| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
|---|
| 04/26/2005 | US6884029 Heat-tolerated vortex-disrupting fluid guide component |
| 04/26/2005 | US6884028 Turbomachinery blade retention system |
| 04/26/2005 | US6884027 Sealing of turbomachinery casing segments |
| 04/26/2005 | US6884023 Integral swirl knife edge injection assembly |
| 04/26/2005 | US6884021 Single cascade multistage turbine |
| 04/26/2005 | US6883700 Turbine blade closure system |
| 04/26/2005 | US6883303 Aircraft engine with inter-turbine engine frame |
| 04/26/2005 | US6883234 Process for machining axial blade slots in turbine disks for jet engines |
| 04/26/2005 | CA2376163C Efficiency enhanced turbine engine |
| 04/26/2005 | CA2372623C Axial flow turbine having stepped portion formed in axial-flow turbine passage |
| 04/26/2005 | CA2113376C Device for securing rotor blades axially and for eliminating rotor imbalances in axial-flow compressors or turbines |
| 04/21/2005 | WO2005035947A1 Hollow turbine blade stiffening |
| 04/21/2005 | WO2005035946A1 Rotor balancing device and method |
| 04/21/2005 | WO2005035464A1 Braze-based protective coating for silicon- based substrate |
| 04/21/2005 | WO2005001260A3 Blade cooling in a gas turbine engine |
| 04/21/2005 | US20050085989 Turbine component tracking system |
| 04/21/2005 | US20050084381 Tri-property rotor assembly of a turbine engine, and method for its preparation |
| 04/21/2005 | US20050084380 Hollow turbine blade stiffening |
| 04/21/2005 | US20050084379 Compressor blade root for engine blades of aircraft engines |
| 04/21/2005 | US20050084377 Turbomachine blade, in particular a fan blade, and its method of manufacture |
| 04/21/2005 | US20050084376 Blade retention arrangement |
| 04/21/2005 | US20050084375 Device for attaching a moving blade to a turbine rotor disk in a turbomachine |
| 04/21/2005 | US20050084372 Internal core profile for the airfoil of a turbine bucket |
| 04/21/2005 | US20050084371 Base material with cooling air hole |
| 04/21/2005 | US20050084370 Cooled turbine blade |
| 04/21/2005 | US20050084368 Repair method for a blade of a turbomachine |
| 04/21/2005 | US20050081530 Arrangement for bleeding the boundary layer from an aircraft engine |
| 04/21/2005 | DE19619438B4 Wärmestausegment für eine Turbomaschine Heat shield segment for a turbomachine |
| 04/20/2005 | EP1524410A1 Gas turbine rotor stage and rotor blade with coated rotor blade root and method for coating such a rotor blade root |
| 04/20/2005 | EP1524409A2 Blade-locking system |
| 04/20/2005 | EP1524408A2 Internal core profile for the airfoil of a turbine bucket |
| 04/20/2005 | EP1524406A1 Configuration of a turbomachine rotor blade |
| 04/20/2005 | EP1524405A2 Turbine rotor blade for gas turbine engine |
| 04/20/2005 | EP1524334A1 Protective coating for protecting a structural member against corrosion and oxidation at high temperatures and structural member |
| 04/20/2005 | EP1524328A1 Method of selective region vapor phase aluminizing |
| 04/20/2005 | EP1524061A2 Plasma arc coating apparatus with an environmental cell having a ring with a fluid passageways and plasma arc processes for forming low oxide coatings |
| 04/20/2005 | EP1523609A1 Improved low cycle fatigue life (lcf) impeller design concept |
| 04/20/2005 | EP1343949B1 Further cooling of pre-swirl flow entering cooled rotor aerofoils |
| 04/20/2005 | CN1607319A Apparatus for mounting blade on turbine rotor plate in turbo machine |
| 04/20/2005 | CN1607318A Internal core profile for the airfoil of a turbine bucket |
| 04/20/2005 | CN1607317A A rotor blade for a gas turbine engine |
| 04/19/2005 | US6881038 Airfoil shape for a turbine bucket |
| 04/19/2005 | US6881036 Composite integrally bladed rotor |
| 04/19/2005 | US6881035 Draft inducer having single piece metal impeller and improved housing |
| 04/19/2005 | US6881029 Casing, a compressor, a turbine, and a combustion turbine engine including such a casing |
| 04/19/2005 | US6880338 Lead-in structure and a fixing flange for a turbo generator |
| 04/16/2005 | CA2485152A1 Refractory metal core wall thickness control |
| 04/14/2005 | WO2005033476A1 Turbine |
| 04/14/2005 | WO2005033351A2 Protection of metallic surfaces against thermally-induced wrinkling (rumpling) in particular in gas turbines |
| 04/14/2005 | WO2005032755A2 Laser powder fusion repair of z-notches with inconel 713 powder |
| 04/14/2005 | WO2004111442A3 Strain isolated trim tab |
| 04/14/2005 | US20050079370 Nano-multilayered structures, components and associated methods of manufacture |
| 04/14/2005 | US20050079368 a non-metallic oxide or nitride diffusion barrier layer overlying the substrate; and a protective coating overlying the barrier layer containing at least two platinum group metals (ptatinum or rhodium at least 40%) |
| 04/14/2005 | US20050079343 Brazed layer comprising an intermetallic compound dispersion of silicon nitride particles, silicon oxynitride particles, or a mixture thereof, where brazed layer provides a barrier to the diffusion of oxygen therethrough; high temperature oxidation barrier for silicon-based gas turbine engines |
| 04/14/2005 | US20050079334 Method for making a pin reinforced, crack resistant fiber reinforced composite article |
| 04/14/2005 | US20050079089 Alloy coating, method for forming the same, and member for high temperature apparatuses |
| 04/14/2005 | US20050079062 Blade damper |
| 04/14/2005 | US20050079061 Airfoil shape for a turbine bucket |
| 04/14/2005 | US20050079060 Turbine blades |
| 04/14/2005 | US20050079058 Shrouded turbine blades with locally increased contact faces |
| 04/14/2005 | US20050079050 Gas turbine engine and method of producing the same |
| 04/14/2005 | US20050077272 Coating apparatus and processes for forming low oxide coatings |
| 04/14/2005 | US20050076649 Blade tip clearance control |
| 04/14/2005 | US20050076504 Composite structure formed by cmc-on-insulation process |
| 04/14/2005 | US20050076503 Blade for a turbine engine and method for production of said blade |
| 04/14/2005 | US20050076501 Workpiece with a recess which is closed from the exterior by means of a solder film and method for closing a recess by means of a solder film |
| 04/14/2005 | DE10343761A1 Verschleißschutzschicht, Bauteil mit einer derartigen Verschleißschutzschicht sowie Herstellverfahren Wear protective layer component with such a wear-resistant layer or production process |
| 04/13/2005 | EP1522696A2 Gas turbine axial compressor with water injection |
| 04/13/2005 | EP1522679A2 Guide vanes for turbine |
| 04/13/2005 | EP1522678A2 Fixing method for the blading of a fluid-flow machine and fixing arrangement |
| 04/13/2005 | EP1522677A2 Blade damper |
| 04/13/2005 | EP1522676A2 Airfoil shape for a turbine bucket |
| 04/13/2005 | EP1522608A2 Diffusion barrier and protective coating for turbine engine component and method for forming |
| 04/13/2005 | EP1522607A1 Method for fabricating a coated superalloy stabilized against the formation of secondary reaction zone |
| 04/13/2005 | EP1522535A2 Environmental barrier coating |
| 04/13/2005 | EP1522534A2 Aluminate coating for a silicon containing substrate |
| 04/13/2005 | EP1522533A1 Target destined for electron beam evaporation, its process of manufacture, a thermal barrier layer obtained using the target and a workpiece comprising such a layer. |
| 04/13/2005 | EP1522375A1 Method for producing a multilayered system |
| 04/13/2005 | EP1522369A1 Method of repairing metal articles, preferably blades of gas turbines |
| 04/13/2005 | CN2692350Y Improvement of Dongfeng series internal combustion engine pressurizing unit air compressor working wheel structure |
| 04/13/2005 | CN1606655A Reinforcement and cooling structure of a turbine blade |
| 04/13/2005 | CN1605758A 风扇组件 Fan assembly |
| 04/13/2005 | CN1605715A Method of repairing metal articles, preferably blades of gas turbines |
| 04/13/2005 | CN1605460A Nano-multilayered structures, components and associated methods of manufacture |
| 04/13/2005 | CN1196866C Hydraulic seal for rotary pumps |
| 04/12/2005 | US6878041 Method for removing a metallic layer of a layer-system |
| 04/12/2005 | US6877956 Methods and apparatus for integral radial leakage seal |
| 04/12/2005 | US6877955 Mixed flow turbine and mixed flow turbine rotor blade |
| 04/12/2005 | US6877953 Gas turbine |
| 04/12/2005 | US6877651 Brazing alloy for gas turbine engines, fuel cells, and electronic devices; wetting, fluid flow |
| 04/12/2005 | US6877324 Gas turbine, gas turbine apparatus, and refrigerant collection method for gas turbine moving blades |
| 04/08/2005 | CA2483071A1 Blade damper |
| 04/07/2005 | WO2005031120A1 Variable geometry turbocharger |
| 04/07/2005 | WO2005031038A1 Wear-resistant layer, component comprising such a wear-resistant layer, and production method |
| 04/07/2005 | WO2005030429A2 Method and device for welding structural parts |
| 04/07/2005 | WO2005008067A3 Impeller and cutting elements for centrifugal chopper pumps |
| 04/07/2005 | WO2004092567A3 Integrated bypass turbojet engines for aircraft and other vehicles |
| 04/07/2005 | US20050074625 Barrier coatings for use in high temperature |
| 04/07/2005 | US20050074356 Containing at least iron, silicon, manganese, chromium, nickel, molybdenum, tungsten, cobalt, vanadium, nitrogen and niobium and/or tantalum; controlled ratio of nickel to colbalt and molybdenum to tungsten; fuel efficiency |
| 04/07/2005 | US20050074335 Fixing method for the blading of a fluid-flow machine and fixing arrangement |