Inventor · disambiguated record
Ryan Alan Waite
Also filed as: WAITE RYAN A · WAITE RYAN ALAN
20 granted patents·1 pending application·50 citations·filing 2014–2018
91Inventor score
Files withUNITED TECHNOLOGIES CORP21
Top patents by PatentIndex Score
21 records- 0195US10641099B1Impingement cooling for a gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 5, 2020·11 cites·16 claims
- 0293US10208602B2Asymmetric diffuser opening for film cooling holesUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 19, 2019·11 cites·20 claims
- 0390US9845694B2Flow directing cover for engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 19, 2017·5 cites·12 claims
- 0490US9810084B1Gas turbine engine turbine vane baffle and serpentine cooling passageUNITED TECHNOLOGIES CORP·Filed 2015·Granted Nov 7, 2017·5 cites·20 claims
- 0587US10156147B2Method and apparatus for cooling gas turbine engine componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 18, 2018·5 cites·23 claims
- 0684US10018062B2Axial transfer tubeUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 10, 2018·4 cites·16 claims
- 0783US10240470B2Baffle for gas turbine engine vaneUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 26, 2019·7 cites·14 claims
- 0876US10041357B2Cored airfoil platform with outlet slotsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 7, 2018·2 cites·12 claims
- 0961US10808549B2Cored airfoil platform with outlet slotsUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 20, 2020·0 cites·22 claims
- 1060US10465543B2Flow directing cover for engine componentUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 5, 2019·0 cites·14 claims
- 1158US10465542B2Gas turbine engine turbine vane baffle and serpentine cooling passageUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 5, 2019·0 cites·20 claims
- 1248US10378381B2Airfoil with skin core coolingUNITED TECHNOLOGIES CORP·Filed 2014·Granted Aug 13, 2019·0 cites·8 claims
- 1348US9988912B2Thermal regulation channels for turbomachine componentsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 5, 2018·0 cites·16 claims
- 1447US9926789B2Flow splitting baffleUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 27, 2018·0 cites·19 claims
- 1545US10316751B2Shielded pass through passage in a gas turbine engine structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 11, 2019·0 cites·22 claims
- 1644US10385699B2Gas turbine engine airfoil cooling configuration with pressure gradient separatorsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 20, 2019·0 cites·19 claims
- 1741US9957815B2Gas powered turbine component including serpentine coolingUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 1, 2018·0 cites·18 claims
- 1840US10428659B2Crossover hole configuration for a flowpath component in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 1, 2019·0 cites·16 claims
- 1939US9957820B2Heat shield for a vane assembly of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 1, 2018·0 cites·17 claims
- 2038US9771814B2Tolerance resistance coverplatesUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 26, 2017·0 cites·18 claims
- 2137US2017002662A1Gas turbine engine airfoil with bi-axial skin coreUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →