Inventor · disambiguated record
Garrett Kernozicky
Also filed as: KERNOZICKY GARRETT
7 granted patents·7 pending applications·13 citations·filing 2008–2025
77Inventor score
Top patents by PatentIndex Score
14 records- 0189US12318877B2Blend approach based inspection and analysis systems and methodsRAYTHEON TECH CORP·Filed 2022·Granted Jun 3, 2025·2 cites·9 claims
- 0289US12135209B2Airfoil tool mountRAYTHEON TECH CORP·Filed 2022·Granted Nov 5, 2024·2 cites·17 claims
- 0365US12442634B2Visual and/or dimensional tip inspection systems and methodsRAYTHEON TECH CORP·Filed 2022·Granted Oct 14, 2025·0 cites·12 claims
- 0464US12163897B2Multi-stage inspection systems and methodsRAYTHEON TECH CORP·Filed 2022·Granted Dec 10, 2024·0 cites·17 claims
- 0561US2025020557A1In situ engine airfoil process compensated resonance testingRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 0660US2025020558A1Localized Rework Using Powder be Fusion Generated SegmentsRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 0759US2025020062A1Localized rework using directed energy depositionRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 0857US12410711B2Bladed rotor inspection, analysis and repair systems and methodsRAYTHEON TECH CORP·Filed 2023·Granted Sep 9, 2025·0 cites·20 claims
- 0957US2023314341A1Data transfer systems and methods for analysis inputsRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 1055US2025347593A1Blade tip wear detection system and methods for aerospace componentsRTX CORP·Filed 2025·Application pending·0 cites
- 1153US7970555B2Method for developing a repair process to correct a deformed gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2008·Granted Jun 28, 2011·7 cites·25 claims
- 1245US2023315937A1Partial repair systems and methods for integrally bladed rotorsRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 1341US2023315069A1Inspection data management systems and methodsRAYTHEON TECH CORP·Filed 2022·Application pending·0 cites
- 1432US8122601B2Methods for correcting twist angle in a gas turbine engine bladeKERNOZICKY GARRETT·Filed 2008·Granted Feb 28, 2012·2 cites·23 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →