Inventor · disambiguated record
Karl-Heinz Dusel
Also filed as: DUSEL KARL-HEINZ
10 granted patents·6 pending applications·31 citations·filing 2007–2019
84Inventor score
Top patents by PatentIndex Score
16 records- 0186US9952236B2Method and device for process monitoringSATZGER WILHELM·Filed 2012·Granted Apr 24, 2018·10 cites·12 claims
- 0285US10507526B2Method and device for the additive manufacture of at least one component region of a componentMTU Aero Engines AG·Filed 2017·Granted Dec 17, 2019·3 cites·11 claims
- 0376US9771827B2Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbineMTU Aero Engines AG·Filed 2014·Granted Sep 26, 2017·5 cites·16 claims
- 0474US9393622B2Thin-walled structural component, and method for the production thereofJAKIMOV ANDREAS·Filed 2010·Granted Jul 19, 2016·1 cites·16 claims
- 0570US10875258B2Multi-frequency induction heating of generatively produced componentsBAMBERG JOACHIM·Filed 2012·Granted Dec 29, 2020·1 cites·15 claims
- 0668US9784131B2Sealing arrangement for a turbomachine, a guide vane arrangement, and a turbomachine with such a sealing arrangementMTU Aero Engines AG·Filed 2014·Granted Oct 10, 2017·3 cites·2 claims
- 0763US8092148B2Gas turbine having a peripheral ring segment including a recirculation channelSEITZ PETER·Filed 2007·Granted Jan 10, 2012·8 cites·12 claims
- 0846US10633975B2Device for producing, repairing and/or replacing a component by means of a powder that can be solidified by energy radiation, method and component produced according to said methodHESS THOMAS·Filed 2011·Granted Apr 28, 2020·0 cites·20 claims
- 0946US8708682B2Repair methodHUTTNER ROLAND·Filed 2009·Granted Apr 29, 2014·0 cites·4 claims
- 1046US2020080586A1Intermediate sheetMTU Aero Engines AG·Filed 2019·Application pending·0 cites
- 1145US10830068B2Method and device for the generative production of a component using a laser beam and corresponding turbo-engine componentSATZGER WILHELM·Filed 2012·Granted Nov 10, 2020·0 cites·17 claims
- 1244US2011052412A1High-pressure turbine rotor, and method for the production thereofMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 1342US2013055568A1Method and device for producing a componentDUSEL KARL-HEINZ·Filed 2011·Application pending·0 cites
- 1441US2012219726A1Method and device for producing a componentBAYER ERWIN·Filed 2010·Application pending·0 cites
- 1539US2013294891A1Method for the generative production of a component with an integrated damping element for a turbomachine, and a component produced in a generative manner with an integrated damping element for a turbomachineNEUHAEUSLER STEFAN·Filed 2012·Application pending·0 cites
- 1637US2009304497A1Guide blade segment of a gas turbine and method for its productionMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
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