Inventor · disambiguated record
Karl Schreiber
Also filed as: SCHREIBER KARL · SCHREIBER KARL J
43 granted patents·15 pending applications·449 citations·filing 1977–2019
98Inventor score
Files withSCHREIBER KARL22ROLLS ROYCE DEUTSCHLAND19ROLLS ROYCE DEUTSCHLAND LTD & CO KG11POLAROID CORP4FORSCHUNGSZENTRUM JUELICH GMBH1
Top patents by PatentIndex Score
58 records- 0191US8677622B2Intake cone in a fiber compound material for a gas turbine engine and method for its manufactureSCHREIBER KARL·Filed 2007·Granted Mar 25, 2014·14 cites·9 claims
- 0291US8100662B2Fan blade made of a textile composite materialSCHREIBER KARL·Filed 2007·Granted Jan 24, 2012·41 cites·19 claims
- 0391US7918644B2Axial-flow compressor for a gas turbine engineROLLS ROYCE DEUTSCHLAND·Filed 2007·Granted Apr 5, 2011·21 cites·20 claims
- 0489US8777577B2Hybrid fan blade and method for its manufactureSCHREIBER KARL·Filed 2007·Granted Jul 15, 2014·10 cites·2 claims
- 0588US8540492B2Intake cone in a fiber compound material for a gas-turbine engineSCHREIBER KARL·Filed 2010·Granted Sep 24, 2013·11 cites·18 claims
- 0687US9429026B2Decoupled compressor blade of a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2013·Granted Aug 30, 2016·9 cites·19 claims
- 0786US8646279B2Segment component in high-temperature casting material for an annular combustion chamber, annular combustion chamber for an aircraft engine, aircraft engine and method for the manufacture of an annular combustion chamberSCHREIBER KARL·Filed 2012·Granted Feb 11, 2014·9 cites·15 claims
- 0885US8685297B2Method for the manufacture of a fiber-composite component and fiber-composite component manufactured according to this methodSCHREIBER KARL·Filed 2007·Granted Apr 1, 2014·8 cites·6 claims
- 0983US7033131B2Fan blade for a gas-turbine engineROLLS ROYCE DEUTSCHLAND·Filed 2004·Granted Apr 25, 2006·28 cites·23 claims
- 1082US7744346B2Leading edge configuration for compressor blades of gas turbine enginesROLLS ROYCE DEUTSCHLAND·Filed 2006·Granted Jun 29, 2010·22 cites·19 claims
- 1181US9964117B2Compressor blade of a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted May 8, 2018·4 cites·17 claims
- 1280US8246478B2Engine shaft in the form of a fiber-composite plastic tube with metallic driving and driven protrusionsSCHREIBER KARL·Filed 2009·Granted Aug 21, 2012·7 cites·7 claims
- 1380US8221087B2Stator vanes of a stator vane cascade of an aircraft gas turbineSCHREIBER KARL·Filed 2009·Granted Jul 17, 2012·5 cites·16 claims
- 1479US8242406B2Method for the manufacture of a bliskSCHREIBER KARL·Filed 2009·Granted Aug 14, 2012·9 cites·16 claims
- 1579US7156622B2Compressor blade for an aircraft engineROLLS ROYCE DEUTSCHLAND·Filed 2004·Granted Jan 2, 2007·34 cites·16 claims
- 1676US8251664B2Fan blade for a gas-turbine engineSCHREIBER KARL·Filed 2007·Granted Aug 28, 2012·14 cites·10 claims
- 1775US9908173B2Method for producing a component, component and turbomachine having a componentSCHREIBER KARL·Filed 2012·Granted Mar 6, 2018·1 cites·8 claims
- 1873US7076942B2Protective ring for the fan protective casing of a gas turbine engineROLLS ROYCE DEUTSCHLAND·Filed 2003·Granted Jul 18, 2006·27 cites·16 claims
- 1971US7211178B2Fixture for electro-chemical machiningROLLS ROYCE DEUTSCHLAND·Filed 2004·Granted May 1, 2007·7 cites·11 claims
- 2071US6251494B1Honeycomb structure seal for a gas turbine and method of making sameROLLS ROYCE DEUTSCHLAND·Filed 1999·Granted Jun 26, 2001·48 cites·20 claims
- 2169US9828860B2Compressor blade of a gas turbine as well as method for manufacturing said bladeROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2013·Granted Nov 28, 2017·3 cites·6 claims
- 2269US6997995B2Method for producing components with a high load capacity from TiAl alloysROLLS ROYCE DEUTSCHLAND·Filed 2001·Granted Feb 14, 2006·9 cites·8 claims
- 2368US9126361B2Method for the manufacture of hybrid components for aircraft gas turbinesSCHREIBER KARL·Filed 2009·Granted Sep 8, 2015·4 cites·8 claims
- 2468US8647011B2Engine shaft of hybrid designSCHREIBER KARL·Filed 2010·Granted Feb 11, 2014·3 cites·18 claims
- 2567US8827654B2Compressor blade of a gas-turbine engine with a self-sharpening leading-edge structureSCHREIBER KARL·Filed 2011·Granted Sep 9, 2014·3 cites·20 claims
- 2667US4144065APolysilicates in photographic products and processesPOLAROID CORP·Filed 1978·Granted Mar 13, 1979·8 cites·20 claims
- 2766US6532658B2Process for the manufacture of a blade/vane of a turbomachineROLLS ROYCE DEUTSCHLAND·Filed 2000·Granted Mar 18, 2003·22 cites·6 claims
- 2864US8251830B2Engine shaft for a gas-turbine engineSCHREIBER KARL·Filed 2009·Granted Aug 28, 2012·10 cites·11 claims
- 2964US7832245B2Method and apparatus for hot forming of sheet metal in titanium-base alloysROLLS ROYCE DEUTSCHLAND·Filed 2008·Granted Nov 16, 2010·3 cites·19 claims
- 3062US8831172B2Method for filmless radiographic inspection of componentsSCHREIBER KARL·Filed 2011·Granted Sep 9, 2014·1 cites·16 claims
- 3162US7251888B2Hollow fan blade for aircraft engines and method for its manufactureROLLS ROYCE DEUTSCHLAND·Filed 2004·Granted Aug 7, 2007·11 cites·22 claims
- 3258US4359518AStripping sheet for use with diffusion transfer film unitPOLAROID CORP·Filed 1981·Granted Nov 16, 1982·9 cites·22 claims
- 3357US7204089B2Arrangement for the cooling of thermally highly loaded componentsROLLS ROYCE DEUTSCHLAND·Filed 2004·Granted Apr 17, 2007·12 cites·20 claims
- 3457US4267255ANovel photographic processing compositionPOLAROID CORP·Filed 1979·Granted May 12, 1981·5 cites·24 claims
- 3556US2010140230A1Method for the manufacture of a welded rotor for a gas-turbine engineROLLS ROYCE DEUTSCHLAND·Filed 2009·Application pending·0 cites
- 3655US10024234B2Panels of a fan of a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted Jul 17, 2018·1 cites·14 claims
- 3755US2009249622A1Method for the manufacture of integrally bladed rotorsSCHREIBER KARL·Filed 2009·Application pending·0 cites
- 3854US2019301298A1Liner structure from metallic material, method for manufacturing a liner structure and component with a liner structureROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2019·Application pending·0 cites
- 3950US7781696B2Method for joining components in titanium aluminide by brazingROLLS ROYCE DEUTSCHLAND·Filed 2003·Granted Aug 24, 2010·4 cites·25 claims
- 4050US2009265933A1Method for the manufacture of turbine or compressor rotors for gas-turbine enginesSCHREIBER KARL·Filed 2009·Application pending·0 cites
- 4149US10605254B2Bearing element and turbomachine with a bearing elementROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Granted Mar 31, 2020·0 cites·20 claims
- 4249US2010109184A1Method for the manufacture of an engine shaftROLLS ROYCE DEUTSCHLAND·Filed 2009·Application pending·0 cites
- 4348US2014030109A1low-Modulus Gas-Turbine Compressor BladeROLLS ROYCE DEUTSCHLAND·Filed 2013·Application pending·0 cites
- 4443US9278385B2Method for the manufacture of a workpiece with defined surfaceSCHREIBER KARL·Filed 2011·Granted Mar 8, 2016·0 cites·13 claims
- 4543US2010129651A1Hybrid component for a gas-turbine engineROLLS ROYCE DEUTSCHLAND·Filed 2009·Application pending·0 cites
- 4642US9664069B2Panels of a fan of a gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2015·Granted May 30, 2017·0 cites·8 claims
- 4742US4104068ASilver halide emulsions containing microvoidsPOLAROID CORP·Filed 1977·Granted Aug 1, 1978·2 cites·14 claims
- 4842US2010259013A1Abradable labyrinth seal for a fluid-flow machineROLLS ROYCE DEUTSCHLAND·Filed 2010·Application pending·0 cites
- 4942US2019376392A1Gas turbineROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2017·Application pending·0 cites
- 5041US2009087309A1Protective ring for the fan casing of a gas-turbine engineSCHREIBER KARL·Filed 2007·Application pending·0 cites
Showing the top 50 of 58 patent records by PatentIndex Score.
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