Inventor · disambiguated record
Thomas Uihlein
Also filed as: UIHLEIN THOMAS
22 granted patents·14 pending applications·275 citations·filing 1990–2021
95Inventor score
Files withMTU AERO ENGINES GMBH13MTU Aero Engines AG5MTU MUENCHEN GMBH5UIHLEIN THOMAS4EICHMANN WOLFGANG2
Top patents by PatentIndex Score
36 records- 0186US9492906B2Cleaning of a turbo-machine stageRÖSING JÜRGEN·Filed 2011·Granted Nov 15, 2016·24 cites·15 claims
- 0285US5660320AMethod of manufacturing a metallic component or substrate with bonded coatingMTU MUENCHEN GMBH·Filed 1995·Granted Aug 26, 1997·75 cites·20 claims
- 0384US10415400B2Masking method for producing a combination of blade tip hardfacing and erosion-protection coatingMTU Aero Engines AG·Filed 2016·Granted Sep 17, 2019·4 cites·8 claims
- 0484US5756217AStrip coatings for metal components of drive units and their process of manufactureMTU MUENCHEN GMBH·Filed 1995·Granted May 26, 1998·64 cites·12 claims
- 0578US8663814B2Anti-wear coating and component comprising an anti-wear coatingEICHMANN WOLFGANG·Filed 2008·Granted Mar 4, 2014·4 cites·10 claims
- 0678US7942638B2Turbomachine blade with a blade tip armor claddingMTU AERO ENGINES GMBH·Filed 2006·Granted May 17, 2011·20 cites·24 claims
- 0775US6171351B1Strip coatings for metal components of drive units and their process of manufactureMTU MUENCHEN GMBH·Filed 1997·Granted Jan 9, 2001·41 cites·9 claims
- 0874US8153274B2Thermal barrier layerSCHNEIDERBANGER STEFAN·Filed 2007·Granted Apr 10, 2012·4 cites·14 claims
- 0973US9427937B2Anti-wear coatingUIHLEIN THOMAS·Filed 2011·Granted Aug 30, 2016·2 cites·20 claims
- 1073US8936442B2Method for the production of an integrally bladed rotor, and rotorUIHLEIN THOMAS·Filed 2010·Granted Jan 20, 2015·3 cites·17 claims
- 1172US9212555B2Method for removing the coating from a gas turbine componentMANIER KARL-HEINZ·Filed 2006·Granted Dec 15, 2015·5 cites·15 claims
- 1265US8356741B2Method for producing a blade plating on a blade for a turbomachineMTU AERO ENGINES GMBH·Filed 2010·Granted Jan 22, 2013·2 cites·8 claims
- 1365US7927709B2Wear-resistant coating and a component having a wear-resistant coatingMTU AERO ENGINES GMBH·Filed 2004·Granted Apr 19, 2011·9 cites·16 claims
- 1463US8920881B2Method for producing a component covered with a wear-resistant coatingEICHMANN WOLFGANG·Filed 2005·Granted Dec 30, 2014·3 cites·12 claims
- 1559US9114480B2Methods for joining a monocrystalline part to a polycrystalline part by means of an adapter piece made of polycrystalline materialKNOTT ULRICH·Filed 2009·Granted Aug 25, 2015·1 cites·7 claims
- 1656US12359573B2Blade for a turbomachine including blade tip armor and an erosion protection layer, and method for manufacturing sameMTU Aero Engines AG·Filed 2021·Granted Jul 15, 2025·0 cites·13 claims
- 1756US2010239429A1Wear protection coatingMTU AERO ENGINES GMBH·Filed 2008·Application pending·0 cites
- 1854US8012562B2Wear-resistant coatingMTU AERO ENGINES GMBH·Filed 2008·Granted Sep 6, 2011·1 cites·22 claims
- 1954US2011217176A1Method for connecting at least one turbine blade to a turbine disk or a turbine ringMTU AERO ENGINES GMBH·Filed 2009·Application pending·0 cites
- 2052US2010143110A1Vane for a compressor or a turbine of an aircraft engine, aircraft engine comprising such a vane and a method for coating a vane of an aircraft engineMTU AREO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 2150US2010108538A1Method for stripping a componentMTU AERO ENGINES GMBH·Filed 2008·Application pending·0 cites
- 2246US9920411B2Device and method for partially masking a component zone of a componentMTU Aero Engines AG·Filed 2016·Granted Mar 20, 2018·0 cites·16 claims
- 2346US2011020548A1Device and method for the partial coating of componentsMTU AERO ENGINES GMBH·Filed 2009·Application pending·0 cites
- 2446US2010263694A1Decoating device for axially symmetric components, particularly from aircraft enginesMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 2543US10400613B2Method of producing blades or blade arrangements of a turbomachine with erosion protection layers and correspondingly produced componentMTU Aero Engines AG·Filed 2017·Granted Sep 3, 2019·0 cites·20 claims
- 2642US2010284817A1Method for producing a blisk or a bling, component produced therewith and turbine bladeBAMBERG JOACHIM·Filed 2008·Application pending·0 cites
- 2739US5087512ASurface coating for protecting a component against titanium fire and method for making the surface coatingMTU MUENCHEN GMBH·Filed 1990·Granted Feb 11, 1992·7 cites·12 claims
- 2838US2010119376A1Inlet cone for jet engineMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 2937US2016333705A1Combination of blade tip cladding and erosion-resistant layer and method for the production thereofMTU Aero Engines AG·Filed 2016·Application pending·0 cites
- 3037US2011299996A1Anti-erosion coating system for gas turbine componentsUIHLEIN THOMAS·Filed 2010·Application pending·0 cites
- 3137US2010143108A1Device for the Protection of Components Having A Flammable Titanium Alloy From Titanium Fire, and Method for the Production ThereofMTU AERO ENGINES GMBH·Filed 2008·Application pending·0 cites
- 3237US2010064515A1Method for repairing and/or replacing individual elements of a gas turbine componentMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 3336US5202163ASurface coating for protecting a component against titanium fire and method for making the surface coatingMTU MUENCHEN GMBH·Filed 1991·Granted Apr 13, 1993·6 cites·9 claims
- 3436US2009233111A1Thermal Barrier Coating SystemUIHLEIN THOMAS·Filed 2006·Application pending·0 cites
- 3536US2009269207A1Component, in particular, a gas turbine componentMTU AERO ENGINES GMBH·Filed 2006·Application pending·0 cites
- 3632US9951411B2Erosion protection coatingHEUTLING FALKO·Filed 2009·Granted Apr 24, 2018·0 cites·18 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →