Inventor · disambiguated record
Timothy James Conti
Also filed as: CONTI TIMOTHY JAMES
18 granted patents·2 pending applications·25 citations·filing 2015–2025
90Inventor score
Top patents by PatentIndex Score
20 records- 0191US11066188B2Method and apparatus for locating and forming fastener holes in a replacement tip section of a rotor bladeSIKORSKY AIRCRAFT CORP·Filed 2018·Granted Jul 20, 2021·5 cites·16 claims
- 0290US10668604B2Non-destructive cold extractions of press fit bushingsSIKORSKY AIRCRAFT CORP·Filed 2015·Granted Jun 2, 2020·10 cites·9 claims
- 0384US11325695B2Rotor blade internal structure for trailing edge actuationLOCKHEED CORP·Filed 2020·Granted May 10, 2022·2 cites·19 claims
- 0481US10899440B2Rotor blade tip design for improved hover and cruise performanceSIKORSKY AIRCRAFT CORP·Filed 2018·Granted Jan 26, 2021·4 cites·15 claims
- 0580US12110104B2Method of stabilizing articulated rotor bladeLOCKHEED CORP·Filed 2022·Granted Oct 8, 2024·1 cites·13 claims
- 0676US12252240B2Commonly manufactured rotor bladeLOCKHEED CORP·Filed 2024·Granted Mar 18, 2025·0 cites·11 claims
- 0776US11242140B2Method of removal and replacement of a tip section of a rotor bladeSIKORSKY AIRCRAFT CORP·Filed 2018·Granted Feb 8, 2022·2 cites·16 claims
- 0874US11655052B2Method and apparatus for locating and forming fastener holes in a replacement tip section of a rotor bladeSIKORSKY AIRCRAFT CORP·Filed 2021·Granted May 23, 2023·0 cites·17 claims
- 0971US12129023B2Method of removal and replacement of a tip section of a rotor bladeSIKORSKY AIRCRAFT CORP·Filed 2021·Granted Oct 29, 2024·0 cites·20 claims
- 1071US11919627B2Commonly manufactured rotor bladeLOCKHEED CORP·Filed 2022·Granted Mar 5, 2024·0 cites·12 claims
- 1170US2024326994A1Electrical conductor system for a rotor blade and method of manufacturing the electrical conductor systemLOCKHEED CORP·Filed 2024·Application pending·0 cites
- 1268US11498671B2Replacement tip section for a rotor blade and method of replacing a rotor blade tip sectionLOCKHEED CORP·Filed 2019·Granted Nov 15, 2022·1 cites·9 claims
- 1368US2025010983A1Method of stabilizing articulated rotor bladeLOCKHEED CORP·Filed 2024·Application pending·0 cites
- 1463US11548129B2Method and assembly for extracting press fit bushingsSIKORSKY AIRCRAFT CORP·Filed 2020·Granted Jan 10, 2023·0 cites·16 claims
- 1562US12037108B2Replacement tip section for a rotor blade and method of replacing a rotor blade tip sectionLOCKHEED CORP·Filed 2022·Granted Jul 16, 2024·0 cites·10 claims
- 1661US12214872B2Tip end joint arrangement for a rotor blade with reconfigurable attributes for structural and aerodynamic tuningLOCKHEED CORP·Filed 2023·Granted Feb 4, 2025·0 cites·17 claims
- 1761US12030624B2Electrical conductor system for a rotor blade and method of manufacturing the electrical conductor systemLOCKHEED CORP·Filed 2021·Granted Jul 9, 2024·0 cites·16 claims
- 1860US12497166B2Tip end joint arrangement for a rotor blade with reconfigurable attributes for structural and aerodynamic tuningLOCKHEED CORP·Filed 2025·Granted Dec 16, 2025·0 cites·20 claims
- 1952US11794887B1Removable trailing edge assembly and system for rotor blade trailing edge actuationLOCKHEED CORP·Filed 2022·Granted Oct 24, 2023·0 cites·19 claims
- 2038US10589849B2Trim tab retention system, an aircraft employing same and a method of retaining a trim tab within a blade housingSIKORSKY AIRCRAFT CORP·Filed 2016·Granted Mar 17, 2020·0 cites·13 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →