| 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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| 05/09/1996 | WO1996013622A1 Platinum aluminide cvd coating method |
| 05/08/1996 | EP0710766A1 Integral disc seal |
| 05/08/1996 | EP0710728A1 Fibre reinforced metal disc preform and manufacturing method thereof |
| 05/08/1996 | EP0618996B1 Process for the manufacture of a wheel for a turbine with inserted blades and wheel so obtained |
| 05/07/1996 | US5514482 Thermal barrier coating system for superalloy components |
| 05/07/1996 | US5513955 Turbine engine rotor blade platform seal |
| 05/07/1996 | US5513952 Axial flow compressor |
| 05/07/1996 | US5513489 Rotary valve multiple combustor pulse detonation engine |
| 05/02/1996 | WO1996012874A1 Gas turbine blade with enhanced cooling |
| 05/02/1996 | WO1996012873A1 A system for repairing damaged gas turbine engine airfoils |
| 05/01/1996 | EP0709549A1 Bladed rotor especially for a turbomachine |
| 05/01/1996 | EP0709548A2 Inter-blade seal |
| 05/01/1996 | EP0709547A1 Cooling of the rim of a gas turbine rotor disk |
| 05/01/1996 | EP0708876A1 Low thermal stress ceramic turbine nozzle |
| 05/01/1996 | EP0708875A1 Rotor blade with integral platform and a fillet cooling passage |
| 04/30/1996 | US5512382 Porous thermal barrier coating |
| 04/30/1996 | US5511949 Method for producing a monobloc rotor with hollow blades and monobloc rotor with hollow blades obtained by said method |
| 04/30/1996 | US5511948 Rotor blade damping structure for axial-flow turbine |
| 04/30/1996 | US5511946 Cooled airfoil tip corner |
| 04/30/1996 | US5511945 Turbine motor and blade interface cooling system |
| 04/30/1996 | US5511940 Ceramic turbine nozzle |
| 04/30/1996 | US5511937 Gas turbine airfoil with a cooling air regulating seal |
| 04/30/1996 | US5511604 Method for making a titanium metal matrix composite |
| 04/30/1996 | US5511309 Method of manufacturing a turbine airfoil with enhanced cooling |
| 04/30/1996 | US5511308 Method and apparatus for turbine blade rehabilitation |
| 04/25/1996 | WO1996012049A1 Protective layer for protecting parts against corrosion, oxidation and excessive thermal stresses, as well as process for producing the same |
| 04/25/1996 | DE4014808C2 Verfahren zur numerischen Steuerung einer Bearbeitungseinrichtung Method for numerical control machining equipment |
| 04/24/1996 | EP0708227A1 Composite turbomachine blade with integrated brush seal and manufacturing method therefor |
| 04/23/1996 | US5510080 Nickel base alloy containing particles of yttrium oxide dispersed in matrix |
| 04/23/1996 | US5509784 Turbine bucket and wheel assembly with integral bucket shroud |
| 04/23/1996 | US5509783 Reinforced vane |
| 04/23/1996 | US5509286 Method and apparatus for surface treating and prestressing the inside wall of a cavity |
| 04/18/1996 | WO1996011288A1 Multiple nanolayer coating system |
| 04/18/1996 | DE4436730A1 Oscillation damper for blades of thermal flow machine |
| 04/17/1996 | EP0707136A1 Drum rotor for an axial flow turbomachine |
| 04/17/1996 | EP0707135A2 Bladed rotor |
| 04/17/1996 | EP0707091A1 Zirconia-based tipped blades having macrocracked structure and process for producing it |
| 04/16/1996 | US5507623 Laminated inorganic protective coating comprising maximum aluminum concentration at uppermost layer, reducing gradually toward innermost layer; heat, corrosion, chemical and oxidation resistance |
| 04/16/1996 | US5507621 Cooling air cooled gas turbine aerofoil |
| 04/16/1996 | US5507620 Gas turbine with cooled rotor |
| 04/11/1996 | WO1996010684A1 Gas turbine airfoil with a cooling air regulating seal |
| 04/10/1996 | EP0705959A2 Rootconfiguration for turbomachineblades |
| 04/10/1996 | EP0705958A1 Chamfering of stressed regions in a fir-tree turbine blade root |
| 04/10/1996 | EP0705912A2 A coated article |
| 04/04/1996 | WO1996010143A1 Brush seal with fool proofing and anti-rotation tab |
| 04/04/1996 | DE4435321A1 Turbine blade having low density, good mechanical strength and good oxidn resistance |
| 04/04/1996 | DE19535713A1 Hinterkantenverstärkung einer Fan-Verbundschaufel Trailing edge reinforcement of a fan-blade composite |
| 04/03/1996 | EP0704603A2 Sealing and cooking method for the hot side of a gas turbine shaft |
| 04/03/1996 | EP0704602A2 Turbine blade |
| 04/03/1996 | EP0704601A1 Combined heat shield and retainer for turbine assembly bolt |
| 04/03/1996 | CN1119841A Process for hard-rolling a component |
| 04/03/1996 | CN1119698A Making of blade of gas turbine made of 2/beta titan-based alloy |
| 04/02/1996 | US5503529 Turbine blade having angled ejection slot |
| 04/02/1996 | US5503527 Turbine blade having tip slot |
| 03/27/1996 | EP0702748A1 Rotor blade with cooled integral platform |
| 03/27/1996 | CN2223353Y Blade construction for deep-water motor |
| 03/27/1996 | CN1031421C Nozzle use in geothermal turbines and method for preventing scales thereon |
| 03/26/1996 | US5501892 Ceramic parts having small hole(s) and method of manufacturing the same |
| 03/26/1996 | US5501575 Fan blade attachment for gas turbine engine |
| 03/21/1996 | DE4440241C1 Turbine with housing in which is turbine wheel activated on both sides |
| 03/20/1996 | EP0702131A1 Stable blade vibration damper for gas turbine engine |
| 03/20/1996 | EP0702130A2 Blade tip with cutting surface layer |
| 03/20/1996 | EP0702129A2 Cooling the rotor of an axial gasturbine |
| 03/20/1996 | EP0621920B1 Cooling of the shroud of a turbine blade |
| 03/14/1996 | DE4445297C1 Rotor wheel for turbo machine esp. radial compressor |
| 03/13/1996 | EP0700738A1 Method of producing a hollow turbine blade |
| 03/12/1996 | US5498137 Turbine engine rotor blade vibration damping device |
| 03/12/1996 | US5498136 Fluid machinery having blade apparatus and blade apparatus for fluid machinery |
| 03/12/1996 | US5498133 Gas turbine engine airfoil |
| 03/12/1996 | US5498131 Steam turbine with thermal stress reduction system |
| 03/12/1996 | US5498126 Airfoil with dual source cooling |
| 03/12/1996 | CA2051839C Method of forming platinum-silicon-enriched diffused aluminide coating on a superalloy substrate |
| 03/07/1996 | WO1996007018A1 Dynamic control of tip clearance |
| 03/06/1996 | EP0699824A1 Device for locking rotor blades and eliminating rotor imbalance in compressors or turbines of gas turbine engines |
| 03/05/1996 | US5496151 Cooled turbine blade |
| 02/29/1996 | WO1996006266A1 Gas turbine blade with cooled platform |
| 02/29/1996 | WO1995029331A3 Stator vane arrangement for successive turbine stages |
| 02/28/1996 | EP0698725A2 Impingement cooling of wall portion |
| 02/28/1996 | EP0698724A2 Cooling circuit for turbine stator vane trailing edge |
| 02/28/1996 | EP0698723A2 Turbine stator vane segment having closed cooling circuit |
| 02/27/1996 | US5494408 Bucket to wheel dovetail design for turbine rotors |
| 02/27/1996 | US5494402 Low thermal stress ceramic turbine nozzle |
| 02/27/1996 | US5493855 Turbine having suspended rotor blades |
| 02/24/1996 | CA2155376A1 Turbine stator vane segment having closed cooling circuit |
| 02/24/1996 | CA2155375A1 Cooling circuit for turbine stator vane trailing edge |
| 02/22/1996 | WO1996005331A1 Process for reconditioning steel surfaces |
| 02/21/1996 | EP0697503A1 Method for the construction of a turbine blade from an (alpha-beta)-Titanium-base alloy |
| 02/20/1996 | US5492447 Of a gas turbine engine rotor |
| 02/15/1996 | WO1996004467A1 Centrifugal chopper pump |
| 02/15/1996 | WO1996001288A3 Method for improving the erosion resistance of engine components |
| 02/15/1996 | DE4428207A1 Mfg. turbine rotor disc with curved cooling air channels |
| 02/13/1996 | US5490764 Unshrouded blading for high bypass turbofan engines |
| 02/13/1996 | US5490759 Magnetic damping system to limit blade tip vibrations in turbomachines |
| 02/08/1996 | WO1996003584A1 Airfoil noise control |
| 02/08/1996 | WO1996003536A1 Protective coating |
| 02/08/1996 | WO1996003535A1 Protective coating |
| 02/08/1996 | DE4427360A1 Arrangement for preventing contamination and plugging of holes on tip of gas turbine blade |
| 02/07/1996 | EP0695856A1 Compressor disc with asymmetric circumferencial groove |
| 02/06/1996 | US5489346 Useful in casting gas turbine blades or vanes |
| 02/06/1996 | US5489194 Connecting by-pass mold to protrusions to a main mold corresponding to dovetail, shank and vane; casting a single crystal structure by gradual solidification of nickel base alloy in main and by-pass molds |