Patents
Patents for F01D 25 - Component parts, details, or accessories, not provided for in, or of interest apart from, other groups (22,148)
09/2004
09/21/2004US6793458 Turbine frame, turbine assembling method and turbine assembling and transporting method
09/21/2004US6793457 Fabricated repair of cast nozzle
09/21/2004US6793042 Dual independent tank and oil system with single port filling
09/21/2004US6792758 Variable exhaust struts shields
09/21/2004US6792655 Apparatus for correcting airfoil twist
09/21/2004CA2133185C Vertical gas turbine system
09/16/2004US20040181330 Method and apparatus for managing maintenance operations
09/16/2004US20040180233 protective layer of an MCrAlY alloy is applied to the basic body
09/16/2004US20040179935 Seal
09/16/2004US20040177508 Bearing spring plate pedestal and method of installing
09/15/2004EP1457910A2 On-line system and method for processing information relating to the wear of turbine components
09/15/2004EP1457855A1 Methods and apparatus for assessing gas turbine damage
09/15/2004EP1456510A1 Turbine noise absorber
09/15/2004EP1456508A1 Hot gas path subassembly of a gas turbine
09/15/2004EP1456507A1 Sealing module for components of a turbo-engine
09/14/2004US6790002 Steam turbine and power generating equipment
09/14/2004US6790000 Shroud for the roots of variable stator vanes in the high-pressure compressor of a gas turbine
09/14/2004US6789315 Establishing a throat area of a gas turbine nozzle, and a technique for modifying the nozzle vanes
09/10/2004WO2004076821A1 Air thrust bearing for a gas turbine engine
09/10/2004WO2004076820A1 Gas turbine engines
09/09/2004US20040175597 Turbine components with thermal barrier coatings
09/09/2004US20040175264 Method for cooling a turbo machine and turbo machine
09/09/2004US20040175262 Method and apparatus for sealing turbine casing
09/09/2004US20040175260 Structure comprising a rotor and fixed perturbation sources and method for reducing vibrations in said structure
09/09/2004US20040173975 Sealing arrangements
09/09/2004US20040172827 Fan and compressor blade dovetail restoration process
09/09/2004US20040172826 Turbine element repair
09/09/2004US20040172825 Turbine element repair
09/09/2004DE10061846B4 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine
09/08/2004EP1455101A1 Screw and process for making a screw with a protective coating
09/08/2004EP1455066A1 Cooling of a turbine and method therefore
09/08/2004EP1455055A1 Turbomachine with cooled shroud segments
09/08/2004EP1454707A1 Fan and compressor blade dovetail restoration process
09/08/2004CN2639531Y Air chamber low-pressure internal cylinder structure of assembling steam turbine
09/08/2004CN1527922A Coolable segment for a turbomachinery and combustion turbine
09/08/2004CN1526965A Bolt and method for forming protective layer on bolt
09/08/2004CN1526928A Method for cooling turbomachine and turbomachine for applicating the same method
09/08/2004CN1526918A Gas-turbine engine turbon-nozzle arc section with single-branch open cavity hollow blade
09/08/2004CN1526916A Steam turbine and its rotor and method for active colling the same rotor and application of the same method
09/08/2004CN1526915A Steam turbine and method for running steam turbine
09/08/2004CN1165698C Sealing system, esp for sealing device of rotary machine
09/08/2004CN1165672C Exhaust-gas turbo charger with failure fuel tank
09/08/2004CN1165670C Steam turbine
09/07/2004US6787947 Cooling the upstream end plate of a high pressure turbine by means of a system of dual injectors at the end of the combustion chamber
09/07/2004US6787074 Method for removing volatile components from a gel-cast ceramic article
09/07/2004US6786635 Turbine blade (bucket) health monitoring and prognosis using neural network based diagnostic techniques in conjunction with pyrometer signals
09/07/2004US6786488 Seal structure, turbine having the same, and leak-preventing seal system for rotating shaft
09/07/2004US6786052 Insulation system for a turbine and method
09/07/2004US6786051 Trailer mounted mobile power system
09/07/2004CA2087761C High pressure turbine component interference fit up
09/02/2004WO2004074654A1 Integral cooling system for rotary engine
09/02/2004WO2004074653A1 Compact compound engine package
09/02/2004US20040172187 Methods and apparatus for assessing gas turbine engine damage
09/02/2004US20040171330 Apparatus and method for consistently retaining a gas turbine engine blade in a predetermined position and orientation
09/02/2004US20040170499 Gas turbine engine turbine nozzle segment with a single hollow vane having a bifurcated cavity
09/02/2004US20040170498 Gas turbine engine turbine nozzle bifurcated impingement baffle
09/02/2004US20040170496 Turbine nozzle segment cantilevered mount
09/02/2004US20040168786 Method of manufacturing gas turbine part using porous metal
09/02/2004US20040168520 Dynamic pressure probe holder and method of obtaining a dynamic pressure signal
09/02/2004US20040168504 Vehicle ultraviolet gas emission analysis
09/02/2004US20040168443 Methods and apparatus for assembling gas turbine engines
09/02/2004DE10307552A1 Mounting for connecting inner and outer casings of gas turbine consists of radial rings forming bayonet fittings with annular U-shaped fittings on casings which allow them to tip
09/02/2004CA2516717A1 Integral cooling system for rotary engine
09/01/2004EP1452936A2 Method for detecting an impending sensor failure
09/01/2004EP1452802A1 Methods and apparatus for washing gas turbine engine combustors
09/01/2004EP1452694A2 Damper and seal for turbine
09/01/2004EP1452693A2 Turbine nozzle segment cantilevered mount
09/01/2004EP1452692A2 Turbine bucket damper pin
09/01/2004EP1452690A2 Gas turbine engine turbine nozzle bifurcated impingement baffle
09/01/2004EP1452689A1 Gas turbine vane segment having a bifurcated cavity
09/01/2004EP1452688A1 Steam turbine rotor, method and use of actively cooling such a rotor
09/01/2004EP1452275A1 Apparatus and method for consistently retaining a gas turbine engine blade in predetermined position and orientation
09/01/2004EP1452264A1 Method of manufacturing gas turbine part using porous metal
09/01/2004EP1451459A1 High energy particle arrestor for air turbine starters
09/01/2004EP1451458A1 Arrangement at gas turbine
09/01/2004EP1451450A1 Gas turbo group
09/01/2004EP1451449A1 Method and device for minimizing oil consumption in a gas turbine engine
09/01/2004CN1525055A Methods and apparatus for assessing gas turbine damage
09/01/2004CN1525049A Turbine nozzle segment cantilevered mount
09/01/2004CN1525048A Gas turbine engine turbine nozzle bifurcated impingement baffle
09/01/2004CN1525047A Turbine bucket damper pin
08/2004
08/31/2004US6785633 Method and apparatus for assessing performance of combined cycle power-plants
08/31/2004US6783324 Compressor bleed case
08/31/2004US6783321 Diffusing coupling cover for axially joined turbines
08/31/2004US6783319 Method and apparatus for supporting rotor assemblies during unbalances
08/31/2004CA2071363C System for providing early warning of potential water induction events and enabling rapid steam turbine restarts
08/28/2004CA2455673A1 Methods and apparatus for assessing gas turbine engine damage
08/26/2004US20040166003 Method for manufacturing a turbocharger assembly having a thermally decoupled flange
08/26/2004US20040165983 Damper seal
08/26/2004US20040163678 comprises coupling a nozzle assembly against the combustor, wherein the nozzle assembly includes an inlet end, a discharge end, a hollow nozzle body extending therebetween, and a centerbody positioned within the nozzle body
08/26/2004US20040163394 Coolant recovery type gas turbine
08/26/2004US20040163390 Secondary air induction system
08/26/2004DE10303340A1 Kühleinrichtung Cooling device
08/25/2004CN1524160A Securing system for the rotor blades of axial flow turbo engines
08/24/2004US6782314 Method of detecting in-range engine sensor faults
08/24/2004US6779973 Gas turbine
08/24/2004US6779972 Flowpath sealing and streamlining configuration for a turbine
08/24/2004US6779963 Apparatus and method to control force exerted on steam turbines by inlet pipes
08/24/2004US6779597 Multiple impingement cooled structure
08/24/2004US6779336 Cooled variable geometry exhaust nozzle