| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
|---|
| 10/01/2009 | WO2009119133A1 Cover for cooling passage, method of manufacturing the cover, and gas turbine |
| 10/01/2009 | WO2009119127A1 Gas turbine, intermediate shaft for gas turbine, and method of cooling gas turbine compressor |
| 10/01/2009 | WO2009118245A1 Guide vane for a gas turbine and gas turbine comprising such a guide vane |
| 10/01/2009 | WO2009118235A2 Guide vane for a gas turbine |
| 10/01/2009 | WO2009118234A1 Blade for a rotating thermal engine |
| 10/01/2009 | WO2009118036A1 Turbine rotor for a gas turbine |
| 10/01/2009 | US20090246032 Method of machining airfoil root fillets |
| 10/01/2009 | US20090246031 Method of restoring an airfoil blade |
| 10/01/2009 | US20090246030 Impeller |
| 10/01/2009 | US20090246029 Turbine rotor blade, turbine rotor and steam turbine equipped with the same |
| 10/01/2009 | US20090246028 Fan blade iron isolation |
| 10/01/2009 | US20090246027 Wind/fluid turbine |
| 10/01/2009 | US20090246026 Reinforced Impeller and Method |
| 10/01/2009 | US20090246023 Chambered airfoil cooling |
| 10/01/2009 | US20090246008 Layer System |
| 10/01/2009 | US20090245999 Hybrid impingement cooled airfoil |
| 10/01/2009 | US20090241549 Subsonic and stationary ramjet engines |
| 10/01/2009 | US20090241507 Ground based pulse detonation combustor for power generation |
| 10/01/2009 | DE102008016329A1 Rotor balancing arrangement for gas-turbine engine, has inward aligned strips provided in outer collar of rotor disk, and axial aligned retaining groove provided in strips for balancing bodies that engage in strips and stuck onto strips |
| 10/01/2009 | DE102008016170A1 Bauteil mit sich überlappenden Schweißnähten und ein Verfahren zur Herstellung Component with overlapping welded seams and a process for preparing |
| 10/01/2009 | DE102008015688A1 Turbinenrotor für eine Gasturbine Turbine rotor for a gas turbine |
| 10/01/2009 | CA2719590A1 High temperature resistant coating compositions |
| 10/01/2009 | CA2719575A1 Subsonic and stationary ramjet engines |
| 10/01/2009 | CA2712366A1 Turbine rotor for a gas turbine |
| 09/30/2009 | EP2105579A2 An article formed from a composite material |
| 09/30/2009 | EP2105245A2 Method for repairing an airfoil |
| 09/30/2009 | EP2105244A1 Method of restoring an airfoil blade |
| 09/30/2009 | EP2105236A1 Method for performing electrical discharge machining on an electricity conducting component fitted with a non-conducting coating |
| 09/30/2009 | EP2104656A2 Composite material part with a silicon-containing ceramic matrix protected against corrosion |
| 09/30/2009 | EP2041400B1 Turbocharger having a catalytic coating |
| 09/30/2009 | EP1660758B1 Method for the production of gas turbine rotors with integrated blading |
| 09/30/2009 | CN101545381A Film cooling of turbine components |
| 09/29/2009 | US7594799 Undercut fillet radius for blade dovetails |
| 09/29/2009 | CA2446590C Structure comprising a rotor and fixed perturbation sources and method for reducing vibrations in said structure |
| 09/24/2009 | WO2009117232A2 Methods allowing for visual inspection of coated components for erosion damage |
| 09/24/2009 | WO2009117231A2 Erosions systems and components comprising the same |
| 09/24/2009 | WO2009117230A2 Methods for making components having improved erosion resistance |
| 09/24/2009 | WO2009116596A1 Coating structure and surface treating method |
| 09/24/2009 | WO2009115728A1 Turbine blade with tip cooling and corresponding turbine and turboengine |
| 09/24/2009 | WO2009115390A1 Guide vane for a gas turbine |
| 09/24/2009 | US20090238695 Full coverage trailing edge microcircuit with alternating converging exits |
| 09/24/2009 | US20090238694 Radial split serpentine microcircuits |
| 09/24/2009 | US20090238693 Substrate With Applied Coating and Production Method |
| 09/24/2009 | US20090238692 Blade of a turbo machine |
| 09/24/2009 | US20090238684 Cooling arrangement for CMC components with thermally conductive layer |
| 09/24/2009 | DE202009008234U1 Adaptive kinematische Segmente für bewegliche Statorschaufeln von Vorleitapparaten in Strömungsmaschinen Adaptive kinematic segments for movable stator blades of Vorleitapparaten in turbomachines |
| 09/24/2009 | DE102008014743A1 Verdichterstator mit Teildeckband Compressor stator with partial shroud |
| 09/24/2009 | CA2717560A1 Methods allowing for visual inspection of coated components for erosion damage |
| 09/24/2009 | CA2717557A1 Methods for making components having improved erosion resistance |
| 09/24/2009 | CA2716993A1 Erosions systems and components comprising the same |
| 09/24/2009 | CA2716543A1 Turbine blade with tip cooling and corresponding turbine and turboengine |
| 09/23/2009 | EP2103782A1 Blade structure for gas turbine |
| 09/23/2009 | EP2103781A2 Full coverage trailing edge microcircuit with alternating converging exits |
| 09/23/2009 | EP2103780A2 Cold air buffer supply tube |
| 09/23/2009 | EP2103779A1 Methods and apparatuses for correcting twist angle in a gas turbine engine blade |
| 09/23/2009 | EP2103384A1 Method for manufacturing a welded blisk |
| 09/23/2009 | EP2102379A1 Method for producing a turbine blade with an oxide on a metallic layer, use of such a turbine blade, a turbine and a method of operating a turbine |
| 09/23/2009 | EP1831504B1 Durable thermal barrier coatings |
| 09/23/2009 | CN101542073A Blade arrangement |
| 09/23/2009 | CN101539058A Closed circuit blade-cooled turbine |
| 09/23/2009 | CN101539056A Method and apparatus for operating gas turbine engine system |
| 09/22/2009 | US7591594 Turbomachine with a compact roller bearing |
| 09/22/2009 | US7591070 Turbine blade tip squealer and rebuild method |
| 09/22/2009 | CA2485458C Gas turbine engine with active tip clearance control |
| 09/22/2009 | CA2445057C Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine |
| 09/22/2009 | CA2398515C Turbine airfoil for gas turbine engine |
| 09/22/2009 | CA2398502C Turbine airfoil for gas turbine engine |
| 09/17/2009 | WO2009113335A1 Tial-based alloy, process for production of the same, and rotor blade comprising the same |
| 09/17/2009 | WO2009112776A2 Blade with non-axisymmetric platform: recess and boss on the extrados |
| 09/17/2009 | WO2009112775A2 Blade with non-axisymmetric platform |
| 09/17/2009 | WO2009112774A2 Blade with 3d platform comprising an inter-blade bulb |
| 09/17/2009 | WO2009112756A1 Method for testing the coating of a vane base |
| 09/17/2009 | WO2009112400A1 Hollow-cast cast part |
| 09/17/2009 | WO2009112242A2 Cover disk for a closed impeller |
| 09/17/2009 | WO2009083456A3 Gas turbine |
| 09/17/2009 | WO2009079470A3 Active film cooling for turbine blades |
| 09/17/2009 | WO2009026928A3 Wind turbine blade with submerged boundary layer control means |
| 09/17/2009 | US20090232661 Turbine blade with multiple impingement cooled passages |
| 09/17/2009 | US20090232660 Blade for a gas turbine |
| 09/17/2009 | US20090232658 Blade having a damping element and method of fabricating same |
| 09/17/2009 | US20090232657 Blade |
| 09/17/2009 | US20090232655 Stamped stator assemblies and methods for assemblying stamped stator assemblies |
| 09/17/2009 | US20090232646 Use of a Thermal Barrier Coating for a Housing of a Steam Turbine, and a Steam Turbine |
| 09/17/2009 | US20090231952 Gas foil impeller |
| 09/17/2009 | CA2716248A1 Blade with non-axisymmetric platform |
| 09/17/2009 | CA2716244A1 Blade with 3d platform comprising an inter-blade bulb |
| 09/17/2009 | CA2716227A1 Method for testing the coating of a vane base |
| 09/17/2009 | CA2714439A1 Blade with non-axisymmetric platform: recess and boss on the extrados |
| 09/16/2009 | EP2101040A2 Turbomachine with multi-flow rotor assembly |
| 09/16/2009 | EP2100687A1 Potential-free wire heating during welding and device for this purpose |
| 09/16/2009 | EP2100032A2 Tidal electricity generating apparatus |
| 09/16/2009 | EP2099585A1 Device and method for the surface peening of a component of a gas turbine |
| 09/16/2009 | EP2099583A1 Method and device for pin removal in a confined space |
| 09/16/2009 | EP2099582A1 Device and method for the repair or production of blade tips of blades of a gas turbine, in particular of an aircraft engine |
| 09/16/2009 | EP1877218B1 Method of repairing a threaded generator rotor blower assembly |
| 09/16/2009 | EP1868763B1 Method for producing and/or repairing an integrally bladed rotor by inductive diffusion welding |
| 09/16/2009 | CN101535602A 涡轮叶片 Turbine blades |
| 09/16/2009 | CN101535601A Turbine blade |
| 09/16/2009 | CN101535600A 涡轮增压器 Turbocharger |
| 09/16/2009 | CN101532399A Blade with a cooling groove for a bladed wheel of a turbomachine |