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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07/19/1988 | CA1239381A1 Radial type ceramic turbine rotor and method of producing the same |
07/14/1988 | WO1988005121A1 Interblade seal for turbomachine rotor |
07/14/1988 | WO1988005086A1 Heat-resistant steel and gas turbine made of the same |
07/13/1988 | CN87101148A "v" notched integrally shrouded trubine blade and method for determining shroud tightness and wear of circular array of rotating blades disposed in rotor |
07/06/1988 | EP0273854A2 Abrasive material, especially for turbine blade tips |
07/06/1988 | EP0273852A2 Turbine blade having a fused metal-ceramic abrasive tip |
07/05/1988 | US4754983 Sealing apparatus between rotatable coaxial inner and outer shafts of a gas turbine engine |
06/30/1988 | WO1988004722A1 Turbine rotor cooling |
06/29/1988 | EP0272966A1 Disc connecting system for the rotor of a turbo machine |
06/28/1988 | US4753575 Turbine blade |
06/27/1988 | EP0173715A4 Method and apparatus for the gas jet deposition of conducting and dielectric thin solid films and products produced thereby. |
06/21/1988 | US4752186 Coolable wall configuration |
06/21/1988 | US4751962 Temperature responsive laminated porous metal panel |
06/15/1988 | EP0270723A1 Impeller for a radial turbomachine |
06/15/1988 | EP0270554A1 Method for manufacturing metallic products from powder by hot isostatic pressing using ceramic cores. |
06/14/1988 | US4751123 Process for manufacturing a turbine or compressor wheel made of composite material and wheel thus obtained |
06/14/1988 | CA1237990A1 Abrasive surfaced article for high temperature service |
06/08/1988 | EP0270403A1 Propulsion engine with contrarotating power turbines |
06/07/1988 | US4749334 Ceramic rotor-shaft attachment |
06/01/1988 | EP0269551A2 Methods for weld repairing hollow, air cooled turbine blades and vanes |
05/31/1988 | US4747900 Method of manufacture of compressor rotor assembly |
05/31/1988 | US4747722 Metal-ceramic fitting assembly |
05/31/1988 | CA1237449A1 Sintered dense silicon carbide |
05/31/1988 | CA1237370A1 Captured radial key for steam turbine wheels |
05/18/1988 | EP0267810A2 Idler disk |
05/18/1988 | EP0267718A2 Airfoil with diffused cooling holes and method and apparatus for making the same |
05/18/1988 | EP0267478A2 Gas turbine jet engine with a high pressure compressor |
05/18/1988 | EP0267405A2 Radial-flow turbo machine |
05/17/1988 | US4744725 Abrasive surfaced article for high temperature service |
05/17/1988 | US4744214 Engine modularity |
05/11/1988 | EP0267097A1 Blade-carrying ring for a fan with a large diameter |
05/11/1988 | EP0266954A2 Twisted hollow airfoil with non-twisted internal support ribs |
05/10/1988 | US4743733 Method and apparatus for repairing metal in an article |
05/10/1988 | US4743514 Nickel base alloy |
05/10/1988 | US4743462 Method for preventing closure of cooling holes in hollow, air cooled turbine engine components during application of a plasma spray coating |
05/10/1988 | US4743166 Blade root seal |
05/10/1988 | US4743165 Disk with superalloy composition different from that of seal alloy |
05/10/1988 | US4743164 Interblade seal for turbomachine rotor |
05/04/1988 | EP0266299A2 Thermal barrier coating system |
05/04/1988 | EP0266298A2 Reduced loss swept supersonic fan blade |
05/04/1988 | EP0266297A2 Cooling air manifold for a gas turbine engine |
05/04/1988 | EP0266235A1 Turbo machine with an automatic controlling device for the turbine ventilation flows |
05/03/1988 | US4741667 Stator vane |
05/03/1988 | US4741665 Guide vane ring for turbo-engines, especially gas turbines |
05/03/1988 | US4741205 "V" notched integrally shrouded turbine blade and method for determining shroud tightness and wear of a circular array of rotating blades disposed in a rotor |
05/03/1988 | US4741153 System for controlling heat expansion and thermal stress in a gas turbine disk |
05/02/1988 | EP0247139A4 Wind turbine system using a savonius-type rotor. |
04/27/1988 | EP0264654A1 Zircomium nitride coated article and method for making same |
04/26/1988 | US4740399 Metal-ceramic composite bodies |
04/26/1988 | CA1235633A1 Metal.sup..ceramics composite article and a method of producing the same |
04/26/1988 | CA1235583A1 Processes of intensification of the thermoenergetical cycle and air jet propulsion engines |
04/19/1988 | US4738902 Silicon carbide fiber reinforced glass |
04/19/1988 | US4738588 Film cooling passages with step diffuser |
04/19/1988 | US4738587 Cooled highly twisted airfoil for a gas turbine engine |
04/19/1988 | US4738586 Compressor blade tip seal |
04/19/1988 | US4738561 Device for protecting wheel discs shrink-fitted on shafts against rotation relative to the shafts and method for manufacturing the same |
04/19/1988 | CA1235375A1 Turbine rotor units and method of producing the same |
04/13/1988 | EP0263713A1 Method for repairing by solid state diffusion metal parts having damaged holes |
04/12/1988 | US4737709 Apparatus for measuring axial movement of a rotating member |
04/12/1988 | US4737613 Laser machining method |
04/12/1988 | US4737077 Profiled blade of a fan and its application in motor-driven ventilating devices |
04/12/1988 | US4737076 Means for maintaining concentricity of rotating components |
04/12/1988 | US4736504 Alignment method for pressure welded bladed disk |
04/12/1988 | CA1235073A1 Stationary blade assembly for a steam turbine |
04/12/1988 | CA1235072A1 Fabricated blade with spanwise cooling passages for gas turbine |
04/12/1988 | CA1235071A1 Seal ring means for a bladed rotor assembly |
04/12/1988 | CA1235069A1 Dual alloy radial turbine rotor with hub material exposed in saddle regions of blade ring |
04/06/1988 | EP0263002A1 Sealing and locking device for the vanes of a turbo machine |
04/05/1988 | US4735656 Abrasive material, especially for turbine blade tips |
03/30/1988 | EP0261460A2 Turbo machine with transsonic stages |
03/29/1988 | US4734010 Damping element for independent turbomachine blades |
03/29/1988 | US4734007 Fan casing and fan blade loading/unloading |
03/22/1988 | US4732538 Blade hub air scoop |
03/16/1988 | EP0260175A1 Profiled propeller blade and its use in motor-driven fans |
03/16/1988 | EP0259718A2 Process for bonding together separate building elements |
03/15/1988 | US4730984 Bladed rotor structure having bifurcated blade roots |
03/15/1988 | US4730983 System for attaching a rotor blade to a rotor disk |
03/15/1988 | US4730982 Assembly for controlling the flow of cooling air in an engine turbine |
03/15/1988 | US4730978 Cooling air manifold for a gas turbine engine |
03/09/1988 | EP0258754A2 Turbine blade with a cooling insert |
03/09/1988 | EP0258440A1 Rotor of centrifugal compressor |
03/08/1988 | US4730093 Method and apparatus for repairing metal in an article |
03/08/1988 | US4729799 Nickel |
03/08/1988 | CA1233752A1 Turbine rotor for gas turbine engine |
03/08/1988 | CA1233705A1 Spalling and corrosion resistant ceramic coating for land and marine combustion turbines |
03/02/1988 | EP0257319A1 Method of producing protective coatings |
03/02/1988 | EP0257140A1 Nuclear reactor coolant pump impeller/shaft assembly |
03/01/1988 | US4728258 Turbine engine component and method of making the same |
02/23/1988 | US4726737 Reduced loss swept supersonic fan blade |
02/23/1988 | US4726735 Film cooling slot with metered flow |
02/23/1988 | US4726104 Methods for weld repairing hollow, air cooled turbine blades and vanes |
02/23/1988 | US4726101 Using a tape containing a powder metal alloy with a fugitive binder and adhesive backing |
02/23/1988 | CA1233146A1 Multi stage centrifugal impeller |
02/23/1988 | CA1233126A1 Gas turbine bladed disk assembly |
02/23/1988 | CA1233125A1 Air control means |
02/23/1988 | CA1233124A1 Steam turbine diaphragm |
02/18/1988 | DE3627779A1 Renovated turbine component |
02/16/1988 | US4725200 Apparatus and method for reducing relative motion between blade and rotor in steam turbine |
02/09/1988 | US4723889 Turbomachine rotor disc assembly |
02/04/1988 | DE3724626A1 Coated blade for steam turbines and coating method to be used therefor |