Inventor · disambiguated record
Knut Rosenau
Also filed as: ROSENAU KNUT
5 granted patents·4 pending applications·7 citations·filing 2013–2017
67Inventor score
Top patents by PatentIndex Score
9 records- 0182US10125616B2Fan blade for an aircraft engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Nov 13, 2018·5 cites·21 claims
- 0260US10465705B2Device for adjusting a gap between the housing of an impeller and the impeller in a radial compressor and a turbomachineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Nov 5, 2019·1 cites·19 claims
- 0349US9909433B2Aircraft gas turbine having a booster bleed duct in a stator vane root element of a bypass ductROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2013·Granted Mar 6, 2018·1 cites·7 claims
- 0444US9279326B2Method for balancing and assembling a turbine rotorROLLS ROYCE DEUTSCHLAND·Filed 2014·Granted Mar 8, 2016·0 cites·20 claims
- 0539US2015123680A1Inductive sensor and method of manufacturing an inductive sensorROLLS ROYCE DEUTSCHLAND·Filed 2014·Application pending·0 cites
- 0639US2018094582A1Turbofan engine for a civil supersonic aircraftROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Application pending·0 cites
- 0737US2018094605A1Turbofan engine for a civil supersonic aircraftROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Application pending·0 cites
- 0835US11187243B2Diffusor for a radial compressor, radial compressor and turbo engine with radial compressorROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Nov 30, 2021·0 cites·19 claims
- 0924US2016097301A1Aircraft gas turbine engine with shock-absorbing element for fan blade lossROLLS ROYCE DEUTSCHLAND·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →