Inventor · disambiguated record
Moritz Wirth
Also filed as: WIRTH MORITZ
5 granted patents·7 pending applications·17 citations·filing 2005–2024
70Inventor score
Files withROLLS ROYCE DEUTSCHLAND LTD & CO KG7BUTZ CARSTEN1MTU AERO ENGINES GMBH1PICHEL SACHA1ROTH-FAGARASEANU DAN1
Top patents by PatentIndex Score
12 records- 0165US12359583B2Aircraft engine and method for tempering a fan blade and/or an intake coneROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2023·Granted Jul 15, 2025·0 cites·20 claims
- 0256US8105016B2Damping arrangement for guide vanesBUTZ CARSTEN·Filed 2005·Granted Jan 31, 2012·11 cites·3 claims
- 0351US8388303B2Gas turbine having a rotor including a turbine rotor, expanded shaft and a compressor rotorWEIDMANN WILFRIED·Filed 2008·Granted Mar 5, 2013·6 cites·19 claims
- 0449US11674453B2Gas turbine engine having hollow low-pressure shaft with integrated valve for delivering hot compressed air to a fan diskROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2022·Granted Jun 13, 2023·0 cites·16 claims
- 0544US2024263942A1Method for determining a shape of a mistuned blade of an impeller of a turbomachineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2024·Application pending·0 cites
- 0636US2017284415A1Fan housing and engine assembly with fan housingROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Application pending·0 cites
- 0735US12031503B2Gas turbine engine fanROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2021·Granted Jul 9, 2024·0 cites·16 claims
- 0834US2009293447A1Method for the provision of fire protection for titanium components of an aircraft gas turbine and titanium components for an aircraft gas turbineROTH-FAGARASEANU DAN·Filed 2009·Application pending·0 cites
- 0934US2009028712A1Turbomachine having axial rotor blade securingMTU AERO ENGINES GMBH·Filed 2006·Application pending·0 cites
- 1034US2021017881A1Containment casing and gas turbine engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2020·Application pending·0 cites
- 1133US2017097012A1Flow guiding device and turbo-engine with at least one flow guiding deviceROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Application pending·0 cites
- 1231US2006266114A1Arrangement for precision balancing the rotor of a gas turbine enginePICHEL SACHA·Filed 2006·Application pending·0 cites
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