Inventor · disambiguated record
Ricardo Trindade
Also filed as: TRINDADE RICARDO
29 granted patents·3 pending applications·352 citations·filing 1999–2019
96Inventor score
Files withUNITED TECHNOLOGIES CORP16PRATT & WHITNEY CANADA7PIGGUSH JUSTIN D2AGGARWALA ANDREW S1BEATTIE JEFFREY S1
Top patents by PatentIndex Score
32 records- 0195US8858159B2Gas turbine engine component having wavy cooling channels with pedestalsPIGGUSH JUSTIN D·Filed 2011·Granted Oct 14, 2014·22 cites·21 claims
- 0293US7611326B2HP turbine vane airfoil profilePRATT & WHITNEY CANADA·Filed 2006·Granted Nov 3, 2009·43 cites·16 claims
- 0389US10670273B2Cooling configurations for combustor attachment featuresUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 2, 2020·5 cites·13 claims
- 0487US8100165B2Investment casting cores and methodsPIGGUSH JUSTIN D·Filed 2008·Granted Jan 24, 2012·16 cites·21 claims
- 0585US7004720B2Cooled turbine vane platformPRATT & WHITNEY CANADA·Filed 2003·Granted Feb 28, 2006·47 cites·12 claims
- 0684US7901180B2Enhanced turbine airfoil coolingUNITED TECHNOLOGIES CORP·Filed 2007·Granted Mar 8, 2011·18 cites·29 claims
- 0782US6406260B1Heat transfer promotion structure for internally convectively cooled airfoilsPRATT & WHITNEY CANADA·Filed 1999·Granted Jun 18, 2002·69 cites·41 claims
- 0881US11078796B2Redundant entry cooling air feed hole blockage preventer for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Aug 3, 2021·3 cites·15 claims
- 0981US10690346B2Washer for combustor assemblyUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 23, 2020·3 cites·5 claims
- 1077US7097418B2Double impingement vane platform coolingPRATT & WHITNEY CANADA·Filed 2004·Granted Aug 29, 2006·39 cites·25 claims
- 1176US10704396B2Dual-wall impingement cavity for components of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jul 7, 2020·2 cites·8 claims
- 1274US8105031B2Cooling arrangement for turbine componentsTRINDADE RICARDO·Filed 2008·Granted Jan 31, 2012·16 cites·17 claims
- 1374US7258528B2Internally cooled airfoil for a gas turbine engine and methodPRATT & WHITNEY CANADA·Filed 2004·Granted Aug 21, 2007·28 cites·13 claims
- 1470US11008872B2Extension air feed hole blockage preventer for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 18, 2021·1 cites·11 claims
- 1568US10670274B2Cooling configurations for combustor attachment featuresUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 2, 2020·1 cites·15 claims
- 1667US10697307B2Hybrid cooling schemes for airfoils of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jun 30, 2020·1 cites·20 claims
- 1766US11073024B2Shape recessed surface cooling air feed hole blockage preventer for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Jul 27, 2021·1 cites·8 claims
- 1865US10954815B2Divided baffle for components of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 23, 2021·0 cites·20 claims
- 1965US10227927B2Supply duct for cooling air from gas turbine compressorUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 12, 2019·2 cites·11 claims
- 2062US9243500B2Turbine blade platform with U-channel cooling holesZELESKY MARK F·Filed 2012·Granted Jan 26, 2016·2 cites·15 claims
- 2160US10480347B2Divided baffle for components of gas turbine enginesUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 19, 2019·0 cites·20 claims
- 2260US10180067B2Mate face cooling holes for gas turbine engine componentBEATTIE JEFFREY S·Filed 2012·Granted Jan 15, 2019·2 cites·19 claims
- 2359US7246989B2Shroud leading edge coolingPRATT & WHITNEY CANADA·Filed 2004·Granted Jul 24, 2007·17 cites·8 claims
- 2456US11939883B2Airfoil with arced pedestal rowUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 26, 2024·0 cites·20 claims
- 2550US11808178B2Tangential onboard injector inlet extenderRTX CORP·Filed 2019·Granted Nov 7, 2023·0 cites·18 claims
- 2650US7278826B2Airfoil cooling passage trailing edge flow restrictionPRATT & WHITNEY CANADA·Filed 2004·Granted Oct 9, 2007·14 cites·16 claims
- 2744US11434770B2Tip cooling designUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 6, 2022·0 cites·11 claims
- 2843US2019078786A1Cooling configurations for combustor attachment featuresUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 2942US10364680B2Gas turbine engine component having platform trenchTELLER BRET M·Filed 2012·Granted Jul 30, 2019·0 cites·19 claims
- 3041US9957801B2Airfoil design having localized suction side curvaturesAGGARWALA ANDREW S·Filed 2012·Granted May 1, 2018·0 cites·16 claims
- 3134US2008005903A1External datum system and film hole positioning using core locating holesUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
- 3229US2006099073A1Aspherical dimples for heat transfer surfaces and methodDJERIDANE TOUFIK·Filed 2004·Application pending·0 cites
Join the waitlist — get patent alerts
Get an alert when Ricardo Trindade files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →