Patents for B23P 6 - Restoring or reconditioning objects (6,053)
03/2003
03/05/2003EP1287936A1 Repair method for structure and repair welding apparatus
02/2003
02/27/2003US20030037436 Method for repairing an apertured gas turbine component
02/27/2003US20030037427 Vehicle body manufacturing process
02/27/2003US20030037422 Articulated connector reconditioning process and apparatuses
02/26/2003EP1286020A2 Method for repairing an apertured gas turbine component
02/25/2003US6524395 Detecting and measuring light; fluid flow of pressurized water to clear blockages
02/20/2003US20030035728 Apparatus for retaining an internal coating during article repair
02/20/2003US20030034379 Method of repairing superalloy directional castings
02/20/2003US20030033702 Restoration of thickness to load-bearing gas turbine engine components
02/18/2003US6520836 Method of forming a trailing edge cutback for a turbine bucket
02/13/2003US20030029845 Repair method for structure and repair welding apparatus
02/12/2003CN1101294C Method for guiding inner slot end into component
02/05/2003CN1100642C Weld repair process and articles repaired thereby
01/2003
01/22/2003CN1392023A Laser profile repairing process for damaged blade of smoke gas turbine
01/22/2003CN1392022A Laser method for fast repairing damaged area in smoke machine main shaft
01/22/2003CN1392021A Laser repairing process for failed gas compressor rotor
01/21/2003US6508000 Transient liquid phase bonding repair for advanced turbine blades and vanes
01/21/2003CA2056527C Fabrication of cast articles from high melting temperature superalloy compositions
01/16/2003US20030009872 Symmetrical mill
01/16/2003US20030009870 Method of hot peeling for removing a blade leading edge cap
01/07/2003US6504127 Laser consolidation methodology and apparatus for manufacturing precise structures
01/07/2003US6503349 Heating a repair alloy to a temperature that avoids recrystallization and repair zone incipient melting; rapid cooling and aging; stability of mechanical properties; joint strength; fatique; gas turbine high-pressurue vanes
01/07/2003US6502303 Method of repairing a turbine blade tip
01/02/2003US20030002940 Rotary drilling and cutting tools for manufacturing printed circuit boards
01/02/2003US20030000602 Integrally bladed rotor airfoil fabrication and repair techniques
01/02/2003EP1270141A2 Method for repairing cracks in a turbine blade root trailing edge
01/02/2003EP1268120A1 Production, forming, bonding, joining and repair systems for composite and metal components
12/2002
12/26/2002US20020197152 Airfoils with improved oxidation resistance and manufacture and repair thereof
12/26/2002US20020195176 Integrally bladed rotor airfoil fabrication and repair techniques
12/26/2002US20020194733 Method for repairing cracks in a turbine blade root trailing edge
12/26/2002US20020194722 Portable frog milling machine for use with railroad frog reconditioning and welding table
12/24/2002US6497038 Method for roller tappet suspension in an internal combustion engine for removal of a camshaft or other components
12/18/2002EP1267127A1 Method for replacing combustor liner panels
12/18/2002EP1266718A2 Methods for replacing nuggeted combustor liner panels
12/18/2002EP1265726A1 Method for removing a seal
12/18/2002CN1385281A Method for making and repairing wing surface of integral propeller rotator
12/17/2002US6494683 Repaired turbine rotor wheel
12/17/2002US6494677 Turbine nozzle segment and method of repairing same
12/12/2002US20020187044 Turbine airfoil and method for manufacture and repair thereof
12/12/2002US20020187042 Turbine airfoil with separately formed tip and method for manufacture and repair thereof
12/12/2002US20020185198 Repair of single crystal nickel based superalloy article
12/12/2002US20020184763 Methods for replacing nuggeted combustor liner panels
12/12/2002US20020184762 Methods for replacing combustor liner panels
12/10/2002US6491208 Cold spray repair process
12/10/2002US6490899 Method and apparatus for peening tops of cooled blades
12/10/2002US6490791 Method for repairing cracks in a turbine blade root trailing edge
12/05/2002US20020182021 Cutting tool material rod for machining of printed circuit board and method of fabricating the same
12/04/2002EP1262632A1 Turbine airfoil with separately formed tip and method for manufacture and repair thereof
11/2002
11/26/2002US6485655 Method and apparatus for retaining an internal coating during article repair
11/20/2002EP1258312A2 Repair of a single crystal nickel based superalloy article
11/19/2002US6481407 Thin-walled valve guide insert and method for installing same within a cylinder head construction
11/19/2002CA2199691C Method for affixing an addition to a localized zone of a part using a superalloy
11/14/2002WO2002090039A1 Method of repairing a turbin blade tip
11/14/2002US20020166220 Process for repairing a structure
11/14/2002DE10133876C1 Printing machine cylinder re-conditioning method uses tool for inwards or outwards deformation of mantle wall above undercut channel in printing cylinder
11/13/2002EP1214172A4 Laser cladding a turbine engine vane platform
11/13/2002EP1212167A4 Method for replacing a turbine vane airfoil
11/07/2002WO2001096751A9 Thread replacement system and device
11/07/2002US20020162220 Method of repairing a turbine blade tip
11/06/2002EP1254738A2 Automated system for repairing components
10/2002
10/31/2002US20020161483 Automated system for repairing components
10/30/2002EP1253289A2 Integrally bladed rotor airfoil fabrication and repair techniques
10/29/2002US6470544 Hot Peeling device for a blade leading edge cap
10/22/2002US6467339 Method for deploying shroud segments in a turbine engine
10/17/2002US20020148171 Portable facility and process for reconditioning antifriction bearings
10/17/2002US20020148115 Transient liquid phase bonding repair for advanced turbine blades and vanes
10/15/2002US6464424 Repaired shroud assembly for boiling water reactor
10/15/2002US6464128 Braze repair of a gas turbine engine stationary shroud
10/09/2002EP1247003A1 Turbine blade and method of repair
10/03/2002WO2002018673A3 Compound for metal modification and metal surface restoration
09/2002
09/24/2002US6454156 Method for closing core printout holes in superalloy gas turbine blades
09/24/2002US6453533 Method for reconditioning returnable barrels comprised of sheet metal
09/17/2002US6453211 Nominal shift machining
09/12/2002US20020125215 Chemical milling of gas turbine engine blisks
09/12/2002US20020124374 Apparatus and method for reconditioning an automotive wheel
09/11/2002EP1239059A2 Chemical milling of the blades of a gas turbine engine
09/05/2002US20020123827 System and method for performing electronic triage of a turbine part
09/04/2002EP1236864A2 System and method for perfoming electronic triage of a turbine part and for carrying out a turbine part repair
08/2002
08/29/2002US20020119730 Method of forming a trailing edge cutback for a turbine bucket
08/28/2002EP0758284B1 Gas turbine engine vane assembly repair
08/27/2002US6438838 Method for repairing and producing integrally bladed rotors for a turbine or turbo engine
08/21/2002EP0673292B1 Method of repairing the surface of a superalloy part
08/20/2002US6435788 Thread repair insert
08/20/2002US6434823 Method for repairing a coated article
08/14/2002EP1231010A1 Transient liquid phase bonding repair for turbine blades and vanes
07/2002
07/31/2002EP1227218A2 Turbine nozzle segment and method of repairing same
07/11/2002US20020091459 Method for reconditioning blades
07/09/2002US6416709 Which is not a slurry and does not require nickel precoating; precise dimensional repairs on jet engines; laminated; middle layer of metal powder bonded with ptfe fibers, outer layers of braze alloy bonded with fibrillated ptfe; brazing
07/09/2002US6416278 Turbine nozzle segment and method of repairing same
07/02/2002US6413650 Method for repairing superalloy castings using a metallurgically bonded tapered plug
07/02/2002US6412684 High pressure chemical reactors; stainless steel plates
06/2002
06/25/2002US6408512 Method of correcting deformed turbine blades
06/20/2002US20020073541 Method for removing stuck locking pin in turbine rotor
06/20/2002DE10030776C2 Verfahren zur Instandsetzung von metallischen Bauteilen insbesondere für Gasturbinen A method for repair of metallic components in particular for gas turbines
06/19/2002EP1214172A1 Laser cladding a turbine engine vane platform
06/19/2002CN1354066A Method for repairing curved section of nozzle guide device
06/18/2002US6405435 Process for producing or repairing cooling channels in monocrystalline components of gas turbines
06/13/2002WO2001094069A3 A method of repairing a reactor coolant pump shaft and a reactor coolant pump repaired by such method
06/12/2002EP1212167A1 Method for replacing a turbine vane airfoil
06/12/2002CN2494728Y Reconditioning damaged engine cylinder
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