Inventor · disambiguated record
Predrag Todorovic
Also filed as: TODOROVIC PREDRAG
50 granted patents·12 pending applications·207 citations·filing 2008–2022
98Inventor score
Files withROLLS ROYCE DEUTSCHLAND LTD & CO KG39TODOROVIC PREDRAG16ROLLS ROYCE DEUTSCHLAND6LISIEWICZ STEPHAN1
Top patents by PatentIndex Score
62 records- 0195US8776946B2Gas turbine exhaust coneTODOROVIC PREDRAG·Filed 2012·Granted Jul 15, 2014·22 cites·12 claims
- 0294US11149637B2Nacelle for a turbofan engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2018·Granted Oct 19, 2021·11 cites·20 claims
- 0393US8479877B2Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall elementTODOROVIC PREDRAG·Filed 2012·Granted Jul 9, 2013·16 cites·16 claims
- 0493US8307945B2Gas-turbine exhaust coneTODOROVIC PREDRAG·Filed 2011·Granted Nov 13, 2012·17 cites·20 claims
- 0589US8938944B2Aircraft gas-turbine engine with oil cooler in the engine cowlingTODOROVIC PREDRAG·Filed 2012·Granted Jan 27, 2015·13 cites·20 claims
- 0687US10082079B2Gas-turbine engine with oil cooler in the engine cowlingROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Sep 25, 2018·8 cites·6 claims
- 0786US8690098B2Air ejector nozzle tube for an oil heat exchanger of an aircraft engineTODOROVIC PREDRAG·Filed 2011·Granted Apr 8, 2014·12 cites·20 claims
- 0885US8220586B2Noise-reduced aircraft engine and method for reducing noise emissions of an aircraft engineTODOROVIC PREDRAG·Filed 2010·Granted Jul 17, 2012·11 cites·11 claims
- 0984US9719421B2Gas-turbine engine with telescope-type air inlet of the engine cowling (nacelle)TODOROVIC PREDRAG·Filed 2012·Granted Aug 1, 2017·10 cites·10 claims
- 1083US10738735B2Convergent-divergent nozzle for a turbofan engine of a supersonic aircraft and method for adjusting the nozzle throat surface in a nozzle of a turbofan engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2018·Granted Aug 11, 2020·3 cites·19 claims
- 1183US9657593B2Aircraft gas turbine having a core engine casing with cooling-air tubesROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2014·Granted May 23, 2017·7 cites·5 claims
- 1282US8408008B2Scoop of a running-gap control system of an aircraft gas turbineTODOROVIC PREDRAG·Filed 2010·Granted Apr 2, 2013·13 cites·16 claims
- 1381US11105264B2Asymmetric submerged air intakeROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2019·Granted Aug 31, 2021·2 cites·20 claims
- 1479US10202940B2Engine cowling of an aircraft gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Feb 12, 2019·2 cites·8 claims
- 1579US9328694B2Aviation gas turbine thrust reversing deviceTODOROVIC PREDRAG·Filed 2012·Granted May 3, 2016·6 cites·10 claims
- 1678US10995698B2Mixer assembly group for a turbofan engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Granted May 4, 2021·3 cites·10 claims
- 1777US9194397B2Aircraft gas turbine with adjustable fanROLLS ROYCE DEUTSCHLAND·Filed 2013·Granted Nov 24, 2015·5 cites·10 claims
- 1876US8678319B2De-icing device of an aircraft gas-turbine engineTODOROVIC PREDRAG·Filed 2012·Granted Mar 25, 2014·5 cites·13 claims
- 1973US8833515B2Method for the production of a sound absorber, especially for a gas turbine exhaust coneTODOROVIC PREDRAG·Filed 2012·Granted Sep 16, 2014·4 cites·13 claims
- 2070US10442543B2Engine cowling of an aircraft gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Oct 15, 2019·2 cites·11 claims
- 2169US9784213B2Aeroengine thrust reverser arrangementROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2013·Granted Oct 10, 2017·3 cites·25 claims
- 2268US9546619B2Aircraft gas turbine thrust-reversing device having a guide railROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Jan 17, 2017·2 cites·5 claims
- 2368US8783412B2Sound absorber for a gas turbine exhaust cone, and method for the production thereofTODOROVIC PREDRAG·Filed 2012·Granted Jul 22, 2014·3 cites·16 claims
- 2468US8480032B2Aircraft de-icing device and engine nacelle of an aircraft gas turbine with de-icing deviceTODOROVIC PREDRAG·Filed 2010·Granted Jul 9, 2013·4 cites·19 claims
- 2567US10619565B2Gas turbine inletROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Apr 14, 2020·2 cites·16 claims
- 2666US10364745B2Air intake arrangementROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Jul 30, 2019·1 cites·17 claims
- 2765US10054007B2Joint between componentsROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2014·Granted Aug 21, 2018·2 cites·20 claims
- 2865US8850824B2Aircraft gas turbine with variable bypass nozzle by deforming elementTODOROVIC PREDRAG·Filed 2012·Granted Oct 7, 2014·3 cites·10 claims
- 2963US9376986B2Aircraft gas turbine thrust-reversing deviceROLLS ROYCE DEUTSCHLAND·Filed 2013·Granted Jun 28, 2016·2 cites·13 claims
- 3063US9255523B2Fastening element and de-icing device of an aircraft gas-turbine engineROLLS ROYCE DEUTSCHLAND·Filed 2013·Granted Feb 9, 2016·3 cites·20 claims
- 3162US10947927B2Mixer for an engine manufactured from at least one composite material, manufacturing method and manufacturing deviceROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Granted Mar 16, 2021·1 cites·7 claims
- 3262US9915229B2Bleed duct assembly for a gas turbine engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2014·Granted Mar 13, 2018·1 cites·12 claims
- 3362US8561940B2Arrangement for the suspension of a jet engine to a supporting structureLISIEWICZ STEPHAN·Filed 2010·Granted Oct 22, 2013·5 cites·16 claims
- 3459US11187186B2Exhaust nozzle of a gas turbine engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2019·Granted Nov 30, 2021·0 cites·20 claims
- 3558US10012176B2Aircraft gas turbine comprising a thrust-reverser device with cascade elements and an integrated rack and pinion driveROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2014·Granted Jul 3, 2018·2 cites·5 claims
- 3657US11326553B2Exhaust nozzle of a gas turbine engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2019·Granted May 10, 2022·0 cites·20 claims
- 3757US2009103975A1Attaching elementTODOROVIC PREDRAG·Filed 2008·Application pending·0 cites
- 3855US11313321B2Exhaust nozzle of a gas turbine engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2019·Granted Apr 26, 2022·0 cites·14 claims
- 3955US11215140B2Exhaust nozzle of a gas turbine engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2019·Granted Jan 4, 2022·0 cites·20 claims
- 4054US11448162B2Propelling nozzle for a turbofan engine on a supersonic aircraftROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2018·Granted Sep 20, 2022·0 cites·20 claims
- 4152US11326552B2Exhaust nozzle of a gas turbine engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2019·Granted May 10, 2022·0 cites·20 claims
- 4251US10151270B2Engine cowling of a gas turbine with thrust-reversing device and cross-sectionally adjustable outlet nozzleROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Dec 11, 2018·1 cites·17 claims
- 4350US11248561B2Exhaust nozzle of a gas turbine engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2019·Granted Feb 15, 2022·0 cites·20 claims
- 4450US10428678B2Device of a turbomachine for actuating a setting device and turbomachine with such a deviceROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Granted Oct 1, 2019·0 cites·17 claims
- 4550US9932846B2Aeroengine sealing arrangementROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2013·Granted Apr 3, 2018·0 cites·19 claims
- 4649US9963987B2Fully integrated air guide elementROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted May 8, 2018·0 cites·16 claims
- 4748US2015176527A1Aircraft gas turbine comprising an engine cowling with a thrust-reverser deviceROLLS ROYCE DEUTSCHLAND·Filed 2014·Application pending·0 cites
- 4848US2024392803A1Engine having centrifugal compressor, annular combustion chamber and a guide channel arrangement having different guide channel elementsROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2022·Application pending·0 cites
- 4947US10634006B2Guide vane of a gas turbine engine, in particular of an aircraft engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Apr 28, 2020·0 cites·13 claims
- 5047US9932932B2Aeroengine thrust reverser arrangementROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2013·Granted Apr 3, 2018·0 cites·11 claims
Showing the top 50 of 62 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →