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)
01/2004
01/29/2004US20040018303 Temperature control by a radiation reflectors that can be moved within the chamber to increase and decrease the amount of reflective heat; depositing a ceramic coatings on gas turbine engine for heat resistance
01/29/2004US20040018092 Methods and apparatus for manufacturing rotor shafts
01/29/2004US20040018081 Internal low pressure turbine case cooling
01/29/2004US20040016445 Contacting the surfaces to be cleaned with a cleaning formulation comprising selected from the group consisting of graphite particles and molybdenum-based particles
01/29/2004US20040016319 Furnishing a nonmetallic precursor compound comprising metallic constituent element; chemically reducing nonmetallic precursor compound to produce metallic particle; melting and solidifying metallic particle to produce article
01/29/2004US20040016245 Packaged chilling systems for building air conditioning and process cooling
01/28/2004EP1384871A1 Gas turbine power generation facility
01/28/2004EP1384858A2 Internal cooling of the case of a low pressure turbine
01/28/2004EP1384854A2 Methods and apparatus for manufacturing rotor shafts
01/28/2004EP1183442B1 Cast on-board injection nozzle with adjustable flow area
01/28/2004EP0911488B1 Gas turbine cooled stationary blade
01/28/2004CN1470747A Method and apparatus for operating gas turbine engine
01/28/2004CN1470746A Method and apparatus for turbine nozzle locking piece
01/28/2004CN1136444C Pressure tester
01/27/2004US6682307 Sealing system for a rotor of a turbo engine
01/27/2004US6682300 Seal element for sealing a gap and combustion turbine having a seal element
01/27/2004US6682015 Device for the attachment of an engine to an aircraft
01/27/2004US6681888 Silencing apparatus, notably for a turbo engine
01/27/2004US6681579 Air turbine starter with fluid flow control
01/27/2004US6681557 Low cost high efficiency automotive turbines
01/27/2004US6681556 Apparatus for decreasing combustor emissions
01/27/2004US6681486 Method of forming brush seals between rotating components
01/22/2004WO2004007927A2 Method for influencing and controlling the oxide layer on metallic components of a hot co2/h2o circulating system
01/22/2004WO2004007915A1 Rotor recentring after decoupling
01/22/2004WO2003066430A3 Aircraft fuel tank explosion prevention and smoke alarm response safety improvement method
01/22/2004US20040013516 System to feed cooling air into a gas turbine rotor
01/22/2004US20040012149 Seal structure, turbine having the same, and leak-preventing seal system for rotating shaft
01/22/2004US20040011713 Filter control method, and filter controlled by the method
01/22/2004US20040011443 Nickel base superalloys and turbine components fabricated therefrom
01/22/2004US20040011059 Combustion-chamber arrangement
01/22/2004US20040011053 Gas-turbine engine control system
01/22/2004US20040011052 Fuel delivery system
01/22/2004US20040011046 System for staged chilling of inlet air for gas turbines
01/22/2004US20040011045 Ramjet for a supersonic and hypersonic aircraft
01/22/2004US20040011044 Method for increasing heat transfer from combustors
01/22/2004US20040011021 Gas-turbine engine combustor
01/22/2004US20040011020 Gas turbine control apparatus and gas turbine system using the same
01/22/2004US20040011019 Device and method for preheating combustibles in combined gas and steam turbine installations
01/22/2004US20040011018 Assistance and emergency drive for electrically-driven accessories
01/22/2004DE10231879A1 Verfahren zur Beeinflussung und Kontrolle der Oxidschicht auf metallischen Bauteilen heisser CO2/H2O-Kreislaufsysteme A method for influencing and controlling the oxide layer on metallic components hot CO2 / H2O-loop systems
01/22/2004DE10226721A1 Verfahren und Vorrichtung zur Erwärmung eines einer Brennkammer zugeführten Gases Method and apparatus for heating a combustion chamber of a gas supplied
01/21/2004EP1382817A1 Assistance to the driving of accessories in a turbo-engine
01/21/2004EP1382802A1 Integrated start generator for a turbomachine
01/21/2004EP1382697A1 Superalloy for single crystal turbine vanes
01/21/2004EP1381812A1 Turbine premixing combustor
01/21/2004EP1381811A1 Combustion chamber, in particular of a gas turbine
01/21/2004EP1381481A2 Multi-wall core and process
01/21/2004CN1470152A Device for producing a plasma, ionisation method, use of said method and production processes using said device
01/20/2004US6679757 Shaping tool and method for shaping curved surfaces on workpieces
01/20/2004US6679679 Internal stator shroud
01/20/2004US6679062 Architecture for a combustion chamber made of ceramic matrix material
01/20/2004US6679059 Gas turbine plant
01/20/2004US6679047 Combined cycle gas turbine system
01/20/2004US6679045 Flexibly coupled dual shell bearing housing
01/15/2004WO2004005581A1 Highly oxidation resistant component
01/15/2004WO2004005580A1 Highly oxidation resistant component
01/15/2004WO2004004953A2 Diffusion bond mixture for healing single crystal alloys
01/15/2004US20040009061 Compressors
01/15/2004US20040009059 Stationary blade in gas turbine and gas turbine comprising the same
01/15/2004US20040007878 Turbine power generator including supplemental parallel cooling and related methods
01/15/2004US20040007830 Sealing structure of spindle bolt, and gas turbine
01/15/2004US20040007823 Seal for a rotating member
01/15/2004US20040007422 Device for connecting two tubular pieces of an aircraft turbine engine
01/15/2004US20040007219 Power generation device
01/15/2004US20040006994 Gas turbine engine
01/15/2004US20040006987 Turbine power generation systems and methods using off-gas fuels
01/15/2004US20040006966 Optimizing inlet air for gas turbines
01/14/2004EP1381143A1 Turbine power generator including supplemental parallel cooling and related methods
01/14/2004EP1380796A2 Fuel system
01/14/2004EP1380778A1 Seal
01/14/2004EP1380740A2 Fuel supply system for an electricity generating system
01/14/2004EP1380726A2 Stationary blade in gas turbine and gas turbine comprising the same
01/14/2004EP1380672A1 Highly oxidation resistant component
01/14/2004EP1379764A1 Gas turbine, vehicle comprising said gas turbine and method for engine-braking a gas turbine
01/14/2004CN1468352A Method and device for supplying fuel to a premix burner
01/14/2004CN1468136A Methods for filtering air for a gas turbine system
01/14/2004CN1467407A Gas turbine engine combustor can with trapped vortex cavity
01/14/2004CN1467395A Seal for a rotating member
01/14/2004CN1467380A 涡轮燃油泵 Turbo fuel pump
01/14/2004CN1467366A Failsafe film cooled wall
01/14/2004CN1467365A Structural cover for gas turbine engine bolted flanges
01/14/2004CN1467363A Stationary blade in gas turbine and gas turbine comprising the same
01/13/2004US6676372 Gas turbine with axially mutually displaceable guide parts
01/13/2004US6676370 Shaped part for forming a guide ring
01/13/2004US6676369 Aspirating face seal with axially extending seal teeth
01/13/2004US6675586 Heat shield arrangement for a component carrying hot gas, in particular for structural parts of gas turbines
01/13/2004US6675585 Connection for a two-part CMC chamber
01/13/2004US6675584 Coated seal article used in turbine engines
01/13/2004US6675583 Combustion method
01/08/2004WO2004003362A1 Power fluctuation suppressing method and power generation facility using same
01/08/2004WO2004003357A2 Orbiting combustion nozzle engine
01/08/2004WO2004003347A1 Gas turbine ventilation circuitry
01/08/2004US20040005238 For the production of single-crystal components or components with a directionally solidified microstructure such as for example blades or vanes for gas turbines; can also be used for conventionally cast components.
01/08/2004US20040005217 Methods and apparatus for turbine nozzle locks
01/08/2004US20040005216 Gas turbine shroud structure
01/08/2004US20040003968 Bearing lubrication system for a turbomachine
01/08/2004US20040003889 Method for repairing loose molded-in bushings
01/08/2004US20040003596 Fuel premixing module for gas turbine engine combustor
01/08/2004US20040003595 Combustion turbine power generation system and method of controlling the same
01/08/2004US20040003594 Combustion turbine power generation system and method of controlling the same