| 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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| 06/19/2008 | CA2671733A1 Device and method for the surface peening of a component of a gas turbine |
| 06/18/2008 | EP1933007A2 Gas turbine guide vanes with tandem airfoils and fuel injection and method of use |
| 06/18/2008 | EP1932936A1 Method for coating a component |
| 06/18/2008 | EP1932935A1 Method for the manufacture of a turbine blade with an oxide layer on a metallic coating, a turbine blade and its use, and a method for the operation of a turbine. |
| 06/18/2008 | EP1931814A1 Device for internal coating, retorts and method of internal coating |
| 06/18/2008 | CN101199987A Fixture for positioning gas turbine engine components |
| 06/18/2008 | CN100395432C Recirculation structure for turbo chargers |
| 06/17/2008 | US7388980 Process and apparatus for locating coated cooling holes on turbine vanes |
| 06/17/2008 | US7387690 brazing paste containing a first nickel, boron and chromium alloy with a second nickel based alloy for applying to a crack; brazing paste containing a first nickel, boron and chromium alloy with a second nickel based alloy and applying to a crack |
| 06/17/2008 | US7387495 High efficiency rotor for the first phase of a gas turbine |
| 06/17/2008 | US7387494 Finger dovetail attachment between a turbine rotor wheel and bucket for stress reduction |
| 06/17/2008 | US7387493 Impeller with widened blades |
| 06/17/2008 | US7387490 High efficiency stator for the first phase of a gas turbine |
| 06/17/2008 | US7387487 Turbomachine with fluid supply |
| 06/17/2008 | CA2437758C Thermal barrier coatings with low thermal conductivity |
| 06/17/2008 | CA2398339C Simultaneous offset dual sided laser shock peening using low energy laser beams |
| 06/17/2008 | CA2364931C Bolted joint for rotor disks and method of reducing thermal gradients therein |
| 06/17/2008 | CA2363669C Turbine interstage sealing ring |
| 06/17/2008 | CA2363363C Cooling system for gas turbine stator nozzles |
| 06/17/2008 | CA2359342C Electrochemical stripping of turbine blades |
| 06/17/2008 | CA2358673C Method and apparatus for reducing rotor assembly circumferential rim stress |
| 06/17/2008 | CA2356766C Method and apparatus for supporting rotor assemblies during unbalances |
| 06/17/2008 | CA2352698C Method of adjusting component airflow |
| 06/15/2008 | CA2612810A1 Airfoil leading edge end wall vortex reducing plasma |
| 06/15/2008 | CA2612533A1 Plasma induced virtual turbine airfoil trailing edge extension |
| 06/12/2008 | WO2008068069A1 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 |
| 06/12/2008 | WO2008067962A2 Repairs and/or changes in contour of a form surface of a form tool |
| 06/12/2008 | WO2008067633A1 Method of machining airfoils by disc tools |
| 06/12/2008 | US20080138209 High aspect ratio blade main core modifications for peripheral serpentine microcircuits |
| 06/12/2008 | US20080138208 Core for use in a casting mould |
| 06/12/2008 | US20080134503 Methods and systems for assembling gas turbine engine fan assemblies |
| 06/12/2008 | DE102007056315A1 Beschichtungssysteme mit Schichten auf Rhodiumaluminid-Grundlage Coating systems with layers on Rhodiumaluminid Foundation |
| 06/12/2008 | CA2669582A1 Vane ring, and method for the production thereof |
| 06/11/2008 | EP1930600A2 Advanced booster stator vane |
| 06/11/2008 | EP1930599A2 Advanced booster system |
| 06/11/2008 | EP1930598A2 Advanced booster rotor blade |
| 06/11/2008 | EP1930550A2 Systems for cooling integral turbine nozzle and shroud assemblies |
| 06/11/2008 | EP1930548A2 Ceramic matrix composite articles having small complex features |
| 06/11/2008 | EP1930547A2 Compressor blade for a gas turbine engine |
| 06/11/2008 | EP1930546A2 Airfoil with plasma generator for shielding a boundary layer upstream of a film cooling hole and corresponding operating method |
| 06/11/2008 | EP1930545A2 Airfoil with plasma generator for shielding a boundary layer downstream of a film cooling hole and corresponding operating method |
| 06/11/2008 | EP1930544A1 Turbine blade |
| 06/11/2008 | EP1930477A1 Method for selectively removing coatings from metal substrates |
| 06/11/2008 | EP1930455A1 Nickel-base superalloy with excellent unsusceptibility to oxidation |
| 06/11/2008 | EP1930450A2 Component with residual compressive stress |
| 06/11/2008 | EP1930116A2 Method of diffusion brazing with nonoparticle alloys |
| 06/11/2008 | EP1930097A1 A core for use in a casting mould |
| 06/11/2008 | EP1929126A1 Method of producing a gas turbine component to be coated having exposed openings, apparatus for carrying out the method, and coatable turbine blade having a film-cooling opening |
| 06/11/2008 | EP1529153B1 Turbine blade having angled squealer tip |
| 06/11/2008 | CN201071737Y Vacuum electron beam soldering turbine shaft |
| 06/11/2008 | CN101198768A Rotor for steam turbine and process for producing the same |
| 06/11/2008 | CN101198713A Layer system for a component comprising a thermally insulating layer and a metallic anti-erosion layer, method for the production and method for the operation of a steam turbine |
| 06/10/2008 | US7384244 Fatigue-resistant components and method therefor |
| 06/10/2008 | US7384243 Stator vane profile optimization |
| 06/10/2008 | US7384241 Fan with ring and method of producing the same |
| 06/10/2008 | US7384240 Composite blade |
| 06/10/2008 | CA2393389C Shear pin with locking cam |
| 06/10/2008 | CA2364321C Centrifugal air flow control |
| 06/05/2008 | WO2008064868A2 Turbocharger |
| 06/05/2008 | WO2008039216A3 Turbocharger turbine and shaft assembly |
| 06/05/2008 | US20080131699 Thermally insulating layer incorporating a distinguishing agent |
| 06/05/2008 | US20080131285 RMC-defined tip blowing slots for turbine blades |
| 06/05/2008 | US20080131284 Air-cooled component |
| 06/05/2008 | US20080131271 Advanced booster stator vane |
| 06/05/2008 | US20080131267 Variable Nozzle Turbocharger |
| 06/05/2008 | US20080131265 Downstream plasma shielded film cooling |
| 06/05/2008 | US20080131263 Methods and system for shielding cooling air to facilitate cooling integral turbine nozzle and shroud assemblies |
| 06/05/2008 | US20080131262 Methods and system for cooling integral turbine nozzle and shroud assemblies |
| 06/05/2008 | US20080131261 Method and system to facilitate enhanced local cooling of turbine engines |
| 06/05/2008 | US20080128475 Nickel-based braze alloy compositions and related processes and articles |
| 06/05/2008 | US20080127491 Method and system to facilitate preferentially distributed recuperated film cooling of turbine shroud assembly |
| 06/05/2008 | DE102007003035A1 Internal-combustion engine e.g. petrol engine, has turbocharger including compressor with surge line, and compressor wheel including blade with channel formed from pressing side of blade to suction side of blade in flow-through manner |
| 06/04/2008 | EP1927774A1 Device for connecting two rotating shafts, in particular in a turbomachine |
| 06/04/2008 | EP1927732A2 Articles comprising composite structures having mounting flanges |
| 06/04/2008 | EP1927728A2 Methods for reducing stress on composite structures |
| 06/04/2008 | EP1927727A2 Turbine blade and turbine blade cooling system and methods |
| 06/04/2008 | EP1927726A1 An air-cooled component |
| 06/04/2008 | EP1927725A2 System to facilitate preferentially distributed recuperated film cooling of turbine shroud assembly |
| 06/04/2008 | EP1927724A2 Turbomachine blade |
| 06/04/2008 | EP1927723A1 Stator stage of an axial compressor in a flow engine with transverse fins to increase the action |
| 06/04/2008 | EP1927722A1 Rotary assembly components and methods of fabricating such components |
| 06/04/2008 | EP1927675A1 Ceramic corrosion resistant coating for oxidation resistance |
| 06/04/2008 | EP1927414A2 RMC-Defined tip blowing slots for turbine blades |
| 06/04/2008 | CN101191424A Turbine blade and turbine blade cooling system and methods |
| 06/04/2008 | CN101191423A Rotary assembly components and methods of fabricating such components |
| 06/04/2008 | CN100392152C Method for removing a layer area of a component |
| 06/04/2008 | CN100392150C Method of adopting inorganic seriflux mixture for applicating coating contg aluminium |
| 05/30/2008 | CA2612744A1 Method for making a laser hole in a part made of composite material with ceramic matrix, hole obtained by the method, composite material with ceramic matrix comprising said hole, turboreactor comprising said part |
| 05/30/2008 | CA2611339A1 Advanced booster rotor blade |
| 05/30/2008 | CA2611336A1 Advanced booster system |
| 05/30/2008 | CA2610541A1 Advanced booster stator vane |
| 05/29/2008 | WO2008062566A1 Mixed flow turbine, or radial turbine |
| 05/29/2008 | WO2008062051A1 Non wetable surface coating of steam turbine parts which work in wet steam |
| 05/29/2008 | WO2008061856A1 Blade arrangement |
| 05/29/2008 | WO2006133363A3 Impeller with machining access panel |
| 05/29/2008 | US20080124225 Turbine Blade for a Gas Turbine, Use of a Turbine Blade and Method for Cooling a Turbine Blade |
| 05/29/2008 | US20080124223 Hp turbine vane airfoil profile |
| 05/29/2008 | US20080124222 Heater assembly for deicing and/or anti-icing a component |
| 05/29/2008 | US20080124221 Lp turbine vane airfoil profile |
| 05/29/2008 | US20080124220 Lp turbine blade airfoil profile |