| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
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| 08/02/2001 | WO2001015869A3 Shim removing tool and method |
| 08/02/2001 | WO2000071781A3 Bond coats for turbine components and method of applying the same |
| 08/02/2001 | US20010010798 Rotary apparatus for a gas turbine engine |
| 08/02/2001 | US20010010797 Connector tube for a turbine rotor cooling circuit |
| 08/02/2001 | EP1144163A3 Shim removing tool and method |
| 08/02/2001 | DE10004128A1 Luftgekühlte Turbinenschaufel Air-cooled turbine blade |
| 08/01/2001 | EP1120545A2 Locking of rotorblades in axial turbines |
| 08/01/2001 | EP1120544A1 Turbo machine with a device for supplying a pressurized gas |
| 08/01/2001 | EP1120543A2 Methods and apparatus for directing airflow to a compressor bore |
| 08/01/2001 | EP1120480A2 Enhanced coating system for turbine airfoil applications |
| 08/01/2001 | EP1120177A2 Method of producing a cooling liner |
| 07/31/2001 | US6267902 Process for removing a coating from a hole in a metal substrate |
| 07/31/2001 | US6267558 Dual intensity peening and aluminum-bronze wear coating surface enhancement |
| 07/31/2001 | US6267557 Aerofoil blade damper |
| 07/31/2001 | US6267556 Steam turbine |
| 07/31/2001 | US6267553 Gas turbine compressor spool with structural and thermal upgrades |
| 07/31/2001 | US6267552 Arrangement of holes for forming a cooling film |
| 07/31/2001 | CA2012234C Gamma titanium alloys modified by chromium and silicon and method of preparation |
| 07/26/2001 | WO2001020133A8 Film cooling hole construction in gas turbine moving-vanes |
| 07/26/2001 | US20010009643 Steam turbine |
| 07/26/2001 | US20010009368 Nondestructive method for determining the thickness of a metallic protective layer on a metallic base material |
| 07/26/2001 | US20010009247 Method of removing a thermal barrier coating |
| 07/26/2001 | US20010009246 Method of removing ceramic coatings |
| 07/26/2001 | US20010009108 Method of producing a lining artefact |
| 07/25/2001 | EP1118747A2 An aerofoil for an axial flow turbomachine |
| 07/25/2001 | EP1118695A2 Method of removing a thermal barrier coating |
| 07/25/2001 | EP1118419A2 Method of forming cooling holes |
| 07/25/2001 | EP1117913A1 Fuel preheating in a gas turbine |
| 07/25/2001 | CN2440115Y Unequidistant vane-variable cascade |
| 07/25/2001 | CN1305049A Technique for cooling blades of gas turbine |
| 07/24/2001 | US6265080 Pest resistant molybdenum disilicide type materials |
| 07/24/2001 | US6265022 Process of plugging cooling holes of a gas turbine component |
| 07/24/2001 | US6264717 Comprising fine-grain, homogeneous microstructure is essentially oxide- and sulfide-free and segregation defect free |
| 07/24/2001 | US6264429 Compressor blade or vane and compressor using a blade or vane |
| 07/24/2001 | US6264428 Cooled aerofoil for a gas turbine engine |
| 07/24/2001 | US6264426 Gas turbine stationary blade |
| 07/24/2001 | US6264425 Fluid-flow machine for compressing or expanding a compressible medium |
| 07/24/2001 | CA2234922C Cooled shroud of gas turbine stationary blade |
| 07/24/2001 | CA2229322C Cooling medium path in gas turbine moving blade |
| 07/19/2001 | WO2001051772A1 Turbine blade and method of repair |
| 07/19/2001 | WO1999051866A3 Compressor endwall bleed system |
| 07/19/2001 | US20010008708 Ceramic heat barrier coating having low thermal conductivity, and process for the deposition of said coating |
| 07/19/2001 | US20010008070 Air impingement cooling system |
| 07/19/2001 | DE10001516A1 Non-destructive metallic protection layer thickness determination involves detecting foreign material layer including oxide particle or carbide material in between metallic base material and metallic protection layer |
| 07/19/2001 | DE10001109A1 Cooled blade for gas turbine, with several internal cooling channels running radially in blade |
| 07/18/2001 | EP1116861A2 A cooling circuit for and method of cooling a gas turbine bucket |
| 07/18/2001 | EP1116545A1 Joining of single crystal turbine parts |
| 07/18/2001 | EP1116523A2 Masking fixture and method |
| 07/18/2001 | EP1115963A2 Gas turbine engine |
| 07/18/2001 | EP1115906A1 Method for processing the interior of a hollow part |
| 07/18/2001 | CN1303990A Moving vane of turbine |
| 07/17/2001 | US6261643 Composites |
| 07/17/2001 | US6261063 Seal structure between gas turbine discs |
| 07/17/2001 | US6261058 Stationary blade of integrated segment construction and manufacturing method therefor |
| 07/17/2001 | US6261056 Ceramic turbine nozzle including a radially splined mounting surface |
| 07/17/2001 | US6261054 Coolable airfoil assembly |
| 07/17/2001 | US6261053 Cooling arrangement for gas-turbine components |
| 07/17/2001 | US6260794 Dolphin cascade vane |
| 07/17/2001 | US6260352 Turbofan aircraft engine |
| 07/17/2001 | US6260269 Method for overhauling a steam turbine to increase its power |
| 07/12/2001 | WO2001049975A1 Turbine engine damper |
| 07/12/2001 | US20010007719 Mixed oxide overcoating metal or alloy; gas turbine engine |
| 07/12/2001 | US20010007633 Configuration for axial retention of blades in a disc |
| 07/12/2001 | DE19963377A1 Turbinenschaufel mit aktiv gekühltem Deckbandelement Turbine blade with actively cooled shroud element |
| 07/12/2001 | DE19963375A1 Cooling for the paddle tip at a gas turbine has a system to generate coolant air eddies at the gap between the paddle tip and the housing section where the hot gas flows through |
| 07/12/2001 | DE19960278A1 Maschinensatz Machine set |
| 07/12/2001 | DE10053432A1 Selbstbindende MCrAlY-Pulver Self-binding MCrAlY powder |
| 07/11/2001 | EP1114916A1 Device for the axial retention of blades in a rim |
| 07/11/2001 | EP1114878A1 Alloy of molybdenum disilicide containing rhenium which is pest resistant |
| 07/11/2001 | EP0824606B1 Porous thermal barrier coating |
| 07/11/2001 | CN1068409C Cooling system for gas turbine |
| 07/10/2001 | US6258226 Device for preventing plating of material in surface openings of turbine airfoils |
| 07/10/2001 | US6257831 Cast airfoil structure with openings which do not require plugging |
| 07/10/2001 | US6257830 Gas turbine blade |
| 07/10/2001 | US6257828 Turbine blade and method of producing a turbine blade |
| 07/10/2001 | CA2208113C Structure of output section of jet propulsion engine or gas turbine |
| 07/05/2001 | WO2001048424A2 Cold air refrigerating system and turboexpander turbine for this system |
| 07/05/2001 | WO2001002742A3 Rotor with a split rotor blade |
| 07/05/2001 | US20010006601 Steam cooling system for a gas turbine |
| 07/05/2001 | US20010006600 Turbine blade with actively cooled shroud-band element |
| 07/05/2001 | US20010006599 Enhanced fan and fan drive assembly |
| 07/05/2001 | DE19963716A1 Gekühlte Strömungsumlenkvorrichtung für eine bei hohen Temperaturen arbeitende Strömungsmaschine Chilled flow deflection for operating at high temperatures turbomachine |
| 07/05/2001 | DE19963714A1 Method for repairing rotating components of gas turbine uses focussed material jet of water to separate predeterminable interface over an area of a component and then locking on replacement part with keyed engagement |
| 07/05/2001 | DE19963346A1 Blade assembly in a turbo-engine and method for fitting blades on a rotor fits blades on a rotor crosswise to their operating orientation with a butt end in a perimeter recess for twisting them into their operating orientation. |
| 07/05/2001 | CA2395808A1 Cold air refrigerating system and turboexpander turbine for this system |
| 07/04/2001 | EP1113145A1 Blade for gas turbines with metering section at the trailing edge |
| 07/04/2001 | EP1113144A2 Cooled fluid directing means for a turbomachine working at high temperatures |
| 07/04/2001 | EP1112440A1 Turbine guide blade |
| 07/04/2001 | EP1112439A1 Turbine bucket |
| 07/04/2001 | EP1112141A1 Method for repairing and producing integrally bladed rotors for a hydraulic engine |
| 07/04/2001 | CN1301911A Turbine blade with effectively cooled circular piece |
| 07/03/2001 | US6255000 Single-cast, high-temperature, thin wall structures |
| 07/03/2001 | US6254935 Method for applying a barrier layer to a silicon based substrate |
| 07/03/2001 | US6254756 Preparation of components having a partial platinum coating thereon |
| 07/03/2001 | US6254347 Striated cooling hole |
| 07/03/2001 | US6254346 Gas turbine cooling moving blade |
| 07/03/2001 | US6254345 Internally cooled blade tip shroud |
| 07/03/2001 | US6254343 Low-noise cooling fan for electronic components and method of making the same |
| 07/03/2001 | US6254334 Method and apparatus for cooling a wall within a gas turbine engine |
| 07/03/2001 | US6254333 Method for forming a cooling passage and for cooling a turbine section of a rotary machine |