Inventor · disambiguated record
Carsten Clemen
Also filed as: CLEMEN CARSTEN
50 granted patents·25 pending applications·242 citations·filing 2007–2025
98Inventor score
Top patents by PatentIndex Score
75 records- 0197US9447973B2Combustion chamber of a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Sep 20, 2016·12 cites·12 claims
- 0294US8444378B2Bypass duct of a turbofan engineCLEMEN CARSTEN·Filed 2010·Granted May 21, 2013·15 cites·15 claims
- 0392US8678760B2Bypass duct of a turbofan engineCLEMEN CARSTEN·Filed 2011·Granted Mar 25, 2014·17 cites·4 claims
- 0491US10465708B2Diffuser part for a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Nov 5, 2019·7 cites·14 claims
- 0589US10012390B2Combustion chamber of a gas turbine with bolted combustion chamber headROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Jul 3, 2018·7 cites·15 claims
- 0688US10330204B2Burner seal of a gas turbine and method for manufacturing the sameROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Granted Jun 25, 2019·4 cites·13 claims
- 0788US9506653B2Combustion chamber of a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Nov 29, 2016·5 cites·6 claims
- 0886US9683743B2Combustion chamber tile of a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2013·Granted Jun 20, 2017·8 cites·20 claims
- 0985US10712006B2Combustion chamber arrangement of a gas turbine and aircraft gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Granted Jul 14, 2020·4 cites·18 claims
- 1084US9303875B2Gas-turbine combustion chamber having non-symmetrical fuel nozzlesROLLS ROYCE DEUTSCHLAND·Filed 2013·Granted Apr 5, 2016·9 cites·16 claims
- 1184US8696306B2Bypass duct of a turbofan engineCLEMEN CARSTEN·Filed 2011·Granted Apr 15, 2014·9 cites·20 claims
- 1283US8683811B2Jet engine with compressor air circulation and method for operating the jet engineCLEMEN CARSTEN·Filed 2008·Granted Apr 1, 2014·21 cites·1 claims
- 1382US10837646B2Combustion chamber shingle arrangement of a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2018·Granted Nov 17, 2020·3 cites·10 claims
- 1482US10670270B2Gas turbine combustion chamber with wall contouringROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2016·Granted Jun 2, 2020·3 cites·8 claims
- 1581US8221080B2Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub coneCLEMEN CARSTEN·Filed 2009·Granted Jul 17, 2012·10 cites·9 claims
- 1680US10174947B1Combustion chamber tile of a gas turbine and method for its manufactureROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2013·Granted Jan 8, 2019·6 cites·13 claims
- 1780US9370789B2Method for producing a component by direct laser depositioning using first and second lasers operated at different powersROLLS ROYCE DEUTSCHLAND·Filed 2014·Granted Jun 21, 2016·3 cites·5 claims
- 1880US8784042B2Fan downstream guide vanes of a turbofan engineCLEMEN CARSTEN·Filed 2011·Granted Jul 22, 2014·5 cites·11 claims
- 1979US8152473B2Airfoil design for rotor and stator blades of a turbomachineCLEMEN CARSTEN·Filed 2007·Granted Apr 10, 2012·19 cites·8 claims
- 2078US9696036B2Gas turbine combustion chamber tile having effusion cooling holes including straight and offset sectionsROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2014·Granted Jul 4, 2017·5 cites·6 claims
- 2177US9206766B2Jet engine device with a bypass ductCLEMEN CARSTEN·Filed 2012·Granted Dec 8, 2015·6 cites·20 claims
- 2276US9279587B2Device for mixing fuel and air of a jet engineCLEMEN CARSTEN·Filed 2012·Granted Mar 8, 2016·3 cites·20 claims
- 2376US8047802B2Course of leading edges for turbomachine componentsROLLS ROYCE DEUTSCHLAND·Filed 2008·Granted Nov 1, 2011·12 cites·4 claims
- 2474US9803869B2Gas turbine combustion chamber and method for manufacturing the sameROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Oct 31, 2017·2 cites·5 claims
- 2573US10041415B2Burner seal for gas-turbine combustion chamber head and heat shieldROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2014·Granted Aug 7, 2018·4 cites·7 claims
- 2673US8220276B2Gas-turbine compressor with bleed-air tappingCLEMEN CARSTEN·Filed 2009·Granted Jul 17, 2012·16 cites·16 claims
- 2771US10591162B2Heat shield for a gas turbine combustion chamberROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2014·Granted Mar 17, 2020·3 cites·8 claims
- 2870US8262351B2Casing structure for stabilizing flow in a fluid-flow machineCLEMEN CARSTEN·Filed 2009·Granted Sep 11, 2012·6 cites·18 claims
- 2969US9366148B2Assembly of an axial turbomachine and method for manufacturing an assembly of this typeROLLS ROYCE DEUTSCHLAND·Filed 2013·Granted Jun 14, 2016·3 cites·18 claims
- 3069US9097259B2Bleed air outlet in the bypass duct of a turbofan engineCLEMEN CARSTEN·Filed 2011·Granted Aug 4, 2015·2 cites·6 claims
- 3168US12196165B2Fuel nozzle having different first and second discharge orifices for providing a hydrogen-air mixtureROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2022·Granted Jan 14, 2025·0 cites·16 claims
- 3267US12196420B2Connecting apparatus for the flow connection between a fuel feed line system and a nozzle apparatus, nozzle apparatus and gas turbine arrangementROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2023·Granted Jan 14, 2025·0 cites·22 claims
- 3366US8523517B2Cross-sectional profile for the struts or the fairing of struts and service lines of a turbofan engineCLEMEN CARSTEN·Filed 2010·Granted Sep 3, 2013·3 cites·5 claims
- 3464US9366436B2Combustion chamber of a gas turbineROLLS ROYCE DEUTSCHLAND·Filed 2015·Granted Jun 14, 2016·1 cites·8 claims
- 3563US8701385B2Method and apparatus for the operation of a turboprop aircraft engine provided with pusher propellersCLEMEN CARSTEN·Filed 2009·Granted Apr 22, 2014·7 cites·14 claims
- 3663US2025297739A1Injector assembly for a gas turbine and aircraftROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2025·Application pending·0 cites
- 3762US12007118B2Pilot arrangement, nozzle device, method and gas turbine arrangementROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2023·Granted Jun 11, 2024·0 cites·15 claims
- 3860US12460822B2Combustion chamber assembly for operation with liquid and/or gaseous fuel, gas turbine assembly and methodROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2023·Granted Nov 4, 2025·0 cites·18 claims
- 3960US2025276802A1Method for operating an aircraft, and aircraftROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2025·Application pending·0 cites
- 4059US12435876B2Combustion chamber assembly for an engine with at least one heat exchanger channel for fuel to be injectedROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2022·Granted Oct 7, 2025·0 cites·26 claims
- 4159US11549862B2Measuring device comprising at least one fluid channel for guiding a measurement fluidROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2019·Granted Jan 10, 2023·0 cites·17 claims
- 4256US2024345605A1Method for producing a nonlinear cylindrical spring and use of such a springROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2024·Application pending·0 cites
- 4355US2025198616A1Nozzle assembly with a central fuel supply and at least one air channelROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2023·Application pending·0 cites
- 4453US10808557B2Nozzle assembly for a combustion chamber of an engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2018·Granted Oct 20, 2020·0 cites·13 claims
- 4553US2021285640A1Nozzle with jet generator channel for fuel to be injected into a combustion chamber of an engineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2021·Application pending·0 cites
- 4653US2025257693A1Valve unit for controlling the fuel feed in a fuel supply system, in particular of an aircraftROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2025·Application pending·0 cites
- 4752US12320302B2Drive system for an aircraft, aircraft having a drive system and method for operating an aircraftROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2023·Granted Jun 3, 2025·0 cites·13 claims
- 4851US12320301B2Combustion chamber module having an annular combustion chamberROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2024·Granted Jun 3, 2025·0 cites·13 claims
- 4951US2009238677A1Centrifugal compressor with air extraction and return at the casingCLEMEN CARSTEN·Filed 2009·Application pending·0 cites
- 5051US2025237381A1Nozzle assembly for a combustion chamber of an engine, and burner sealROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2025·Application pending·0 cites
Showing the top 50 of 75 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →