Inventor · disambiguated record
Adam P. Generale
Also filed as: GENERALE ADAM · GENERALE ADAM P
22 granted patents·3 pending applications·28 citations·filing 2016–2023
91Inventor score
Top patents by PatentIndex Score
25 records- 0193US11473444B2Ceramic airfoil with cooling air turnUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 18, 2022·9 cites·20 claims
- 0290US10934857B2Shell and spar airfoilUNITED TECHNOLOGIES CORP·Filed 2018·Granted Mar 2, 2021·5 cites·20 claims
- 0388US11492914B1Engine with cooling passage circuit for air prior to ceramic componentRAYTHEON TECH CORP·Filed 2020·Granted Nov 8, 2022·2 cites·18 claims
- 0487US11162368B2Airfoil assembly with ceramic airfoil pieces and sealUNITED TECHNOLOGIES CORP·Filed 2019·Granted Nov 2, 2021·3 cites·19 claims
- 0581US11608749B2Airfoil having environmental barrier topcoats that vary in composition by locationUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 21, 2023·2 cites·6 claims
- 0678US10822963B2Axial flow cooling scheme with castable structural rib for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 3, 2020·2 cites·19 claims
- 0777US11131212B2Gas turbine engine cooling componentUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 28, 2021·2 cites·21 claims
- 0876US12044146B2Airfoil having environmental barrier topcoats that vary in composition by locationRAYTHEON TECH CORP·Filed 2023·Granted Jul 23, 2024·0 cites·17 claims
- 0975US10711624B2Airfoil with geometrically segmented coating sectionUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jul 14, 2020·2 cites·13 claims
- 1071US11078844B2Thermal gradient reducing device for gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 3, 2021·1 cites·18 claims
- 1160US11092015B2Airfoil with metallic shieldUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 17, 2021·0 cites·19 claims
- 1259US11242758B2Trailing edge insert for airfoil vaneRAYTHEON TECH CORP·Filed 2019·Granted Feb 8, 2022·0 cites·20 claims
- 1356US11339667B2Cooling arrangement including overlapping diffusersRAYTHEON TECH CORP·Filed 2020·Granted May 24, 2022·0 cites·20 claims
- 1456US11280201B2Baffle with tailUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 22, 2022·0 cites·12 claims
- 1555US11261749B2Components for gas turbine enginesRAYTHEON TECH CORP·Filed 2020·Granted Mar 1, 2022·0 cites·20 claims
- 1653US10648351B2Gas turbine engine cooling componentUNITED TECHNOLOGIES CORP·Filed 2017·Granted May 12, 2020·0 cites·16 claims
- 1752US10822962B2Vane platform leading edge recessed pocket with coverUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 3, 2020·0 cites·18 claims
- 1852US10513947B2Adjustable flow split platform cooling for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2017·Granted Dec 24, 2019·0 cites·20 claims
- 1946US11415002B2Baffle with impingement holesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 16, 2022·0 cites·24 claims
- 2045US2020182068A1Axial flow cooling scheme with structural rib for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 2144US10655496B2Platform flow turning elements for gas turbine engine componentsUNITED TECHNOLOGIES CORP·Filed 2017·Granted May 19, 2020·0 cites·13 claims
- 2244US2021108517A1Cmc airfoil with cooling holesUNITED TECHNOLOGIES CORP·Filed 2019·Application pending·0 cites
- 2343US10619492B2Vane air inlet with filletUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 14, 2020·0 cites·18 claims
- 2442US11371360B2Components for gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jun 28, 2022·0 cites·16 claims
- 2542US2019345833A1Vane including internal radiant heat shieldUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
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