Inventor · disambiguated record
James Glaspey
Also filed as: GLASPEY JAMES
17 granted patents·1 pending application·47 citations·filing 2011–2023
91Inventor score
Top patents by PatentIndex Score
18 records- 0191US11753951B2Rotor assembly for gas turbine enginesRAYTHEON TECH CORP·Filed 2021·Granted Sep 12, 2023·2 cites·12 claims
- 0290US11136888B2Rotor assembly with active damping for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 5, 2021·6 cites·22 claims
- 0387US10344601B2Contoured flowpath surfaceUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jul 9, 2019·11 cites·20 claims
- 0486US8834098B2Detuned vane airfoil assemblyGLASPEY JAMES·Filed 2011·Granted Sep 16, 2014·11 cites·20 claims
- 0585US11092020B2Rotor assembly for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 17, 2021·3 cites·24 claims
- 0685US11009036B2Fan blade having closed metal sheathUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 18, 2021·3 cites·22 claims
- 0785US10822969B2Hybrid airfoil for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 3, 2020·3 cites·24 claims
- 0876US12286905B2Rotor assembly for gas turbine enginesRTX CORP·Filed 2023·Granted Apr 29, 2025·0 cites·20 claims
- 0973US11306601B2Pinned airfoil for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Apr 19, 2022·1 cites·9 claims
- 1070US8733156B2PMC laminate embedded hypotube latticeSTILIN NICHOLAS D·Filed 2012·Granted May 27, 2014·5 cites·20 claims
- 1167US11499566B2Fan blade having closed metal sheathRAYTHEON TECH CORP·Filed 2021·Granted Nov 15, 2022·0 cites·20 claims
- 1262US11391167B2Hybrid airfoil for gas turbine enginesRAYTHEON TECH CORP·Filed 2020·Granted Jul 19, 2022·0 cites·21 claims
- 1362US10018048B2T-shaped platform leading edge anti-rotation tabsUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jul 10, 2018·2 cites·7 claims
- 1456US11359500B2Rotor assembly with structural platforms for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 14, 2022·0 cites·19 claims
- 1554US10280767B2Fan hub attachment for leading and trailing edges of fan bladesUNITED TECHNOLOGIES CORP·Filed 2017·Granted May 7, 2019·0 cites·20 claims
- 1649US10533575B2Fan blade tip with frangible stripUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jan 14, 2020·0 cites·14 claims
- 1744US10724535B2Fan assembly of a gas turbine engine with a tip shroudUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 28, 2020·0 cites·20 claims
- 1842US2019063452A1Conical fan hub and method for reducing blade off loadsUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →