Inventor · disambiguated record
Takayuki Kurimura
Also filed as: KURIMURA TAKAYUKI
11 granted patents·6 pending applications·23 citations·filing 2004–2022
83Inventor score
Files withMITSUBISHI HEAVY IND AERO ENGINES LTD7MITSUBISHI HEAVY IND LTD5MITSUBISHI HITACHI POWER SYS3MITSUBISHI HITACHI POWER SYS LTD2
Top patents by PatentIndex Score
17 records- 0186US11034106B2Method for repairing ceramic matrix composite and ceramic matrix composite memberMITSUBISHI HEAVY IND LTD·Filed 2018·Granted Jun 15, 2021·2 cites·7 claims
- 0283US11365159B2Coated member and method of manufacturing the sameMITSUBISHI HEAVY IND AERO ENGINES LTD·Filed 2016·Granted Jun 21, 2022·2 cites·9 claims
- 0378US10570754B2Steam turbine rotor blade, method for manufacturing steam turbine rotor blade, and steam turbineMITSUBISHI HITACHI POWER SYS·Filed 2015·Granted Feb 25, 2020·2 cites·10 claims
- 0468US11608303B2Coated member and method of manufacturing the sameMITSUBISHI HEAVY IND AERO ENGINES LTD·Filed 2022·Granted Mar 21, 2023·0 cites·8 claims
- 0568US11407688B2Coating structure, turbine part having same, and method for manufacturing coating structureMITSUBISHI HITACHI POWER SYS LTD·Filed 2017·Granted Aug 9, 2022·1 cites·10 claims
- 0668US2021245460A1Ceramic matrix composite memberMITSUBISHI HEAVY IND LTD·Filed 2021·Application pending·0 cites
- 0766US7334328B2Method of manufacturing axis seals having reduced gas leakage properties and a rotary machine using axis sealsMITSUBISHI HEAVY IND LTD·Filed 2004·Granted Feb 26, 2008·16 cites·13 claims
- 0865US2023082214A1Coating method, coating layer, and turbine shroudMITSUBISHI HEAVY IND AERO ENGINES LTD·Filed 2022·Application pending·0 cites
- 0959US11530168B2Coating method, coating layer, and turbine shroudMITSUBISHI HEAVY IND AERO ENGINES LTD·Filed 2017·Granted Dec 20, 2022·0 cites·6 claims
- 1055US10465548B2Shroud and method for implementing abradable coatingMITSUBISHI HEAVY IND AERO ENGINES LTD·Filed 2017·Granted Nov 5, 2019·0 cites·8 claims
- 1147US2015136280A1Method for setting aging conditions and method for producing turbine vanesMITSUBISHI HITACHI POWER SYS·Filed 2013·Application pending·0 cites
- 1246US2019283271A1Manufacturing method of turbine blade memberMITSUBISHI HEAVY IND LTD·Filed 2018·Application pending·0 cites
- 1342US11059751B2Coated member, coating material, and method of manufacturing coated memberMITSUBISHI HEAVY IND AERO ENGINES LTD·Filed 2016·Granted Jul 13, 2021·0 cites·10 claims
- 1441US10994301B2Method for constructing abradable coating, and shroudMITSUBISHI HEAVY IND AERO ENGINES LTD·Filed 2017·Granted May 4, 2021·0 cites·7 claims
- 1538US2016209343A1Thermal load testing device and thermal load testing methodMITSUBISHI HITACHI POWER SYS·Filed 2016·Application pending·0 cites
- 1636US11441447B2Ring-segment surface-side member, ring-segment support-side member, ring segment, stationary-side member unit, and methodMITSUBISHI HITACHI POWER SYS LTD·Filed 2017·Granted Sep 13, 2022·0 cites·14 claims
- 1736US2019041061A1Joined structure, combustor, and combustion deviceMITSUBISHI HEAVY IND LTD·Filed 2016·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →