Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
04/2004
04/28/2004EP1413714A2 Guide vane for a turbine
04/28/2004EP1413713A2 Self-aspirating high-area-ratio interstage turbine duct assembly for use in a gas turbine engine
04/28/2004EP1413712A1 Shrouded turbine blade with tip sealing
04/28/2004EP1413711A1 Process and device for cooling of gas turbine rotor blades
04/28/2004EP1412547A1 Sintered tin-containing cobalt-based and nickel-based alloys
04/28/2004EP1212167B1 Method for replacing a turbine vane airfoil
04/28/2004EP1198619B1 Bond coats for turbine components and method of applying the same
04/28/2004EP1017510A4 Method and apparatus for gas phase coating complex internal surfaces of hollow articles
04/28/2004EP0944767B1 Process for preparing an abradable seal, abradable seal, and gas turbine engine component comprising such an abradable seal
04/28/2004CN1147662C Design mehtod of radial and mixed flow cylinder face sesant element three-dimensional impeller
04/28/2004CN1147375C Radial and mixed-flow three-component blade wheel single-shaft feed milling process
04/27/2004US6727459 Method for metal deposition on an edge
04/27/2004US6726452 Turbine blade arrangement
04/27/2004US6726448 Ceramic turbine shroud
04/27/2004US6726445 Reduced noise fan stationary blade
04/27/2004US6726444 Hybrid high temperature articles and method of making
04/27/2004US6725540 Method for repairing turbine engine components
04/27/2004CA2195500C Mobile fan blade designed for safety
04/23/2004CA2446035A1 Flow directing device
04/22/2004WO2004033871A2 Leak resistant vane cluster
04/22/2004US20040076540 Welding material, gas turbine blade or nozzle and a method of repairing a gas turbine blade or nozzle
04/22/2004US20040076523 Method and apparatus for facilitating preventing failure of gas turbine engine blades
04/22/2004US20040076521 Undercut leading edge for compressor blades and related method
04/22/2004US20040076520 Turbine and stationary blade for a turbine
04/22/2004US20040076519 High effectiveness cooled turbine vane or blade
04/22/2004US20040076511 Gas turbine
04/22/2004US20040076437 Two stage optical amplifier
04/22/2004US20040075026 Advanced high turning compressor airfoils
04/22/2004US20040074873 Process for removing aluminosilicate material from a substrate, and related compositions
04/22/2004US20040074572 Method and device for hardening a metal component by plasma pulse technology
04/22/2004US20040074093 Apparatus and methods for repairing compressor airfoils in situ
04/22/2004DE10346666A1 Compressor vane profile with high diversion for compressing gas, has curvature of external bulge at maximum from 10 to 35 per cent vane chord length
04/22/2004DE10247031A1 Device for sealing gap between rotating and stationary components of rotary flow machine e.g. gas turbines, has honeycomb structure each side of gap, with cells of one honeycomb structure differing cross sectionally from cells of other
04/21/2004EP1411210A1 Method of depositing an oxidation and fatigue resistant MCrAIY-coating
04/21/2004EP1411209A2 Cooled stationary blades in a gas turbine
04/21/2004EP1411208A1 Compressor blade with unloaded leading edge and method of unloading the leading edge of a compressor blade
04/21/2004EP1411149A1 Process for stripping coatings from components
04/21/2004EP1411136A1 Ni-BASE SINTERED ALLOY
04/21/2004EP1410873A2 Apparatus and methods for repairing compressor airfoils in situ
04/21/2004EP1410872A1 Welding material, gas turbine blade or nozzle and a method of repairing a gas turbine blade or nozzle
04/21/2004EP1409926A1 Baffle cooling device
04/21/2004EP1409848A1 Third-stage turbine nozzle airfoil
04/21/2004EP1409847A1 First-stage high pressure turbine bucket airfoil
04/21/2004EP1409846A1 Second-stage turbine nozzle airfoil
04/21/2004EP1409098A2 Shaped element for aerodynamic or hydrodynamic parts
04/21/2004EP1181437B1 Steam turbine component and method for producing a protective coating on the component
04/21/2004CN1491292A Method for plasma coating turbine blade and coating device
04/21/2004CN1490497A 燃气轮机 Gas turbine
04/21/2004CN1490496A Gas turbine disc rim with air cooling duct shortened axially and declined peripherily
04/20/2004US6723951 Method for reestablishing holes in a component
04/20/2004US6722853 Airfoil shape for a turbine nozzle
04/20/2004US6722852 Third stage turbine bucket airfoil
04/20/2004US6722851 Internal core profile for a turbine bucket
04/20/2004US6722848 Turbine nozzle retention apparatus at the carrier horizontal joint face
04/20/2004US6722134 Linear surface concavity enhancement
04/20/2004US6722119 Turbojet power plant with heat exchanger
04/20/2004CA2070099C Freestanding mixed tuned steam turbine blade
04/15/2004WO2004031573A1 Hydraulic machine rotor
04/15/2004WO2004030858A1 Device and method for machining surfaces of workpieces
04/15/2004US20040072014 Method for providing turbulation on the inner surface of holes in an article, and related articles
04/15/2004US20040071544 Method and apparatus for retrofitting a steam turbine and a retrofitted steam turbine
04/15/2004US20040069748 Electrochemical process for the simultaneous stripping of diverse coatings from a metal substrate
04/15/2004US20040069380 Nickel-based superalloy having high resistance to hot-corrosion for monocrystalline blades of industrial turbines
04/15/2004DE10344843A1 Integrierte Rotier-Messerkanten-Injektionsanordnung Integrated Rotier knife edge injection assembly
04/15/2004DE10245396A1 Vorrichtung und Verfahren zur Oberflächenbearbeitung von Werkstücken Apparatus and method for surface treatment of workpieces
04/15/2004CA2499830A1 Hydraulic machine rotor
04/14/2004EP1408634A2 Two stage optical amplifier
04/14/2004EP1408201A2 Steam turbine inspecting method
04/14/2004EP1408199A1 Leak resistant vane cluster
04/14/2004EP1408197A1 Method for forming abrasion-resistant layer for moving blade, abrasion-resistant layer and method for regeneration thereof, and gas turbine
04/14/2004EP1408196A2 Method of forming cooling apertures in airfoil-shaped blades
04/14/2004EP1408134A1 Method for repairing ni base alloy component
04/14/2004EP1408133A1 Member coated with thermal barrier coating film and thermal spraying powder
04/14/2004EP1407852A2 Process for machining axial blade slots in turbine disks for jet engines
04/14/2004EP1407193A1 Coolable segment for a turbomachinery and combustion turbine
04/14/2004EP1407158A2 Enhanced capacity bearing
04/14/2004EP1407130A1 Jet engine using exhaust gas
04/14/2004EP1407126A1 Means for wear reduction in a gas turbine combustor
04/14/2004EP1327006B1 Austenitic nickel/chrome/cobalt/molybdenum/tungsten alloy and use thereof
04/14/2004EP1276972B1 Turbine
04/14/2004EP1068428B1 Apparatus for cooling a gas turbine airfoil and method of making same
04/14/2004CN1488839A Cooling structure of stationary blade, and gas turbine
04/13/2004US6720567 Apparatus and method for focal point control for laser machining
04/13/2004US6719529 Gas turbine blade and method for producing a gas turbine blade
04/13/2004US6719528 Stator vane arrangement for rotating machinery
04/09/2004CA2444177A1 The electrical process for the simultaneous stripping of diverse coatings from a metal substrate
04/08/2004WO2004029417A1 Blade retention scheme using a retention tab
04/08/2004WO2004029416A1 Turbine blade turbulator cooling design
04/08/2004WO2004029415A1 Heat-tolerant vortex-disrupting fluid guide arrangement
04/08/2004WO2004029330A1 A thermal barrier coating and a method of applying such a coating
04/08/2004WO2004028739A1 Method and device for creating internal compression stresses within the surface of workpieces
04/08/2004US20040067139 Fiber reinforced composite article
04/08/2004US20040067138 Fluid machinery
04/08/2004US20040067137 Radial retainer for single lobe turbine blade attachment and method for radially retaining a turbine blade in a turbine blade slot
04/08/2004US20040067131 Leak resistant vane cluster
04/08/2004US20040064945 Method of forming turbine blade root
04/08/2004US20040064944 Process for machining axial blade slots in turbine disks for jet engines
04/08/2004US20040064930 Method of forming cooling apertures in airfoil-shaped blades
04/08/2004DE10245197A1 Verfahren und Vorrichtung zum Herstellen von Gabelfüßen von Turbinenschaufeln Method and apparatus for the manufacture of fork feet of turbine blades
04/07/2004EP1406019A1 Drum rotor for a turbomachine