Patents for B23P 6 - Restoring or reconditioning objects (6,053)
07/2005
07/28/2005US20050160580 Tool setting apparatus for use in reconditioning of articulated connector
07/28/2005US20050160579 Pivot gauge appartus for measuring male articulated connector
07/28/2005US20050160578 Drop-in bore gauge apparatus for female articulated connector
07/28/2005US20050160577 Apparatus and method for aligning female connector in fixture for use in reconditioning of articulated connector
07/21/2005US20050158460 Method for protecting new/used engine parts
07/21/2005DE202005008299U1 Tool for straightening dents, in an automobile bodywork, has a pull rod with a grip within a hollow sleeve for adhesive at the rod end to bond with the metal and pull the dent straight
07/21/2005DE10360063A1 Removal of protective coating from gas turbine blades involves heating to point where particles can be sucked or blown off
07/20/2005CN2710822Y Means for repairing half-axis sleeve screw thread of motor vehicle
07/20/2005CN1640613A Apparatus and method for repairing workpiece with meshing teeth
07/19/2005US6919956 Method of automatically repairing cracks and apparatus for use in such method
07/14/2005US20050150095 Methods of generator rotor removal in a combined-cycle stag application
07/13/2005EP1268120A4 Production, forming, bonding, joining and repair systems for composite and metal components
07/13/2005CN1638897A Method of removing casting defects
07/12/2005US6916387 Repairing a void on a nickel or cobalt base superalloy investment casting by vibrating the casting before repairing; vibrating the casting while filling the void; impinging each incremental deposit with a cooling gas
07/05/2005US6915236 Method and system for automated repair design of damaged blades of a compressor or turbine
07/05/2005US6914210 Method of repairing a stationary shroud of a gas turbine engine using plasma transferred arc welding
07/05/2005US6913442 Internal coating on an internal passage wall exposed at a passage opening through an article external surface is protected from removal during repair of the article, including removal of at least a portion of an external coating, by a
06/2005
06/30/2005US20050139581 High-strength superalloy joining method for repairing turbine blades
06/29/2005EP1432847B8 Method for removing at least one area of a layer of a component consisting of metal or a metal compound
06/28/2005US6912446 Systems and methods for automated sensing and machining for repairing airfoils of blades
06/23/2005US20050132569 Method of repairing a part using laser cladding
06/22/2005EP1543912A1 Method of machining a component and component
06/22/2005CN1207126C Pile-up welding for repairing toothed wheel and shaft of oil-pumping machine
06/21/2005US6908657 Coated component with through-hole having improved surface finish
06/21/2005US6907918 Deformable end cap for heat pipe
06/16/2005WO2005053892A1 Method for producing a piece or the part thereof provided with a weld deposit and a piece produced by said method
06/16/2005US20050126664 Subjecting superalloy turbine blade or nozzle to a first hot isostatic pressing, deliverying weld fillers to metallic component, sealing microcracking by exposing to a second hot isostatic pressing; welding
06/16/2005US20050126001 Process for removing thermal barrier coatings
06/15/2005EP1541714A1 Method for repairing components using environmental bond coatings and resultant repaired components
06/15/2005EP1540026A1 Property recovering method for nickel superalloy
06/14/2005US6905728 Repair degradation in turbine blades; heating to fusion temperature; impacting with paticles; deformation surfaces; vacuum sintering; hot isotactic pressing
06/14/2005US6905308 Turbine nozzle segment and method of repairing same
06/14/2005US6904676 Methods for replacing a portion of a combustor liner
06/14/2005CA2104521C Method for metallurgical enhancement of a failed bolt hole
06/09/2005US20050120555 Process for repairing metallic pieces especially turbine blades of a gas turbine motor
06/09/2005DE10337971A1 Verfahren zur Erhöhung der Festigkeit und/oder Belastbarkeit von Werkstücken A method for increasing the strength and / or resilience of workpieces
06/08/2005EP1450987B1 Method and device for polishing the surface of a gas turbine blade
06/07/2005US6902096 Method of joining material
06/02/2005US20050118330 Method of fabricating or repairing an assembly
06/01/2005EP1535692A1 A method of fabricating or repairing an assembly
06/01/2005EP1534450A1 Method for closing an aperture in a component
05/2005
05/26/2005WO2005046927A1 Gas turbine and rotating blade for a turbomachine
05/26/2005US20050109816 Bonding fixture
05/25/2005EP1533396A2 Method for repairing coated components using NiAl bond coats
05/25/2005EP1533071A2 Method for repairing gas turbine rotor blades
05/24/2005US6895653 Methods for repairing water-cooled generator stator bar clips
05/19/2005WO2005045198A2 A turbine blade and a method of manufacturing and repairing a turbine blade
05/19/2005US20050106998 Method of determining shape data
05/19/2005US20050106316 High pressure turbine blades; nickel substrate overcoated with ceramic heat barrier; diffusion bonding using aluminum intermetallics
05/19/2005US20050106315 Method for repairing components using environmental bond coatings and resultant repaired components
05/19/2005US20050102835 Method for repairing gas turbine rotor blades
05/19/2005DE10336589B3 Repair method for carrier structure, e.g. frame construction of automobile body, has replacement profile section for damaged profile section joined to original profile section via cold-joining method
05/18/2005EP1531232A2 Method for repairing a high pressure turbine blade
05/17/2005US6892931 Methods for replacing portions of turbine shroud supports
05/17/2005US6892930 Process for reconditioning worn or out-of-spec components
05/14/2005CA2487503A1 Method for repairing gas turbine rotor blades
05/12/2005US20050098608 Process for manufacturing or repairing a monobloc bladed disc
05/12/2005US20050098243 applying coatings to the surface of turbines by a hyper-velocity oxyfuel (HVOF) or a low-pressure plasma spray (LPPS) and heating to a high temperature to diffusion bond the coating to the surface
05/11/2005EP1529925A2 Method and apparatus for arresting a crack within a ceramic matrix composite body
05/11/2005CN1614526A Method for profiling involute straight teeth conical gear
05/05/2005US20050091848 Turbine blade and a method of manufacturing and repairing a turbine blade
05/05/2005US20050091847 Method for repairing gas turbine compressor rotor blades
05/05/2005US20050091846 Method and apparatus for rebuilding gas turbine engines
05/05/2005US20050091816 Wallpaper seam repair tool
05/05/2005US20050091815 Manipulator needle portion repairing method and needle set
05/04/2005EP1527845A2 Method for repairing gas turbine compressor rotor blades
04/2005
04/28/2005WO2005037483A1 Method for production of a coating system
04/27/2005EP1525942A1 Gas turbine engine and moving blade for a turbomachine
04/27/2005CN1608794A Repairing method for crack in bottom of large inflammable and explosive medium storing tank
04/21/2005WO2005035177A1 Weld structure having excellent brittle crack propagation resistance and method of welding the weld structure
04/21/2005US20050084368 Repair method for a blade of a turbomachine
04/21/2005US20050082039 Deformable end cap for heat pipe
04/21/2005US20050081354 Method and apparatus for rivet removal and in-situ rehabilitation of large metal structures
04/14/2005DE10343760A1 Process for repairing a rotor of a compressor comprises inserting a profiled groove into the surface of a replacement blade section before welding so that the groove corresponds to the shape and size of a blunt section
04/13/2005EP1522375A1 Method for producing a multilayered system
04/13/2005EP1522369A1 Method of repairing metal articles, preferably blades of gas turbines
04/13/2005CN1605715A Method of repairing metal articles, preferably blades of gas turbines
04/06/2005CN2690095Y Software program control mold welder
03/2005
03/31/2005US20050067466 Crack repair method
03/31/2005US20050067065 From an article with an oriented microstructure by locating and locally melting the defect, and then epitaxially solidifying the melt; cobalt or nickel super alloy for gas turbines
03/31/2005DE10340827A1 Reparaturverfahren für eine Schaufel einer Strömungsarbeitsmaschine Repair method for a blade of a turbomachine
03/30/2005EP1518637A1 Apparatus and method for the repair of heat exchangers, especially for the repair of heat exchanger tubings
03/30/2005EP1517762A2 Diffusion bond mixture for healing single crystal alloys
03/23/2005EP1516690A1 Method of manufacturing or repairing a bladed rotor disc
03/23/2005CN1599655A Method and device for polishing the surface of a gas turbine blade
03/17/2005US20050059321 Method and device for polishing the surface of a gas turbine blade
03/09/2005EP1512490A2 Repairing method for a blade of a turbomachine
03/09/2005EP1432847B1 Method for removing at least one area of a layer of a component consisting of metal or a metal compound
03/03/2005WO2005018954A2 Wheel reconditioning station and method of use
03/03/2005WO2005018865A1 Method for increasing the stability and/or load carrying ability of work pieces by means of friction welding
03/03/2005CA2535823A1 Method for increasing the stability and/or load carrying ability of work pieces by means of friction welding
02/2005
02/24/2005US20050040698 Wheel reconditioning station and method of use
02/24/2005US20050039328 Wheel reconditioning station and method of use
02/23/2005CN1584104A Turbine element repair
02/23/2005CN1584103A Turbine element repair
02/23/2005CN1190295C Repair of single crystal nickel superalloy part
02/22/2005CA2438429A1 Method of re-building francis turbine runners
02/10/2005US20050033555 Method and system for automated repair design of damaged blades of a compressor or turbine
02/10/2005US20050029235 Method for the restoration of damaged areal components
02/09/2005EP1505169A1 Ion plating method
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