Inventor · disambiguated record
Wilfried Smarsly
Also filed as: SMARSLY WILFRIED
26 granted patents·13 pending applications·302 citations·filing 1984–2018
95Inventor score
Top patents by PatentIndex Score
39 records- 0193US7389808B2Method for producing a cast componentG4T GMBH·Filed 2005·Granted Jun 24, 2008·13 cites·4 claims
- 0291US5634189AStructural component made of metal or ceramic having a solid outer shell and a porous core and its method of manufactureMTU MUENCHEN GMBH·Filed 1994·Granted May 27, 1997·84 cites·11 claims
- 0385US10526902B2Method for producing a blade for a turbomachineMTU Aero Engines AG·Filed 2017·Granted Jan 7, 2020·2 cites·20 claims
- 0484US5073459ASintered light-weight structural material and method of its manufactureMTU MUENCHEN GMBH·Filed 1990·Granted Dec 17, 1991·43 cites·15 claims
- 0583US8888461B2Material for a gas turbine component, method for producing a gas turbine component and gas turbine componentSMARSLY WILFRIED·Filed 2008·Granted Nov 18, 2014·8 cites·14 claims
- 0681US7389809B2Tool for producing cast components, method for producing said tool, and method for producing cast componentsG4T GMBH·Filed 2004·Granted Jun 24, 2008·16 cites·5 claims
- 0780US7360579B2Method for the production of cast componentsG4T GMBH·Filed 2004·Granted Apr 22, 2008·13 cites·11 claims
- 0875US10029309B2Production process for TiAl componentsMTU Aero Engines AG·Filed 2015·Granted Jul 24, 2018·1 cites·19 claims
- 0975US9551231B2Ductile compensation layer for brittle componentsMTU Aero Engines AG·Filed 2013·Granted Jan 24, 2017·4 cites·20 claims
- 1074US6773817B1Antiabrasion coatingMTU AERO ENGINES GMBH·Filed 1999·Granted Aug 10, 2004·48 cites·16 claims
- 1172US8012271B2Material for components of a gas turbineMTU AERO ENGINES GMBH·Filed 2006·Granted Sep 6, 2011·2 cites·20 claims
- 1271US4599215AProcess and device for producing compressed mouldings from loose or sintered metal powderLUFT & RAUMFAHRT DEUTSCHE·Filed 1984·Granted Jul 8, 1986·26 cites·18 claims
- 1369US9994934B2Creep-resistant TiA1 alloyMTU Aero Engines AG·Filed 2014·Granted Jun 12, 2018·1 cites·15 claims
- 1468US8882442B2Component for a gas turbine and a method for the production of the componentSMARSLY WILFRIED·Filed 2009·Granted Nov 11, 2014·13 cites·19 claims
- 1562US10458001B2Method for producing a component from a composite material comprising a metal matrix and incorporated intermetallic phasesMTU Aero Engines AG·Filed 2016·Granted Oct 29, 2019·1 cites·20 claims
- 1660US10385434B2Process and apparatus for producing forged TiAl componentsMTU Aero Engines AG·Filed 2016·Granted Aug 20, 2019·0 cites·14 claims
- 1760US5032353ASintering method for producing structural components of an intermetallic compoundMTU MUENCHEN GMBH·Filed 1990·Granted Jul 16, 1991·21 cites·17 claims
- 1858US10590520B2High temperature resistant TiAl alloy, production method therefor and component made therefromMTU Aero Engines AG·Filed 2017·Granted Mar 17, 2020·0 cites·20 claims
- 1958US10544485B2Additive manufacturing of high-temperature components from TiAlMTU Aero Engines AG·Filed 2017·Granted Jan 28, 2020·0 cites·20 claims
- 2056US10267167B2Ductile compensation layer for brittle componentsMTU Aero Engines AG·Filed 2017·Granted Apr 23, 2019·0 cites·20 claims
- 2155US10107112B2Method for producing forged components from a TiAl alloy and component produced therebyMTU Aero Engines AG·Filed 2013·Granted Oct 23, 2018·0 cites·18 claims
- 2254US2015315919A1LIGHTWEIGHT STRUCTURAL NiAl ALLOY WITH A HIGH HIGH-TEMPERATURE STRENGTHMTU Aero Engines AG·Filed 2014·Application pending·0 cites
- 2353US10465264B2Al-rich high-temperature TiAl alloyMTU Aero Engines AG·Filed 2015·Granted Nov 5, 2019·0 cites·19 claims
- 2453US2016273368A1Blade of a turbomachine made of different materials and method for the production thereofMTU Aero Engines AG·Filed 2016·Application pending·0 cites
- 2551US2015147220A1MATERIAL OF LAVES PHASE AND FERRITIC Fe-Al PHASEMTU Aero Engines AG·Filed 2014·Application pending·0 cites
- 2650US2019070665A1Method for manufacturing a titanium aluminide component with a ductile core and correspondingly manufactured componentMTU Aero Engines AG·Filed 2018·Application pending·0 cites
- 2749US10364686B2TiAl blade with surface modificationMTU Aero Engines AG·Filed 2014·Granted Jul 30, 2019·0 cites·20 claims
- 2846US10577948B2Turbine blade and aircraft engine comprising sameMTU Aero Engines AG·Filed 2015·Granted Mar 3, 2020·0 cites·19 claims
- 2945US2017314402A1Method for producing a blade for a turbomachineMTU Aero Engines AG·Filed 2017·Application pending·0 cites
- 3045US2007190352A1Wear protection coating for a gas turbine componentBAYER ERWIN·Filed 2004·Application pending·0 cites
- 3145US2008069720A1Titanium-Aluminum AlloyG4T GMBH·Filed 2005·Application pending·0 cites
- 3244US2018105901A1Method of making a molybdenum alloy having a high titanium contentMTU Aero Engines AG·Filed 2017·Application pending·0 cites
- 3342US7699581B2Run-in coating for gas turbines and method for producing sameMTU AERO ENGINES GMBH·Filed 2004·Granted Apr 20, 2010·5 cites·16 claims
- 3442US2017241271A1Component of a molybdenum alloy and method for forming an oxidation protection layer thereforMTU Aero Engines AG·Filed 2017·Application pending·0 cites
- 3541US8895134B2Apparatus and method for coating a compressor housingSMARSLY WILFRIED·Filed 2005·Granted Nov 25, 2014·1 cites·10 claims
- 3641US2005279481A1Method and device for producing precision investment-cast ne metal alloy members and ne metal alloys for carrying out said methodMTU AERO ENGINES GMBH·Filed 2003·Application pending·0 cites
- 3739US2017145837A1Method of making a bladed rotor for a turbomachineMTU Aero Engines AG·Filed 2016·Application pending·0 cites
- 3839US2014202601A1FORGED TiAl COMPONENTS, AND METHOD FOR PRODUCING SAMEHELM DIETMAR·Filed 2012·Application pending·0 cites
- 3938US2016060734A1Creep- and oxidation-resistant molybdenum superalloyMTU Aero Engines AG·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →