Inventor · disambiguated record
Masatake Hatano
Also filed as: HATANO MASATAKE
11 granted patents·2 pending applications·2 citations·filing 2012–2017
78Inventor score
Top patents by PatentIndex Score
13 records- 0152US11752710B2Composite material, pultrusion device, and pultrusion methodMITSUBISHI HEAVY IND LTD·Filed 2017·Granted Sep 12, 2023·0 cites·4 claims
- 0252US11247417B2Composite material member, gap material, pultrusion device, and pultrusion methodMITSUBISHI HEAVY IND LTD·Filed 2017·Granted Feb 15, 2022·0 cites·7 claims
- 0349US11318710B2Joined member assembly method and joined memberMITSUBISHI HEAVY IND LTD·Filed 2017·Granted May 3, 2022·0 cites·2 claims
- 0449US11241844B2Method for inserting out-of-plane reinforcement threads and method for producing fiber-containing materialMITSUBISHI HEAVY IND LTD·Filed 2017·Granted Feb 8, 2022·0 cites·5 claims
- 0549US11192313B2Production method for a pultruded articleMITSUBISHI HEAVY IND LTD·Filed 2017·Granted Dec 7, 2021·0 cites·8 claims
- 0649US9027881B2Composite material structure and aircraft wing provided therewithTANAKA YUYA·Filed 2012·Granted May 12, 2015·1 cites·4 claims
- 0748US11396145B2Method and device for producing pultruded materialMITSUBISHI HEAVY IND LTD·Filed 2017·Granted Jul 26, 2022·0 cites·6 claims
- 0848US11059243B2Production device and production method for pultrusion molded articleMITSUBISHI HEAVY IND LTD·Filed 2017·Granted Jul 13, 2021·0 cites·3 claims
- 0947US11285679B2Device and method for producing pultruded articleMITSUBISHI HEAVY IND LTD·Filed 2017·Granted Mar 29, 2022·0 cites·6 claims
- 1047US9751608B2Composite material structure, and aircraft wing and aircraft fuselage provided therewithTANAKA YUYA·Filed 2012·Granted Sep 5, 2017·1 cites·6 claims
- 1143US2019217558A1Composite material member, reinforced molded body, pultrusion device, and pultrusion methodMITSUBISHI HEAVY IND LTD·Filed 2017·Application pending·0 cites
- 1242US2019184605A1Fiber-containing material, method for inserting out-of-plane reinforcement threads, and method for producing fiber-containing materialMITSUBISHI HEAVY IND LTD·Filed 2017·Application pending·0 cites
- 1334US11526635B2Method, design device, and design program for cross-sectional shape of fuselageMITSUBISHI HEAVY IND LTD·Filed 2017·Granted Dec 13, 2022·0 cites·4 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →