| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
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| 03/10/2004 | EP1396608A2 Integrally bladed rotor |
| 03/10/2004 | EP1396299A1 Process for filling up a hole in a component |
| 03/10/2004 | CN1481293A Method for smoothing surface of gas turbine blade |
| 03/09/2004 | US6703137 Segmented thermal barrier coating and method of manufacturing the same |
| 03/09/2004 | US6702552 Impeller having blade(s) conforming to the golden section of a logarithmic curve |
| 03/09/2004 | US6702551 Steam turbine |
| 03/09/2004 | US6702549 Turbine installation |
| 03/09/2004 | US6702547 Gas turbine |
| 03/09/2004 | US6701717 Cycle gas turbine engine |
| 03/09/2004 | US6701616 Method of repairing shroud tip overlap on turbine buckets |
| 03/09/2004 | US6701615 Inspection and sorting system and method for part repair |
| 03/04/2004 | WO2004018844A1 Recirculation structure for a turbocompressor |
| 03/04/2004 | WO2003100110A3 Method for removing at least one partial area of a component made of metal or a metallic compound |
| 03/04/2004 | US20040043889 Strain tolerant aggregate material |
| 03/04/2004 | US20040042927 Gas turbine blades; chemical and heat resistance |
| 03/04/2004 | US20040042902 Organic matrix composite integrally bladed rotor |
| 03/04/2004 | US20040042900 Gas turbine engine disk rim with axially cutback and circumferentially skewed cooling air slots |
| 03/04/2004 | US20040042896 Gas turbine shaft and heat shield cooling arrangement |
| 03/04/2004 | US20040042692 Foil bearing |
| 03/04/2004 | US20040040361 Method of producing bladed components, blanks for bladed components, and use of the blanks |
| 03/04/2004 | US20040040360 Method of manufacturing blade retainer and manufacturing devices therefor |
| 03/04/2004 | US20040040314 Gas turbine and spacer member for the use therein |
| 03/04/2004 | DE10330084A1 Rezirkulationsstruktur für Turboverdichter A recirculation for turbo compressors |
| 03/04/2004 | DE10236273A1 'Turax' turbine-type motor with triple action has axial rotor blades with jets and medium flow around radial blades |
| 03/03/2004 | EP1394387A2 Turbochargers |
| 03/03/2004 | EP1394361A1 Gas turbine |
| 03/03/2004 | EP1394360A1 Nondestructive method for testing a component as well as method to produce a gas turbine blade |
| 03/03/2004 | EP1394359A2 Mixed flow turbine and mixed flow turbine rotor blade |
| 03/03/2004 | EP1394358A2 Gas turbine engine disk rim with axially cutback and circumferentially skewed cooling air slots |
| 03/03/2004 | EP1394278A1 Reduced-tantalum superalloy composition and article made therefrom, and method for selecting a reduced-tantalum superalloy |
| 03/03/2004 | EP1394139A2 Protective overlayer for ceramics |
| 03/03/2004 | EP1394138A2 Protective overlayer for ceramics |
| 03/03/2004 | EP1393836A1 Method for producing bladed elements, blanks for the bladed elements and use of the blanks |
| 03/03/2004 | EP1392957A1 Abradeable seal system |
| 03/03/2004 | EP1392956A2 Ceramic composite vane with metallic substructure |
| 03/03/2004 | CN1140699C Gas turbine cooling blades |
| 03/02/2004 | US6699607 Barium strontium aluminasilicate protective coating for articles exposed to high temperatures including the hostile thermal environment of a gas turbine engine |
| 03/02/2004 | US6699604 Protective coating including porous silicon nitride matrix and noble metal |
| 03/02/2004 | US6699015 Blades having coolant channels lined with a shape memory alloy and an associated fabrication method |
| 03/02/2004 | US6698645 Method of producing fiber-reinforced metallic building components |
| 03/02/2004 | US6698182 Gas turbine combined plant |
| 02/26/2004 | WO2004016911A1 Method for manufacturing a stator or rotor component |
| 02/26/2004 | WO2004016819A1 Intermetallic material and use of said material |
| 02/26/2004 | US20040038086 Thermal barrier coatings with low thermal conductivity |
| 02/26/2004 | US20040038085 Heat resistant layer is made of a mixed oxide containing 15 mol % of at least one lanthanide sesquioxide, selected from LA, Pr, Nd, Sm, Eu, Tb and mixtures, and balance oxide selected from zirconia, ceria, and hafnia |
| 02/26/2004 | US20040037703 System for connecting and locking rotor blades of an axial compressor |
| 02/26/2004 | US20040037641 Stress defender holes |
| 02/26/2004 | US20040035163 Apparatus and method of correcting deformation of gas turbine blade |
| 02/26/2004 | US20040035118 Blade cooling in a gas turbine engine |
| 02/26/2004 | DE10334827A1 Schaufeldämpfer für einen Bläsernabenhohlraum unter der Schaufel Blade damper for a fan hub cavity under the blade |
| 02/25/2004 | EP1391581A1 Gas turbine moving blade |
| 02/25/2004 | EP1391537A1 COATING FORMING METHOD AND COATING FORMING MATERIAL, AND ABRASIVE COATING FORMING SHEET |
| 02/25/2004 | EP1391531A2 Thermal barrier coating with nitride particles |
| 02/25/2004 | CN1477292A Turbomachine blade and gas turbomachine |
| 02/25/2004 | CN1477230A Hign temp-resistant article and its mfg. method |
| 02/24/2004 | US6696144 Multilayer; heat resistant exterior; toughness, impact strength interior |
| 02/24/2004 | US6695960 Containing a modifying element such as platinum, palladium, ruthenium or rhenium that enhances the capacity of the coating to form from phase beta, by exposure to oxygen at high temperature, an adhesive alumina surface barrier |
| 02/24/2004 | US6695587 Gas turbine airfoil protected by aluminide and platinum aluminide coatings, and its preparation |
| 02/24/2004 | US6695582 Turbine blade wall cooling apparatus and method of fabrication |
| 02/19/2004 | WO2004015273A1 Compressor impeller |
| 02/19/2004 | US20040033158 Precipitation hardened Co-Ni based heat-resistant alloy and production method therefor |
| 02/19/2004 | US20040033156 Nickel-based superalloy having very high resistance to hot-corrosion for monocrystalline blades of industrial turbines |
| 02/19/2004 | US20040033134 Labyrinth seal for fan assembly |
| 02/19/2004 | US20040031140 Methods for salvaging a cast article |
| 02/19/2004 | DE10236676A1 Turbine paddle, for a gas turbine, has at least one cooling passage opening with a structured cooling air flow linking the inner zone with the outer surface |
| 02/19/2004 | DE10236339B3 Method for manufacturing turbine blades with cooling ducts involves making ceramic core with positioning pins embedded in free end to protrude into surrounding moulding shell for removal during mechanical finishing of hardened blades |
| 02/19/2004 | DE10211423B4 Turbinenlaufrad Turbine impeller |
| 02/18/2004 | EP1389668A1 Gas turbine |
| 02/18/2004 | EP0894946B1 Gas turbine cooling stationary vane |
| 02/17/2004 | US6692587 For stationary or moving blades of a gas turbine; high temperature strength and room temperature ductility |
| 02/17/2004 | US6692228 Rotor insert assembly and method of retrofitting |
| 02/17/2004 | US6692222 Micro gas turbine engine with active tip clearance control |
| 02/17/2004 | CA2193165C Cooled turbine vane |
| 02/13/2004 | CA2433613A1 Spray method for mcralx coating |
| 02/12/2004 | US20040028941 Mullite undercoating; heat resistance, waterproofing |
| 02/12/2004 | US20040028938 Method of making a protective coating forming a thermal barrier with a bonding underlayer on a superalloy substrate, and a part obtained thereby |
| 02/12/2004 | US20040028527 Film cooled article with improved temperature tolerance |
| 02/12/2004 | US20040028526 Axial flow compressor |
| 02/12/2004 | US20040025494 Device for centering a tube in a turbine shaft |
| 02/12/2004 | DE10247358B3 Heat removal turbine for power generation |
| 02/11/2004 | EP1388642A2 Variable-geometry turbine stator blade, particularly for aircraft engines |
| 02/11/2004 | EP1387926A1 Inner platform impingement cooling by supply air from outside |
| 02/11/2004 | CN1474907A Lead-in structure and fixing flange for turbo generator |
| 02/11/2004 | CN1474037A Gas turbine and method for discharging gas from gas turbine |
| 02/11/2004 | CN1474035A Adjusting method for realizing large area adjustment for grouped gurbine guide blade |
| 02/11/2004 | CN1474033A Vortex wheel turbine |
| 02/10/2004 | US6689995 Apparatus and method for healing a workpiece of metal |
| 02/10/2004 | US6689487 Thermal barrier coating |
| 02/10/2004 | US6688847 Shaft structure and bearing structure for tail end of rotor of gas turbine |
| 02/10/2004 | US6688512 Apparatus and method for friction welding |
| 02/10/2004 | US6688110 Air impingement cooling system |
| 02/10/2004 | US6687994 Method for the manufacture of a welded rotor of a fluid-flow machine |
| 02/05/2004 | WO2004011788A1 Single rotor turbine |
| 02/05/2004 | WO2003059569A9 Method of forming turbine blade root |
| 02/05/2004 | US20040023596 Backer inserts for blocking backwall water jet strikes |
| 02/05/2004 | US20040023056 Metallic material that can be worn away by abrasion; parts, casings, and a process for producing said material |
| 02/05/2004 | US20040023020 Thermal barrier coating utilizing a dispersion strengthened metallic bond coat |
| 02/05/2004 | US20040022648 Compressor impeller |
| 02/05/2004 | US20040022634 Hollow fan hub under blade bumper |
| 02/05/2004 | US20040022633 Insulated cooling passageway for cooling a shroud of a turbine blade |