| 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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| 04/07/2004 | CN1487180A Aero-gas turbine having control blades used for backward rotary low-pressure turbine |
| 04/07/2004 | CN1144935C Axial flow turbine |
| 04/07/2004 | CN1144897C Method for simultanously calorization of nickel based and cobalt based super alloy |
| 04/06/2004 | US6715993 Methods and apparatus for manufacturing rotor shafts |
| 04/06/2004 | US6715990 First stage turbine bucket airfoil |
| 04/06/2004 | US6715988 Turbine airfoil for gas turbine engine |
| 04/06/2004 | US6715983 Method and apparatus for reducing distortion losses induced to gas turbine engine airflow |
| 04/06/2004 | CA2111045C Method for producing a monobloc rotor with hollow blades and monobloc rotor with hollow blades obtained by said method |
| 04/01/2004 | WO2004027219A1 Variable geometry turbocharger having internal bypass exhaust gas flow |
| 04/01/2004 | WO2004027217A1 Method for testing a component in a non-destructive manner and for producing a gas turbine blade |
| 04/01/2004 | US20040062865 Gas distributor for vapor coating method and container |
| 04/01/2004 | US20040062864 Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure |
| 04/01/2004 | US20040062655 Tailored attachment mechanism for composite airfoils |
| 04/01/2004 | US20040062653 Blade retention scheme using a retention tab |
| 04/01/2004 | US20040062652 Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine |
| 04/01/2004 | US20040062651 Blade for turbine engine |
| 04/01/2004 | US20040062649 Tolerant internally-cooled fluid guide component |
| 04/01/2004 | US20040062643 Turbomachinery blade retention system |
| 04/01/2004 | US20040062637 Integral swirl knife edge injection assembly |
| 04/01/2004 | US20040062636 Crack-resistant vane segment member |
| 04/01/2004 | US20040060964 Turbine blade closure system |
| 04/01/2004 | US20040060839 Container and pallet for receiving blades of a fluid machine |
| 04/01/2004 | US20040060347 Method and system for detecting damage to the rotor of an aircraft engine |
| 04/01/2004 | DE10244199A1 Device for supplying secondary fluid to transsonic primary flow e.g. for supplying cooling air for film cooling in turbine plant |
| 04/01/2004 | DE10244192A1 Gasturbine mit Vorrichtung zur Arbeitsentnahme zur Kühlung von Scheiben Gas turbine with a device to work removing the cooling of discs |
| 04/01/2004 | DE10243415A1 Verfahren zur Erzeugung von Druckeigenspannungen in der Oberfläche von Werkstücken A method for generating internal compressive stress in the surface of workpieces |
| 03/31/2004 | EP1403469A2 Method for selective surface protection of a gas turbine blade |
| 03/31/2004 | EP1403398A2 Method for treating organs subject to erosion by liquids and anti-erosion coating alloy |
| 03/31/2004 | EP1403397A1 Cobalt-based alloy for the coating of components subject to erosion by liquid |
| 03/31/2004 | EP1403395A1 Method for vapor phase aluminiding of a gas turbine blade partially masked with a masking enclosure |
| 03/31/2004 | EP1403233A1 An article comprising a silicon based substrate |
| 03/31/2004 | EP1402981A1 Method and device for manufacturing a fork-shaped foot of a turbine blade |
| 03/31/2004 | EP1402152A1 Securing system for the rotor blades of axial flow turbo engines |
| 03/31/2004 | EP1402151A1 Fastening of blades |
| 03/31/2004 | CN1485528A Mixed flow turbine and mixed flow turbine rotor blade |
| 03/31/2004 | CN1143954C 燃气轮机 Gas turbine |
| 03/31/2004 | CN1143945C Internally cooled steam turbine shaft and method for cooling the same |
| 03/30/2004 | US6713722 Rotor and method for welding an element of a rotor |
| 03/30/2004 | US6712120 Device and method for casting a workpiece and workpiece |
| 03/25/2004 | WO2004025086A1 Gas turbine sealing air supply system |
| 03/25/2004 | WO2004024971A1 Property recovering method for nickel superalloy |
| 03/25/2004 | US20040058200 Method of forming a ceramic coating on a substrate by electron-beam physical vapor deposition |
| 03/25/2004 | US20040058191 Compliant layer coating for a ceramic turbine blade wherein the layer is capable of operating at higher temperatures and levels of stress in an oxidizing environment |
| 03/25/2004 | US20040057834 Connection method for turbo charger turbine shaft |
| 03/25/2004 | US20040057833 First stage turbine bucket airfoil |
| 03/25/2004 | US20040057832 Gas turbine blade |
| 03/25/2004 | US20040055736 Method of making turbine blades having cooling channels |
| 03/25/2004 | US20040055676 High strength, toughness, impact strength; high speed working; rotor blades |
| 03/25/2004 | DE10336863A1 Thermal turbo-machine e.g. gas turbine, has at least two adjacent turbine vanes, and continuous cover band that extends in rear part of vane to smallest cross-section region of maximum plus/minus 3 per cent of chord length |
| 03/24/2004 | EP1400698A1 Axial positioning control of a compressor blade |
| 03/24/2004 | EP1400669A1 Gas turbine engine with apparatus for generation of mechanical work for cooling of discs |
| 03/24/2004 | EP1400659A1 Methods and apparatus for sealing gas turbine engine variable vane assemblies |
| 03/24/2004 | EP1400657A2 First stage turbine bucket airfoil |
| 03/24/2004 | EP1400656A2 Airfoil shape of a second stage turbine blade |
| 03/24/2004 | EP1400610A1 Thermal barrier coatings with low thermal conductivity comprising lanthanide sesquioxides |
| 03/24/2004 | EP1400607A1 Thermal barrier coating with improved strength and fracture toughness |
| 03/24/2004 | CN1484731A Rotary nozzle turbine |
| 03/24/2004 | CN1143056C Discharge header for guiding hot gas in gas turbine |
| 03/23/2004 | US6709239 Three dimensional blade |
| 03/23/2004 | US6709237 Turbine blade or vane and process for producing a turbine blade or vane |
| 03/23/2004 | US6709233 Aerofoil for an axial flow turbomachine |
| 03/23/2004 | US6709232 Cambered vane for use in turbochargers |
| 03/23/2004 | US6709231 Stator of a variable-geometry axial turbine for aeronautical applications |
| 03/23/2004 | US6709230 Ceramic matrix composite gas turbine vane |
| 03/23/2004 | US6708482 Aircraft engine with inter-turbine engine frame |
| 03/18/2004 | WO2004022980A1 Aperiodic struts for enhanced blade responses |
| 03/18/2004 | WO2004022923A1 Turbine moving blade |
| 03/18/2004 | WO2004022922A1 Improved cambered vane for use in turbochargers |
| 03/18/2004 | WO2004022266A1 Method for closing an aperture in a component |
| 03/18/2004 | US20040052643 Linear surface concavity enhancement |
| 03/18/2004 | US20040052636 Methods and apparatus for sealing gas turbine engine variable vane assemblies |
| 03/18/2004 | US20040051219 Method for vibration damping using superelastic alloys |
| 03/18/2004 | US20040050909 Diffusion bond mixture for healing single crystal alloys |
| 03/18/2004 | US20040050033 Rotary nozzle turbine |
| 03/18/2004 | DE10241741A1 Gas turbine has surface exposed to cooling fluid which has burls which are formed by arc welding |
| 03/17/2004 | EP1398394A1 Cold spraying method for MCrAIX coating |
| 03/17/2004 | EP1398393A1 Property recovering method |
| 03/17/2004 | EP1398098A1 Method for fabrication of turbine blades with cooling channels |
| 03/16/2004 | US6706319 Mixed powder deposition of components for wear, erosion and abrasion resistant applications |
| 03/16/2004 | US6706241 Nickel-base superalloy |
| 03/16/2004 | US6705836 Gas turbine blade cooling circuits |
| 03/16/2004 | US6705834 Axial flow turbine type rotor machine for elastic fluid operation |
| 03/16/2004 | US6705832 Turbine |
| 03/16/2004 | US6705831 Linked, manufacturable, non-plugging microcircuits |
| 03/16/2004 | US6705383 Process for the rapid production of hollow components of flow machines for manufacturing development |
| 03/16/2004 | US6705011 Turbine element manufacture |
| 03/16/2004 | CA2188138C Centrifugal chopper pump |
| 03/11/2004 | WO2003098020A3 Gas turbine with stator shroud in the cavity beneath the chamber |
| 03/11/2004 | US20040048090 Corrosion-resistant layered coatings |
| 03/11/2004 | US20040047727 Cambered vane for use in turbochargers |
| 03/11/2004 | US20040047724 Combustion turbine with airfoil having enhanced leading edge diffusion holes and related methods |
| 03/11/2004 | US20040047722 Aperiodic struts for enhanced blade responses |
| 03/11/2004 | US20040046326 Gas turbine |
| 03/11/2004 | US20040045936 Chemical milling of gas turbine engine blisks |
| 03/11/2004 | US20040045644 T-tial alloy-based component comprising areas having a graduated structure |
| 03/11/2004 | US20040045291 Flow laminarizing device |
| 03/11/2004 | DE10243169A1 Verfahren zur Herstellung beschaufelter Bauteile, Rohlinge für beschaufelte Bauteile und Verwendung der Rohlinge Process for the preparation of bladed components, blanks for bladed components and use of the blanks |
| 03/10/2004 | EP1396621A1 Surface-reformed exhaust gas guide assembly of vgs type turbo charger, and method of surface-reforming component member thereof |
| 03/10/2004 | EP1396620A1 Exhaust guide assembly for vgs type turbo charger improved in heat resistance and method of producing heat-resisting members applicable thereto, and method of producing raw material for variable vanes applicable thereto |
| 03/10/2004 | EP1396609A2 Gas turbine with a spacer member and a turbine rotor disk defining an air cooling passage |