Inventor · disambiguated record
Michael Ray Tuertscher
Also filed as: TUERTSCHER MICHAEL RAY
14 granted patents·1 pending application·161 citations·filing 2014–2023
92Inventor score
Files withGEN ELECTRIC15
Top patents by PatentIndex Score
15 records- 0198US10378373B2Flow path assembly with airfoils inserted through flow path boundaryGEN ELECTRIC·Filed 2017·Granted Aug 13, 2019·15 cites·20 claims
- 0297US10385709B2Methods and features for positioning a flow path assembly within a gas turbine engineGEN ELECTRIC·Filed 2017·Granted Aug 20, 2019·13 cites·20 claims
- 0396US9915159B2Ceramic matrix composite nozzle mounted with a strut and concepts thereofGEN ELECTRIC·Filed 2014·Granted Mar 13, 2018·46 cites·16 claims
- 0495US10309240B2Method and system for interfacing a ceramic matrix composite component to a metallic componentGEN ELECTRIC·Filed 2015·Granted Jun 4, 2019·29 cites·24 claims
- 0594US10017425B2Methods and materials for forming in-situ cavities for silicon-based ceramic matrix composite componentsGEN ELECTRIC·Filed 2014·Granted Jul 10, 2018·20 cites·20 claims
- 0690US11466580B2CMC nozzle with interlocking mechanical joint and fabricationGEN ELECTRIC·Filed 2018·Granted Oct 11, 2022·6 cites·21 claims
- 0786US11391171B2Methods and features for positioning a flow path assembly within a gas turbine engineGEN ELECTRIC·Filed 2019·Granted Jul 19, 2022·3 cites·20 claims
- 0886US10400616B2Turbine nozzle with impingement baffleGEN ELECTRIC·Filed 2014·Granted Sep 3, 2019·14 cites·14 claims
- 0985US11149569B2Flow path assembly with airfoils inserted through flow path boundaryGEN ELECTRIC·Filed 2019·Granted Oct 19, 2021·3 cites·6 claims
- 1085US10301954B2Turbine airfoil trailing edge cooling passageGEN ELECTRIC·Filed 2016·Granted May 28, 2019·4 cites·17 claims
- 1180US11092023B2Ceramic matrix composite nozzle mounted with a strut and concepts thereofGEN ELECTRIC·Filed 2018·Granted Aug 17, 2021·2 cites·20 claims
- 1276US10180073B2Mounting apparatus for low-ductility turbine nozzleGEN ELECTRIC·Filed 2014·Granted Jan 15, 2019·5 cites·9 claims
- 1368US10738628B2Joint for band features on turbine nozzle and fabricationGEN ELECTRIC·Filed 2018·Granted Aug 11, 2020·1 cites·23 claims
- 1463US12467369B2Composite component having an additively printed inner portionGEN ELECTRIC·Filed 2023·Granted Nov 11, 2025·0 cites·19 claims
- 1537US2017051619A1Cmc nozzles with split endwalls for gas turbine enginesGEN ELECTRIC·Filed 2015·Application pending·0 cites
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →