Inventor · disambiguated record
Reinhold Meier
Also filed as: MEIER REINHOLD
18 granted patents·17 pending applications·398 citations·filing 1992–2011
95Inventor score
Top patents by PatentIndex Score
35 records- 0191US7634854B2Method for joining blades to blade roots or rotor disks when manufacturing and/or repairing gas turbine blades or integrally bladed gas turbine rotorsMTU AERO ENGINES GMBH·Filed 2005·Granted Dec 22, 2009·25 cites·12 claims
- 0286US5701669ARepair method for lengthening turbine bladesMTU MUENCHEN GMBH·Filed 1996·Granted Dec 30, 1997·58 cites·24 claims
- 0384US5479704AProcess for repairing damaged blades of turboenginesMTU MUENCHEN GMBH·Filed 1994·Granted Jan 2, 1996·60 cites·20 claims
- 0482US7775766B2Gas turbine componentMTU AERO ENGINES GMBH·Filed 2004·Granted Aug 17, 2010·42 cites·19 claims
- 0581US6438838B1Method for repairing and producing integrally bladed rotors for a turbine or turbo engineMTU AERO ENGINES GMBH·Filed 1999·Granted Aug 27, 2002·50 cites·20 claims
- 0679US6616408B1Blade and rotor for a gas turbine and method for linking blade partsMTU AERO ENGINES GMBH·Filed 1999·Granted Sep 9, 2003·63 cites·15 claims
- 0778US6543134B2Method for reconditioning bladesMTU AERO ENGINES GMBH·Filed 2001·Granted Apr 8, 2003·22 cites·16 claims
- 0869US7841084B2Gas turbine components and method for machining gas turbine componentsMTU AERO ENGINES GMBH·Filed 2008·Granted Nov 30, 2010·10 cites·16 claims
- 0964US8158903B2Method for repairing or manufacturing a componentMEIER REINHOLD·Filed 2005·Granted Apr 17, 2012·11 cites·19 claims
- 1064US6626350B2Method of repairing metallic componentsMTU AERO ENGINES GMBH·Filed 2001·Granted Sep 30, 2003·8 cites·19 claims
- 1163US8434663B2Process for manufacturing a honeycomb sealMEIER REINHOLD·Filed 2005·Granted May 7, 2013·1 cites·21 claims
- 1257US2009041610A1Gas turbine honeycomb sealMTU AERO ENGINES GMBH·Filed 2008·Application pending·0 cites
- 1356US7559728B2Milling tool and method for milling recessesMTU AERO ENGINES GMBH·Filed 2004·Granted Jul 14, 2009·8 cites·6 claims
- 1451US2008090093A1Method for the Production of a Composite Component Comprising Two Component Sections with a Basic Adhesive Nickel Layer Located Between the Two Component SectionsMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 1550US2009101634A1Joining MethodMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 1648US2009304515A1Method and device for joining by way of inductive hf pressure welding a rotor blade with a rotor support of a gas turbine with automatic supply of the rotor bladeMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 1747US7950147B2Method for producing gas turbine componentsMTU AERO ENGINES GMBH·Filed 2004·Granted May 31, 2011·9 cites·14 claims
- 1847US5968299AFoil coating on a local region of a component and its method of production and installationMTU MUENCHEN GMBH·Filed 1997·Granted Oct 19, 1999·14 cites·8 claims
- 1946US2009096138A1Method for Production of a Honeycomb SealMEIER REINHOLD·Filed 2007·Application pending·0 cites
- 2046US2007119830A1Method for connecting componentsMTU AERO ENGINES GMBH·Filed 2005·Application pending·0 cites
- 2145US2007271759A1Method For Connecting ComponentsMEIER REINHOLD·Filed 2005·Application pending·0 cites
- 2244US2009041607A1Method for the production of a sealing segment, and sealing segment to be use in compressor and turbine componentsMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 2344US2007090152A1Method for cladding the blade tips of rotor blades of a gas turbine power plant and device for carrying out the methodMTU AERO ENGINES GMBH·Filed 2004·Application pending·0 cites
- 2443US2006131815A1Honeycomb sealMEIER REINHOLD·Filed 2003·Application pending·0 cites
- 2541US6299953B1Enclosure arrangement for fixing workpieces to be processed and a process for manufacturing and separating the enclosure arrangementMTU MUENCHEN GMBH·Filed 1992·Granted Oct 9, 2001·9 cites·28 claims
- 2640US2013187066A1Infrared emitterHELLER HANS-WILLI·Filed 2011·Application pending·0 cites
- 2739US8501297B2Honeycomb structureMEIER REINHOLD·Filed 2008·Granted Aug 6, 2013·0 cites·10 claims
- 2838US6291934B1Halogen incandescent lamp having U-shaped inner supply lead held mechanically in a fold in the foilPATENT TREUHAND GES FUER ELEKTRISCHE GLUEHLAMPEN MBH·Filed 1999·Granted Sep 18, 2001·8 cites·13 claims
- 2938US2009317548A1Gas turbine component with a thermal barrier coating, thermal barrier coating for a gas turbine component and process for producing a thermal barrier coating on a gas turbine componentMEIER REINHOLD·Filed 2007·Application pending·0 cites
- 3038US2005205644A1Method and device for holding a metallic component to be connected, especially a gas turbine bladeMEIER REINHOLD·Filed 2003·Application pending·0 cites
- 3137US2009031564A1Method of repairing a shroud segment of a gas turbineMEIER REINHOLD·Filed 2006·Application pending·0 cites
- 3237US2009304497A1Guide blade segment of a gas turbine and method for its productionMTU AERO ENGINES GMBH·Filed 2007·Application pending·0 cites
- 3335US2007273103A1Sealing DeviceMEIER REINHOLD·Filed 2005·Application pending·0 cites
- 3431US9333589B2Component and method for joining metal elementsHANRIEDER HERBERT·Filed 2007·Granted May 10, 2016·0 cites·23 claims
- 3521US2006243709A1Method and device for restoring and producing geometrically complex componentsBORN WERNER·Filed 2003·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →