| 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) |
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| 06/30/2005 | US20050139295 Gas turbine blades; chemical and heat resistance |
| 06/30/2005 | US20050139019 Air turbine starter having a low differential check valve |
| 06/30/2005 | US20050138932 Aircraft protection method and system |
| 06/30/2005 | US20050138931 Bulkhead panel for use in a combustion chamber of a gas turbine engine |
| 06/30/2005 | US20050138806 Methods and apparatus for optimizing turbine engine shell radial clearances |
| 06/30/2005 | DE10355917A1 Gasturbine, insbesondere Flugtriebwerk, und Verfahren zur Erzeugung elektrischer Energie bei einer Gasturbine Gas turbine, in particular aircraft engine, and method for generating electrical energy in a gas turbine |
| 06/30/2005 | CA2549748A1 Pressurized oil supply for propeller engine system |
| 06/29/2005 | EP1548238A2 Methods and apparatus for optimizing turbine engine shell radial clearances |
| 06/29/2005 | EP1548234A2 Impingement baffle with embedded deflector |
| 06/29/2005 | EP1548231A2 Fairing for a turbine frame strut |
| 06/29/2005 | EP1548229A2 Airfoil surface impedance modification for noise reduction in turbofan engines |
| 06/29/2005 | EP1548135A1 High temperature alloys, and articles made and repaired therewith |
| 06/29/2005 | EP1547714A2 Hole drilling guide and method |
| 06/29/2005 | EP1546622A1 A reduced carbon dioxide emission system and method for providing power for refrigerant compression and electrical power for a light hydrocarbon gas liquefaction process using cooled air injection to the turbines |
| 06/29/2005 | EP1546527A1 Nested channel ducts for nozzle construction and the like |
| 06/29/2005 | EP1546526A2 Particle separator for a turbine engine |
| 06/29/2005 | EP1546522A1 Internally mounted radial flow intercooler for a combustion air charger |
| 06/29/2005 | CN1633554A Ejector based engines |
| 06/28/2005 | US6911742 Method and apparatus for turbine/alternator on common shaft during start-up |
| 06/28/2005 | US6910863 Methods and apparatus for assembling a bearing assembly |
| 06/28/2005 | US6910854 Leak resistant vane cluster |
| 06/28/2005 | US6910853 Structures for attaching or sealing a space between components having different coefficients or rates of thermal expansion |
| 06/28/2005 | US6910852 Methods and apparatus for cooling gas turbine engine rotor assemblies |
| 06/28/2005 | US6910851 Turbofan jet engine having a turbine case cooling valve |
| 06/28/2005 | US6910620 Method for providing turbulation on the inner surface of holes in an article, and related articles |
| 06/28/2005 | US6910327 Apparatus and methods for varying inlet lip geometry of a jet engine inlet |
| 06/28/2005 | CA2371470C High thrust turbocharger rotor with ball bearings |
| 06/23/2005 | WO2005057032A1 Bearing device for turbocharger |
| 06/23/2005 | WO2005056994A1 Air-storage plant |
| 06/23/2005 | WO2005042948A3 Air turbine starter with unitary inlet and stator |
| 06/23/2005 | US20050137441 A fuel deoxygenator and an oxygen scavenger module for removing dissolved oxygen, increasing usable cooling capability of a fuel |
| 06/23/2005 | US20050136249 Heat resistant article having thermal barrier coatinging |
| 06/23/2005 | US20050135929 Pressurized oil supply for propeller engine system |
| 06/23/2005 | US20050133193 Investment casting cores |
| 06/23/2005 | US20050133122 High temperature alloys, and articles made and repaired therewith |
| 06/23/2005 | US20050132717 Gas turbine part provided with a protective coating, and a method of making a protective coating on a superalloy metal substrate |
| 06/23/2005 | US20050132715 Methods and apparatus for assembling gas turbine engines |
| 06/23/2005 | US20050132711 Variable turbine cooling flow system |
| 06/23/2005 | US20050132710 Bifurcated oil scavenge system for a gas turbine engine |
| 06/23/2005 | US20050132707 Gas turbo set |
| 06/23/2005 | US20050132706 Device for supplying secondary air in a gas turbine engine |
| 06/23/2005 | US20050132695 Single-piece turbine rotor and pinion gear and manufacturing technique for same |
| 06/23/2005 | US20050132693 Gas turbine engine architecture |
| 06/23/2005 | US20050132570 Methods and apparatus for machining components |
| 06/23/2005 | CA2490337A1 High temperature alloys, and articles made and repaired therewith |
| 06/22/2005 | EP1544481A1 Metal sheet comprising means for fixing to a support and a seal |
| 06/22/2005 | EP1544437A2 Multi-stage fuel deoxygenator |
| 06/22/2005 | EP1544436A1 Method for operating a gas turbine system, and a corresponding system |
| 06/22/2005 | EP1544417A2 Bifurcated oil scavenge system for a gas turbine engine |
| 06/22/2005 | EP1544416A2 Bearing assembly for a gas turbine rotor |
| 06/22/2005 | EP1544185A2 Environmental barrier coating comprising a gas velocity reducing top layer |
| 06/22/2005 | EP1543918A2 Holding Device for Gas Turbine Rotor Blades and Machine Tool incorporating such a device |
| 06/22/2005 | EP1543896A2 Investment casting cores |
| 06/22/2005 | CN1629541A Thick coated combustor liner |
| 06/22/2005 | CN1629465A Electricity generating and liquid purifying apparatus |
| 06/22/2005 | CN1629464A Mounting of the rotor of a gas turbine |
| 06/22/2005 | CN1628922A Investment casting cores |
| 06/22/2005 | CA2489963A1 Hole-drilling guide and method |
| 06/21/2005 | US6910156 Method and system for diagnosing a technical installation |
| 06/21/2005 | US6909263 Gas turbine engine starter-generator exciter starting system and method including a capacitance circuit element |
| 06/21/2005 | US6909199 Method and apparatus for compensating output voltage fluctuations of turbine/alternator on common shaft |
| 06/21/2005 | US6908518 Noncracking; high temperature heat resistance; high strength;heating, casting |
| 06/21/2005 | US6908303 Premixed air-fuel mixture supply device |
| 06/21/2005 | US6908285 Methods and apparatus for assembling rotatable machines |
| 06/21/2005 | US6907738 Pilot air apparatus and method for a combustor of gas turbine |
| 06/21/2005 | US6907724 Combined cycle engines incorporating swirl augmented combustion for reduced volume and weight and improved performance |
| 06/19/2005 | CA2486052A1 Investment casting cores |
| 06/18/2005 | CA2489629A1 Methods and apparatus for machining components |
| 06/18/2005 | CA2488304A1 Multi-stage fuel deoxygenator |
| 06/16/2005 | WO2005055688A1 Control arrangement |
| 06/16/2005 | WO2005054645A1 Gas turbine, in particular aircraft engine and method for generating electrical energy in a gas turbine |
| 06/16/2005 | WO2004069749B1 Improved configuration and process for carbonyl removal |
| 06/16/2005 | US20050131616 Turbine mechanical output computation device and gas turbine control device equipped therewith |
| 06/16/2005 | US20050130089 Premixed air-fuel mixture supply device |
| 06/16/2005 | US20050129976 An aluminum plate having a purity of 99.5% or more, is caused to contact at least one side of a ceramic substrate of aluminum nitride or alumina to be heated at a temperature of 620 to 650 degrees C. in an inert gas to bond the aluminum plate directly to the ceramic substrate, power modules |
| 06/16/2005 | US20050129973 Velocity barrier layer for environmental barrier coatings |
| 06/16/2005 | US20050129972 Thermal barrier coating system method of manufacturing the same |
| 06/16/2005 | US20050129862 Thermal barrier coating protected by alumina and method for preparing same |
| 06/16/2005 | US20050129506 Mounting of the rotor of a gas turbine |
| 06/16/2005 | US20050129505 Turbine engine bearing support |
| 06/16/2005 | US20050126182 Hybrid microturbine for generating electricity |
| 06/16/2005 | US20050126179 Gas fuel compression by liquification |
| 06/16/2005 | US20050126177 Thermal gas compression engine |
| 06/16/2005 | US20050125983 Method of manufacturing axis seals, axis seals, axis seal members and rotary machine using axis seals |
| 06/16/2005 | DE102004055760A1 Dichtungsanordnung für eine Turbine, Schaufel, dieselbe enthaltende Turbine, Verfahren zum Abdichten des Zwischenraums zwischen den rotierenden und stationären Komponenten einer Turbine A sealing arrangement for a turbine blade, turbine containing the same, methods for sealing the gap between the rotating and stationary components of a turbine |
| 06/15/2005 | EP1541834A1 Power take-off for the accessories of a twin spool turbo-jet engine |
| 06/15/2005 | EP1541833A1 Gas generator and jet engine being equipped with the same for starting |
| 06/15/2005 | EP1541807A2 Use of spray coatings to achieve non-uniform seal clearances in turbomachinery |
| 06/15/2005 | EP1541714A1 Method for repairing components using environmental bond coatings and resultant repaired components |
| 06/15/2005 | EP1540157A1 Improved fuel delivery system |
| 06/15/2005 | EP1540143A1 Rotor recentring after decoupling |
| 06/15/2005 | EP1540141A1 Method for manufacturing a stator or rotor component |
| 06/15/2005 | EP1540026A1 Property recovering method for nickel superalloy |
| 06/15/2005 | EP1539573A1 Torsionally de-coupled engine mount system |
| 06/15/2005 | EP1463879A4 A gas turbine apparatus and a starting method thereof |
| 06/15/2005 | EP1421258B1 Blade for a turbine engine and method for production of said blade |
| 06/15/2005 | EP1244881B1 Brush seals |
| 06/15/2005 | CN1626877A Burner of gas turbine |
| 06/15/2005 | CN1626783A Turbine mechanical output computation device and gas turbine control device equipped therewith |
| 06/15/2005 | CN1626774A Use of spray coatings to achieve non-uniform seal clearances in turbo machinery |