Inventor · disambiguated record
Brian Craig
Also filed as: CRAIG BRIAN · CRAIG BRIAN R · CRAIG BRIAN RICHARD
13 granted patents·6 pending applications·10 citations·filing 2017–2025
84Inventor score
Top patents by PatentIndex Score
19 records- 0197US11603769B2Forming lined cooling aperture(s) in a turbine engine componentRAYTHEON TECH CORP·Filed 2021·Granted Mar 14, 2023·6 cites·17 claims
- 0291US11898465B2Forming lined cooling aperture(s) in a turbine engine componentRAYTHEON TECH CORP·Filed 2021·Granted Feb 13, 2024·2 cites·20 claims
- 0386US11813706B2Methods for forming cooling apertures in a turbine engine componentRAYTHEON TECH CORP·Filed 2021·Granted Nov 14, 2023·1 cites·19 claims
- 0485US2025052695A1Forming and/or inspecting cooling aperture(s) in a turbine engine componentRTX CORP·Filed 2024·Application pending·0 cites
- 0583US11542831B1Energy beam positioning during formation of a cooling apertureRAYTHEON TECH CORP·Filed 2021·Granted Jan 3, 2023·1 cites·20 claims
- 0677US12123839B2Forming and/or inspecting cooling aperture(s) in a turbine engine componentRTX CORP·Filed 2021·Granted Oct 22, 2024·0 cites·20 claims
- 0775US11913358B2Forming lined cooling aperture(s) in a turbine engine componentRAYTHEON TECH CORP·Filed 2023·Granted Feb 27, 2024·0 cites·10 claims
- 0869US12203384B1Method of restoring alloy depletion in an airfoil around cooling holesRTX CORP·Filed 2023·Granted Jan 21, 2025·0 cites·17 claims
- 0968US11913119B2Forming cooling aperture(s) in a turbine engine componentRAYTHEON TECH CORP·Filed 2021·Granted Feb 27, 2024·0 cites·20 claims
- 1066US2024293892A1Forming cooling aperture(s) in a turbine engine componentRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 1165US2025163808A1Method of restoring alloy depletion in an airfoil around cooling holesRTX CORP·Filed 2025·Application pending·0 cites
- 1261US11814979B1Systems and methods of hybrid blade tip repairRAYTHEON TECH CORP·Filed 2022·Granted Nov 14, 2023·0 cites·14 claims
- 1360US11732590B2Transition section for accommodating mismatch between other sections of a cooling aperture in a turbine engine componentRAYTHEON TECH CORP·Filed 2021·Granted Aug 22, 2023·0 cites·17 claims
- 1460US2023052285A1Forming cooling aperture(s) in a turbine engine componentRAYTHEON TECH CORP·Filed 2021·Application pending·0 cites
- 1553US10774685B2Gas turbine engine exhaust componentUNITED TECHNOLOGIES CORP·Filed 2018·Granted Sep 15, 2020·0 cites·15 claims
- 1649US2024263557A1Systems and methods of blade tip repair and manufacturing using field assisted sinteringRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 1746US12472590B2Systems and methods of blade leading edge repair using field assisted sintering technologyRAYTHEON TECH CORP·Filed 2022·Granted Nov 18, 2025·0 cites·12 claims
- 1844US10746049B2Gas turbine engine case including bearing compartmentUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 18, 2020·0 cites·20 claims
- 1941US2019040749A1Method of fabricating a turbine bladeUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →