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)
11/2005
11/06/2005CA2504449A1 Integrated ceramic/metallic components and methods of making the same
11/06/2005CA2500503A1 Cooled turbine airfoil
11/04/2005CA2506092A1 Aircraft engine with means of hanging from an aircraft structure
11/03/2005WO2005103567A1 Liquid fuel injection with purge air
11/03/2005WO2005103465A1 Turbine nozzle segment, turbine nozzle, turbine, and gas turbine engine
11/03/2005US20050244266 Turbine casing having refractory hooks and obtained by a powder metallurgy method
11/03/2005US20050242781 Power fluctuation suppressing method and power generation facility using same
11/03/2005US20050241320 System for cooling cooling air in a gas turbine, and method for cooling cooling air
11/03/2005US20050241318 Multiple electric fuel metering systems for gas turbine applications
11/03/2005US20050241314 Cooling structure of gas turbine tail pipe
11/03/2005US20050241290 Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing
11/03/2005US20050241288 High efficiency rotor for the first phase of a gas turbine
11/03/2005US20050241287 High efficiency stator for the first phase of a gas turbine
11/03/2005US20050241149 Method for manufacturing a stator component
11/03/2005DE102005014565A1 Method for preventing ice build up especially in air intake of gas turbine engine has controlled feedback of heated compressed air into the air intake to match computed expected icing levels
11/03/2005CA2562540A1 Liquid fuel injection with purge air
11/02/2005EP1591714A1 Device for lubricating a component in an assembly
11/02/2005EP1591644A1 Device for the exploitation of waste heat from compressors
11/02/2005EP1591643A1 Noise reduction assembly for flight gas turbine
11/02/2005EP1591623A2 Turbine engine and assembly method for this engine
11/02/2005EP1590072A1 Evaporative duplex counterheat exchanger
11/02/2005EP1546526A4 Particle separator for a turbine engine
11/02/2005EP1173656B1 High pressure turbine cooling of gas turbine engine
11/02/2005CN1692250A Cooling structure of gas turbine tail pipe
11/02/2005CN1690389A Rotating seal arrangement for turbine bucket cooling circuits
11/02/2005CN1690388A Integral spark detector in fitting which supports igniter in gas turbine engine
11/02/2005CN1690387A Detecting spark in igniter of gas turbine engine by detecting signals in grounded shielding
11/02/2005CN1690365A Methods and apparatus for assembling gas turbine engine rotor assemblies
11/02/2005CN1690364A Turbulator on the underside of a turbine blade tip turn and related method
11/01/2005US6960900 Method and apparatus for starting a gas turbine using a polyphase electric power generator
11/01/2005US6960840 Integrated turbine power generation system with catalytic reactor
11/01/2005US6960395 zirconia and stabilizer with three metal oxides (yttria, lanthana and ytterbia); physical vapor deposition onto metal substrate exposed to high temperatures; columnar microstructure
11/01/2005US6960245 Filter arrangement and methods
11/01/2005US6960060 Dual coolant turbine blade
11/01/2005US6959552 Gas turbine inlet flow straightener
11/01/2005US6959536 Fuel pump metering system
11/01/2005US6959535 Differential pressure induced purging fuel injectors
10/2005
10/27/2005WO2005100941A1 Apparatus and method of balancing a shaft of an aircraft engine
10/27/2005WO2005100765A1 Dual inlet turboprop
10/27/2005WO2005100753A1 Strut comprising a sound-absorbing material for a turbine engine
10/27/2005US20050238907 Highly oxidation resistant component
10/27/2005US20050238893 Substrate with protective coating; chromium, aluminum, yttrium alloy interface
10/27/2005US20050238525 Alloy containing silicon, nickel, carbon, at least a refractory metal which promotes work hardening is selected from molybdenum, niobium, tungsten, tantalum, rhenium, balance is cobalt; having good wear resistance, as well as good ductility due to content of hard particles (e.g. carbide) reduced
10/27/2005US20050238488 Turbulator on the underside of a turbine blade tip turn and related method
10/27/2005US20050238484 Gas turbine engine blade containment assembly
10/27/2005US20050238480 Casing arrangement
10/27/2005US20050238477 Stator of a high-pressure turbine of a turbomachine, and a method of assembling it
10/27/2005US20050236225 Device and method for active soundproofing, and power unit for aeroplanes
10/27/2005US20050235651 Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump
10/27/2005US20050235649 Method for operating a gas turbine
10/27/2005US20050235648 Orbiting combustion nozzle engine
10/27/2005US20050235647 Sealing body
10/27/2005US20050235627 Gas turbine heat exchanger assembly and method for fabricating same
10/27/2005US20050235626 Gas turbine heat exchanger assembly and method for fabricating same
10/27/2005US20050235625 Device for utilizing the waste heat of compressors
10/27/2005US20050235492 Turbine airfoil trailing edge repair and methods therefor
10/27/2005DE102004017682A1 Verfahren und Vorrichtung zum Fördern einer Flüssigkeit Method and apparatus for conveying a liquid
10/27/2005DE102004017096A1 Strebe für ein Turbinentriebwerk Strut for a turbine engine
10/27/2005CA2562710A1 Apparatus and method of balancing a shaft
10/27/2005CA2505058A1 Process for closing a hole in a metal part by means of friction welding, use of a metal bar and a bearing bracket to carry out the process
10/27/2005CA2504167A1 Noise reduction assembly for aircraft turbojet engine
10/26/2005EP1589226A1 Pump assembly
10/26/2005EP1589205A2 Fuel metering unit
10/26/2005EP1589204A2 Gas turbine heat exchanger assembly
10/26/2005EP1589194A2 Gas turbine stator segment anti-rotation lock
10/26/2005EP1589193A2 Coolable rotor blade for a gas turbine engine
10/26/2005EP1588048A1 System and method for generating and sustaining a corona electric discharge for igniting a combustible gaseous mixture
10/26/2005EP1587603A2 Improved configuration and process for carbonyl removal
10/26/2005EP1587602A1 Configuration and process for carbonyl removal
10/26/2005EP1552132A4 Turbine engine apparatus and method
10/26/2005EP1071608B1 Biplanar scarfed nacelle inlet
10/25/2005US6957949 Internal cooling circuit for gas turbine bucket
10/25/2005US6957541 Gas turbine and operation method of gas turbine combined electric generating plant, gas turbine combined electric generating plant, and computer product
10/25/2005US6957539 Power generator with low CO2 emissions and associated method
10/25/2005US6957537 Combustor of a gas turbine having a nozzle pipe stand
10/20/2005WO2005098218A1 Reversible gas turbine gear box
10/20/2005WO2005098217A1 Method and device for transporting a liquid
10/20/2005WO2005097412A2 Seal removal tool for a seal having a grooved inner peripheral surface
10/20/2005US20050233160 Thermal spray compositions for abradable seals
10/20/2005US20050232784 Pump assembly
10/20/2005US20050232774 Turbine engine rotor retainer
10/20/2005US20050232772 Rotating seal arrangement for turbine bucket cooling circuits
10/20/2005US20050232764 Flexible seal assembly between gas turbine components and methods of installation
10/20/2005US20050232755 System for blocking a main shaft of an engine having a fusible bearing
10/20/2005US20050232752 Turbine shroud cooling system
10/20/2005US20050231052 Apparatus and method of balancing a shaft
10/20/2005US20050229606 Annular combustion chamber for a turbomachine with an improved inner fastening flange
10/20/2005US20050229605 Hybrid inlet
10/20/2005US20050229602 Forced air cooling system
10/20/2005US20050229601 Gas Turbine Engine Cooling System and Method
10/20/2005US20050229357 Metal sheet, including means for fixing it to a support and a gasket seal
10/20/2005CA2562290A1 Reversible gas turbine gearbox
10/20/2005CA2504114A1 Turbine, particularly useful for small aircraft
10/19/2005EP1586669A1 Oxidation resistant superalloy and article
10/19/2005EP1373685B1 Gas turbine blade
10/19/2005EP1098724B1 Ceramic shell mold provided with reinforcement, and related processes
10/19/2005CN1685187A Reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process
10/19/2005CN1685066A Producing metallic articles by reduction of nonmetallic precursor compounds and melting
10/19/2005CN1683833A Single crystal articles having controlled crystallographic orientation
10/19/2005CN1683766A Flexible seal assembly between gas turbine components and methods of installation
1 ... 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 ... 309