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