EP1360439A1 A method and a device for supplying fuel to a combustion chamber
11/12/2003EP1360342A1 Method for plasma coating a turbine blade and coating device
11/12/2003EP1129224B1 Device and process for cooling metal components which were subjected to high temperatures
11/12/2003CN1455714A Welding superalloy articles
11/12/2003CN1455152A Multihole facing of combustor lining for gas turbine
11/11/2003US6645560 Oxidation resistant coatings for niobium-based silicide composites
11/11/2003US6645351 Method of making a protective coating forming a thermal barrier with a bonding underlayer on a superalloy substrate, and a part obtained thereby
11/11/2003US6644935 Method and apparatus for increasing the efficiency of a multi-stage compressor
11/11/2003US6644035 Gas turbine and gas turbine high temperature section cooling method
11/11/2003US6644034 Liner supporting structure for annular combuster
11/11/2003US6644033 Tip impingement turbine air starter for turbine engine
11/11/2003US6644031 Fuel injector with an optimized metering device
11/11/2003US6644030 Cooling systems and methods of cooling
11/11/2003US6644016 Process and device for collecting air, and engine associated therewith
11/11/2003US6644013 Gas turbine power generation equipment and air humidifying apparatus
11/11/2003US6644012 Gas turbine set
11/11/2003CA2357553C Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system, and fuel nozzle wash system
11/11/2003CA2357493C Gas turbine fuel system comprising fuel oil distribution control system, fuel oil purge system, purging air supply system, and fuel nozzle wash system
11/11/2003CA2287509C Rotating machine seal device
11/06/2003WO2003091557A1 Fuel premixing module for gas turbine engine combustor
11/06/2003WO2003090955A1 Method and apparatus for production of a cast component
11/06/2003WO2001045877A3 Multi-wall core and process
11/06/2003US20030207151 Rhenium-containing protective layer for protecting a component against corrosion and oxidation at high temperatures
11/06/2003US20030205043 Valve assembly for gas turbine engine
11/05/2003EP1359364A1 Sealing device for a pipe leading through an opening in a wall
11/05/2003EP1359308A1 Outlet silencer and heat recovery structures for gas turbine
11/05/2003EP1359299A1 Uniaxial gas turbine system
11/05/2003EP1359231A1 Nickel-based superalloy
11/05/2003EP1358958A1 A way to manufacture inserts for steam cooled hot gas path components
11/05/2003EP1358954A1 Shaped core for cast cooling passages and enhanced part definition
11/05/2003EP1358401A1 Bulkhead for dual fuel industrial and aeroengine gas turbines
11/05/2003CN1126868C Magnetic fluid accelerator and magnetic fluid jet engine with the same accelerator
11/04/2003US6642490 Compact millimeterwave system for De-icing and for preventing the formation of ice on the outer surfaces of shell structures exposed to meterological influences
11/04/2003US6641144 Supplemental seal for the chordal hinge seals in a gas turbine
11/04/2003US6640550 Gas turbo-group with cooling air system
11/04/2003US6640548 Apparatus and method for combusting low quality fuel
11/04/2003US6640544 Gas turbine combustor, gas turbine, and jet engine
10/2003
10/30/2003WO2003089771A1 Optimizing inlet air temperature for gas trubines using heat exchanging fluid comprising alkali metal formate
10/30/2003WO2003089770A1 Water injection for gas turbine inlet air
10/30/2003WO2003089679A1 Process of masking cooling holes of a gas turbine component
10/30/2003WO2002055754A3 Method and device for gas phase diffusion coating of metal components
10/30/2003WO2002014695A9 Method and system of pulsed or unsteady ejector
10/30/2003US20030201640 Sealing device for connection of a pipe in a hole
10/30/2003US20030201089 Shaped core for cast cooling passages and enhanced part definition
10/30/2003US20030201087 Way to manufacture inserts for steam cooled hot gas path components
10/30/2003US20030201033 Nitrided surface treated steels; hardness; for turbines
10/30/2003US20030200754 Flow divider & purge air system for a gas turbine engine
10/30/2003US20030200752 Multihole patch for combustor liner of a gas turbine engine
10/30/2003DE10202977C1 Drehlagerung mit einer Sollbruchstelle Rotary bearing with a predetermined breaking point
10/30/2003CA2452758A1 Optimizing inlet air temperature for gas turbines using heat exchanging fluid comprising alkali metal formate
10/29/2003EP1357279A2 Noise reducing attachment for a turbofan engine
10/29/2003EP1357201A1 Process to form a composition-gradient ceramic layer by electron-beam PVD
10/29/2003EP1356235A1 Burner unit and method for operation thereof
10/29/2003EP0928326B1 Use of DIMETHYL ETHER FUEL AND METHOD OF GENERATING POWER IN A DRY LOW NOx COMBUSTION SYSTEM
10/29/2003CN1452711A Thermal shielding brick for lining combustion chamber wall, combustion chamber and gas turbine
10/29/2003CN1452689A Method and arrangement for cleaning intake air of gas turbine
10/29/2003CN1451847A Air and steam cooling platform of turbine vane
10/29/2003CN1451846A Turbine vane and casting assemble for mfg. same
10/28/2003US6639328 Microturbine/capacitor power distribution system
10/28/2003US6638008 Gas turbine engine blade containment assembly
10/28/2003US6637752 Supplemental seal for the chordal hinge seal in a gas turbine
10/28/2003US6637751 Supplemental seal for the chordal hinge seals in a gas turbine
10/28/2003US6637720 Component for holding down measuring leads
10/28/2003US6637643 Attaching a foil which comprises the bond coating to the substrate surface, and then fusing the foil to the substrate surface, so that the bond coating adheres to the substrate.
10/28/2003US6637208 Gas turbine in-line front frame strut
10/28/2003US6637187 Rotary inlet flow controller for pulse detonation combustion engines
10/28/2003US6637185 Gas turbine installation
10/23/2003WO2003087559A1 Combustor of gas turbine
10/23/2003WO2003087543A1 Steam and gas turbine installation
10/23/2003WO2003087439A1 Method for producing for producing mono-crystalline structures
10/23/2003US20030196548 High particle separation efficiency system
10/23/2003US20030196439 Gas turbine, combined cycle plant and compressor
10/23/2003CA2482102A1 Steam and gas turbine installation
10/22/2003EP1355040A2 Turbine blade platform with steam as well as air cooling
10/22/2003EP1354977A2 Method for repairing turbine engine components
10/22/2003EP1354074A2 Method of removing ceramic coatings
10/22/2003EP1101024B1 Gerotor compressor and gerotor expander
10/22/2003EP0926313B1 Structure and method for holding inserts for stationary blades of gas turbine
10/22/2003CN1450253A Rotor insert assembly and method of retrofitting
10/21/2003US6634596 Aircraft system architecture
10/21/2003US6634595 Method and apparatus for controlling aircraft inlet air flow
10/21/2003US6634457 Apparatus for damping acoustic vibrations in a combustor
10/21/2003US6634176 Turbine with exhaust vortex disrupter and annular recuperator
10/21/2003US6634165 Control system for gas turbine inlet-air water-saturation and supersaturation system
10/16/2003WO2003085243A1 Gas delivery system
10/16/2003WO2003085163A1 Component comprising a masking layer
10/16/2003WO2003085153A1 Thermal insulation layer system
10/16/2003WO2003067053A3 Air turbine starter with fluid flow control
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