Inventor · disambiguated record
Max Niegl
Also filed as: NIEGL MAX
8 granted patents·3 pending applications·9 citations·filing 2006–2020
77Inventor score
Top patents by PatentIndex Score
11 records- 0174US11389887B2Method of removing Cr(VI) ions from an aqueous electrolyte solutionMTU Aero Engines AG·Filed 2020·Granted Jul 19, 2022·1 cites·20 claims
- 0272US9845526B2Slip and process for producing an aluminum diffusion layerMTU Aero Engines AG·Filed 2013·Granted Dec 19, 2017·1 cites·20 claims
- 0372US8765240B2Molding compound comprising a polyester resin composition, film produced from the molding compound and method for producing a film or film webGRIGO THORSTEN·Filed 2006·Granted Jul 1, 2014·5 cites·29 claims
- 0469US9540522B2Antifouling layer for compressor bladesMTU Aero Engines AG·Filed 2015·Granted Jan 10, 2017·1 cites·15 claims
- 0550US2008152802A1Method for cleaning, method and device for the application of a protective medium to a turbine blade, and a method for placing cooling bores in a turbine bladeMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 0649US8931318B2Device and method for the surface peening of a component of a gas turbineBAYER ERWIN·Filed 2007·Granted Jan 13, 2015·0 cites·12 claims
- 0747US9822258B2Cr(VI)-free corrosion protection layers or adhesion promoter layers produced using a solution comprising phosphate ions and metal powder, wherein the metal powder is coated at least partly with Si or Si alloysMTU Aero Engines AG·Filed 2013·Granted Nov 21, 2017·0 cites·20 claims
- 0847US2009186157A1Method for at least selectively removing a first layer from an engine componentMTU AERO ENGINES GMBH·Filed 2009·Application pending·0 cites
- 0941US8943659B2Method and device for the surface peening of a partial element of a component of a gas turbineBAYER ERWIN·Filed 2007·Granted Feb 3, 2015·1 cites·11 claims
- 1040US8499597B2Device and method for the surface peening of a component of a gas turbineBAYER ERWIN·Filed 2007·Granted Aug 6, 2013·0 cites·13 claims
- 1132US2015252199A1Anti-ice coating for compressor bladesMTU Aero Engines AG·Filed 2015·Application pending·0 cites
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