Inventor · disambiguated record
Alex J. Simpson
Also filed as: SIMPSON ALEX J · SIMPSON ALEX J O · Simpson Alex
17 granted patents·2 pending applications·60 citations·filing 2003–2023
91Inventor score
Files withUNITED TECHNOLOGIES CORP14HEART TEST LABORATORIES INC1RTX CORP1SNYDER DANIEL A1SWANSON TIMOTHY A1
Top patents by PatentIndex Score
19 records- 0194US10060535B2Shaped spring element for a non-contact seal deviceUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 28, 2018·12 cites·20 claims
- 0284US10612669B2Shaped spring element for a non-contact seal deviceUNITED TECHNOLOGIES CORP·Filed 2018·Granted Apr 7, 2020·3 cites·20 claims
- 0377US10598211B2Spherical bearing sleeve configured with one or more discrete collarsUNITED TECHNOLOGIES CORP·Filed 2016·Granted Mar 24, 2020·2 cites·18 claims
- 0474US9938854B2Gas turbine engine airfoil curvatureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 10, 2018·2 cites·8 claims
- 0569US10570950B2Spherical joint assembly with a spherical bearing between integral collarsUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 25, 2020·1 cites·9 claims
- 0669US10100779B2Enhanced durability drive link for high load misalignmentUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 16, 2018·2 cites·20 claims
- 0768US10634092B2Linkage assembly preventing axial rotation of the link rodUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 28, 2020·1 cites·18 claims
- 0867US7874160B2Nozzle-area ratio float biasUNITED TECHNOLOGIES CORP·Filed 2007·Granted Jan 25, 2011·7 cites·16 claims
- 0965US12345169B2Thermally compliant forward outer-diameter ring for a gas turbine engineRTX CORP·Filed 2023·Granted Jul 1, 2025·0 cites·19 claims
- 1064US10443391B2Gas turbine engine stator vane asymmetryUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 15, 2019·1 cites·14 claims
- 1162US10472970B2Gas turbine engine component having contoured rib endUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 12, 2019·2 cites·16 claims
- 1260US7225622B2Turbine engine nozzleUNITED TECHNOLOGIES CORP·Filed 2003·Granted Jun 5, 2007·13 cites·17 claims
- 1358US11248560B2Linkage assembly preventing axial rotation of the link rod for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2020·Granted Feb 15, 2022·0 cites·10 claims
- 1456USD805552SDisplay screen or portion thereof with a graphical user interfaceHEART TEST LABORATORIES INC·Filed 2016·Granted Dec 19, 2017·9 cites·1 claims
- 1554US7770399B2Gas turbine engine nozzle liner with thermally compliant attachment bracketsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Aug 10, 2010·4 cites·16 claims
- 1651US8733107B2Nozzle-area ratio float biasSWANSON TIMOTHY A·Filed 2010·Granted May 27, 2014·1 cites·19 claims
- 1743US9163582B2Convergent-divergent gas turbine nozzle comprising movable flaps having a variable thickness in a lateral directionTREAT CHRISTOPHER·Filed 2012·Granted Oct 20, 2015·0 cites·19 claims
- 1837US2016146040A1Alternating Vane AsymmetryUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 1932US2015322797A1Blade element cross-tiesSNYDER DANIEL A·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →