Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
---|
05/02/2006 | US7037075 Blade cooling |
05/02/2006 | US7037074 Lightweight, foldable, and replaceable fabric fan blades |
05/02/2006 | US7037067 Gas turbine engine |
05/02/2006 | US7036320 Gas turbine with stator shroud in the cavity beneath the chamber |
04/27/2006 | WO2006042398A1 Improved measurement system |
04/27/2006 | US20060088419 Rotor assembly retaining apparatus |
04/27/2006 | US20060088418 Fan assembly and method |
04/27/2006 | US20060088416 Gas turbine rotor blade |
04/27/2006 | US20060088366 Non-explosive device for releasably securing components |
04/27/2006 | DE102004051116A1 Rotor einer Turbomaschine, insbesondere Gasturbinenrotor Rotor of a turbomachine, in particular a gas turbine rotor |
04/27/2006 | DE102004049860A1 Gas turbine, has shaft flange detachably connected to flange of torque-transferring component, which is positioned upstream of shaft flange, such that shaft is connected with torque-transferring component of turbine |
04/27/2006 | CA2584506A1 Improved measurement system |
04/26/2006 | EP1650406A2 Locking assembly for a gas turbine rotor stage |
04/26/2006 | EP1650405A1 Rotor of a turbomachine, in particular gas turbine rotor |
04/26/2006 | EP1650404A2 Rebuild method of a turbine blade tip squealer |
04/26/2006 | EP1649970A1 Method of manufacturing a turbine blade made of titanium |
04/26/2006 | EP1649145A1 Turbofan case and method of making |
04/26/2006 | EP1649143A1 Gas turbine blade inlet cooling flow deflector |
04/26/2006 | CN1763353A Airfoil with large fillet and micro-circuit cooling |
04/26/2006 | CN1763352A Airfoil with impingement cooling of a large fillet |
04/26/2006 | CN1763236A Method of protection of contact surfaces between two metallic pieces |
04/26/2006 | CN1253597C Method for repairing component made from Ni-based alloy |
04/25/2006 | US7034262 Apparatus and methods for repairing tenons on turbine buckets |
04/25/2006 | US7033140 Cooled rotor blade with vibration damping device |
04/25/2006 | US7033136 Cooling circuits for a gas turbine blade |
04/25/2006 | US7033135 Method and apparatus for distributing fluid into a turbomachine |
04/25/2006 | US7033131 Fan blade for a gas-turbine engine |
04/25/2006 | US7032279 Apparatus and methods for repairing compressor airfoils in situ |
04/21/2006 | CA2523255A1 Turbine blade tip squealer and rebuild method |
04/20/2006 | WO2006040221A1 Method for producing a layer system |
04/20/2006 | WO2006040220A1 Method for producing a layer system |
04/20/2006 | WO2006026695A3 Welding shield for automated welding of impellers and blisks, sized to match within vallexs of a particular designed impeller ; method to provide protection from welding related damage in an impeller |
04/20/2006 | WO2005091742A3 Gas-slip prepared reduced surface defect photoconductor aluminum alloy tube |
04/20/2006 | US20060083621 Rotor of a turbo engine, e.g., a gas turbine rotor |
04/20/2006 | US20060083614 Airfoil with large fillet and micro-circuit cooling |
04/20/2006 | US20060083613 Impingement cooling of large fillet of an airfoil |
04/20/2006 | US20060081686 Repair process |
04/20/2006 | US20060081685 Repair process |
04/20/2006 | DE102004050739A1 Gas turbine has slits in radially outer ends of vanes of rotor to contain radially movable sealing element sealing gap between vane and housing |
04/19/2006 | EP1647674A2 A method and test component for rotatable disc parts |
04/19/2006 | EP1647672A2 Airfoil with impingement cooling of a large fillet |
04/19/2006 | EP1647671A1 Thermally stressed component of a turbomachine |
04/19/2006 | CN1252382C Insulation structure type rotor coupler |
04/19/2006 | CN1252376C Turbo-machine comprising sealing system for rotor |
04/19/2006 | CN1252375C Vortex wheel turbine |
04/18/2006 | US7029721 Method for applying a high-temperature bond coat on a metal substrate, and related compositions and articles |
04/18/2006 | US7029237 Retention capacity of blade having an asymmetrical hammerhead connection |
04/18/2006 | US7029236 Closed circuit blade-cooled turbine |
04/18/2006 | US7029235 Cooling system for a tip of a turbine blade |
04/18/2006 | US7029227 Structure comprising a rotor and fixed perturbation sources and method for reducing vibrations in said structure |
04/18/2006 | US7028747 Closed loop steam cooled airfoil |
04/18/2006 | US7028378 Method of shot blasting and a machine for implementing such a method |
04/18/2006 | CA2523183A1 Circumferential feather seal |
04/18/2006 | CA2333809C Convex compressor casing |
04/13/2006 | WO2006038903A1 Turbocharger compressor with non-axisymmetric deswirl vanes |
04/13/2006 | DE10319015B4 Verfahren zur Wartung von Gasturbinen Process for the maintenance of gas turbines |
04/13/2006 | DE10248240B4 Verbindungsverfahren für Komponenten Connection methods for components |
04/12/2006 | EP1645724A2 Method of protection of contact surfaces between two metallic pieces |
04/12/2006 | EP1645723A1 Turbine component, gas turbine engine, method for manufacturing turbine component, surface processing method, vane component, metal component, and steam turbine engine |
04/12/2006 | EP1645722A2 Turbine airfoil with stepped coolant outlet slots |
04/12/2006 | EP1645721A2 Gas turbine airfoil with leading edge cooling |
04/12/2006 | EP1645720A1 Frequency tailored blade thickness for a turbomachinewheel |
04/12/2006 | EP1645661A1 Thermal barrier coatings with low thermal conductivity comprising lanthanide sesquioxides |
04/12/2006 | EP1645654A1 Method of manufacturing a flexible thermal barrier coating |
04/12/2006 | EP1645652A1 Process for the manufacture of a layer system |
04/12/2006 | EP1645347A1 Method for producing a casting of high thermal load |
04/12/2006 | EP1644614A1 Cooled blade for a gas turbine |
04/12/2006 | EP1644613A1 Steam turbine |
04/12/2006 | EP1644242A2 Rotor blade tip section |
04/12/2006 | CN1757883A Strong curved wing section of sea temperature difference energy-solar energy reboil circulation power generating steam turbine |
04/12/2006 | CN1757791A Coating system |
04/12/2006 | CN1250868C Device for centering tube in turbine shaft |
04/12/2006 | CN1250863C Output stage of axial-flow turbine |
04/12/2006 | CN1250361C Method for making turbine vanes |
04/11/2006 | US7026011 Aluminide coating of gas turbine engine blade |
04/11/2006 | US7025570 Axial flow fan assembly |
04/11/2006 | US7025568 Turbomachine aerofoil |
04/11/2006 | US7025563 Stator vane assembly for a gas turbine engine |
04/11/2006 | US7025562 Device for cooling turbine disks |
04/11/2006 | US7024787 Template for evaluating parts and method of using same |
04/11/2006 | US7024744 Frequency-tuned compressor stator blade and related method |
04/06/2006 | WO2005124107A3 Turbine wheel in a waste gas turbine of a waste gas turbocharger |
04/06/2006 | WO2005057001A3 Low-noise fan exit guide vanes |
04/06/2006 | US20060073021 Remotely accessible locking system for turbine blades |
04/06/2006 | US20060073019 Axial-flow thermal turbomachine |
04/06/2006 | US20060073017 Stepped outlet turbine airfoil |
04/06/2006 | US20060073016 Gas turbine airfoil leading edge cooling construction |
04/06/2006 | US20060073015 Gas turbine airfoil film cooling hole |
04/06/2006 | US20060073014 Air foil shape for a compressor blade |
04/06/2006 | DE102005037031A1 Turbolader mit Titankomponente Turbochargers with titanium component |
04/06/2006 | CA2520564A1 Stepped outlet turbine airfoil |
04/05/2006 | EP1643084A1 Turbine engine shroud segment, hanger and assembly |
04/05/2006 | EP1643083A2 Coupled parametric design of flow control and duct shape |
04/05/2006 | EP1643082A1 Turbine blade retention system |
04/05/2006 | EP1643081A2 Corner cooled turbine nozzle |
04/05/2006 | EP1643011A1 Erosion and wear resistant protective structures for turbine components |
04/05/2006 | EP1642993A1 Segmented gadolinia zirconia coatings |
04/05/2006 | EP1642989A2 Nickel base alloy |
04/05/2006 | EP1642666A1 Microwave brazing of airfoil cracks |
04/05/2006 | EP1642006A1 Turbine shroud segment |