Inventor · disambiguated record
Raymond Surace
Also filed as: SURACE RAYMOND · SURACE RAYMOND C
77 granted patents·11 pending applications·424 citations·filing 2001–2025
98Inventor score
Top patents by PatentIndex Score
88 records- 0198US11313242B2Thin seal for an engineRAYTHEON TECH CORP·Filed 2019·Granted Apr 26, 2022·17 cites·17 claims
- 0298US10465545B2Thin seal for an engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Nov 5, 2019·17 cites·5 claims
- 0398US10012099B2Thin seal for an engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jul 3, 2018·19 cites·9 claims
- 0496US12006842B1Airfoil with sandwich compositeRAYTHEON TECH CORP·Filed 2023·Granted Jun 11, 2024·4 cites·14 claims
- 0595US11536148B2Vane arc segment with thermal insulation elementRAYTHEON TECH CORP·Filed 2020·Granted Dec 27, 2022·3 cites·15 claims
- 0694US11939888B2Airfoil anti-rotation ring and assemblyRAYTHEON TECH CORP·Filed 2022·Granted Mar 26, 2024·2 cites·8 claims
- 0792US11781486B2Ceramic component having silicon layer and barrier layerRAYTHEON TECH CORP·Filed 2023·Granted Oct 10, 2023·2 cites·7 claims
- 0890US11555452B1Ceramic component having silicon layer and barrier layerRAYTHEON TECH CORP·Filed 2021·Granted Jan 17, 2023·2 cites·14 claims
- 0990US11215059B1Gas turbine engine airfoil with variable pitch cooling holesRAYTHEON TECH CORP·Filed 2020·Granted Jan 4, 2022·4 cites·18 claims
- 1088US12392247B2Airfoil with sandwich composite flangeRAYTHEON TECH CORP·Filed 2023·Granted Aug 19, 2025·1 cites·14 claims
- 1188US11492914B1Engine with cooling passage circuit for air prior to ceramic componentRAYTHEON TECH CORP·Filed 2020·Granted Nov 8, 2022·2 cites·18 claims
- 1288US10309226B2Airfoil having panelsUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jun 4, 2019·4 cites·22 claims
- 1387US11952917B2Vane multiplet with conjoined singlet vanesRAYTHEON TECH CORP·Filed 2022·Granted Apr 9, 2024·1 cites·15 claims
- 1487US11773742B2Cooled cooling air for blade air seal through outer chamberUNITED TECHNOLOGIES CORP·Filed 2020·Granted Oct 3, 2023·2 cites·2 claims
- 1587US10132191B2Variable area turbine arrangement with secondary flow modulationUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 20, 2018·7 cites·20 claims
- 1687US8403631B2Gas turbine engine component cooling schemeSURACE RAYMOND·Filed 2010·Granted Mar 26, 2013·10 cites·6 claims
- 1787US7125225B2Cooled rotor blade with vibration damping deviceUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 24, 2006·52 cites·19 claims
- 1886US6490791B1Method for repairing cracks in a turbine blade root trailing edgeUNITED TECHNOLOGIES CORP·Filed 2001·Granted Dec 10, 2002·48 cites·16 claims
- 1985US11434768B2Multi-walled airfoil coreRAYTHEON TECH CORP·Filed 2021·Granted Sep 6, 2022·1 cites·20 claims
- 2084US11125087B2Needled ceramic matrix composite cooling passagesRAYTHEON TECH CORP·Filed 2018·Granted Sep 21, 2021·1 cites·17 claims
- 2183US10677079B2Airfoil with ceramic airfoil piece having internal cooling circuitUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jun 9, 2020·3 cites·16 claims
- 2283US8137068B2Castings, casting cores, and methodsSURACE RAYMOND·Filed 2008·Granted Mar 20, 2012·24 cites·23 claims
- 2380US11725522B2Airfoil with wishbone fiber structureRAYTHEON TECH CORP·Filed 2021·Granted Aug 15, 2023·1 cites·14 claims
- 2480US7445432B2Enhanced serpentine cooling with U-shaped divider ribUNITED TECHNOLOGIES CORP·Filed 2006·Granted Nov 4, 2008·20 cites·19 claims
- 2579US8403632B2Gas turbine engine component cooling schemeSURACE RAYMOND·Filed 2010·Granted Mar 26, 2013·5 cites·10 claims
- 2679US7121801B2Cooled rotor blade with vibration damping deviceUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 17, 2006·37 cites·28 claims
- 2779US6932575B2Blade damperUNITED TECHNOLOGIES CORP·Filed 2003·Granted Aug 23, 2005·43 cites·22 claims
- 2878US12371997B2Cooling arrangement for gas turbine engine componentRTX CORP·Filed 2024·Granted Jul 29, 2025·0 cites·19 claims
- 2977US12454893B2Airfoil anti-rotation ring and assemblyRTX CORP·Filed 2024·Granted Oct 28, 2025·0 cites·6 claims
- 3077US12152505B2Vane arc segment with thermal insulation elementRAYTHEON TECH CORP·Filed 2022·Granted Nov 26, 2024·0 cites·11 claims
- 3177US11591915B2Multi-flow cooling circuit for gas turbine engine flowpath componentUNITED TECHNOLOGIES CORP·Filed 2019·Granted Feb 28, 2023·2 cites·16 claims
- 3277US11220917B1Diffused cooling arrangement for gas turbine engine componentsRAYTHEON TECH CORP·Filed 2020·Granted Jan 11, 2022·1 cites·21 claims
- 3376US8016546B2Systems and methods for providing vane platform coolingUNITED TECHNOLOGIES CORP·Filed 2007·Granted Sep 13, 2011·17 cites·20 claims
- 3475US10036282B2Vane support systemsUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 31, 2018·2 cites·14 claims
- 3575US7862291B2Gas turbine engine component cooling schemeUNITED TECHNOLOGIES CORP·Filed 2007·Granted Jan 4, 2011·11 cites·12 claims
- 3675US2024401487A1Airfoil with sandwich compositeRTX CORP·Filed 2024·Application pending·0 cites
- 3774US12055068B2Airfoil leading edge venturi cooling passageRTX CORP·Filed 2023·Granted Aug 6, 2024·0 cites·16 claims
- 3873US10415407B2Airfoil pieces secured with endwall sectionUNITED TECHNOLOGIES CORP·Filed 2016·Granted Sep 17, 2019·1 cites·17 claims
- 3972US12474052B1Dovetail features on panel rails or impingement sheet to hold panelsRTX CORP·Filed 2024·Granted Nov 18, 2025·0 cites·16 claims
- 4072US11015457B2Multi-walled airfoil coreUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 25, 2021·1 cites·12 claims
- 4172US7217093B2Rotor blade with a stick damperUNITED TECHNOLOGIES CORP·Filed 2004·Granted May 15, 2007·29 cites·14 claims
- 4272US2021381387A1Needled ceramic matrix composite cooling passagesRAYTHEON TECH CORP·Filed 2021·Application pending·0 cites
- 4371US10036264B2Variable area gas turbine engine component having movable spar and shellUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jul 31, 2018·3 cites·20 claims
- 4470US12479773B2Ceramic matrix composite part release from chemical vapor infiltration toolingRAYTHEON TECH CORP·Filed 2022·Granted Nov 25, 2025·0 cites·14 claims
- 4569US11118474B2Vane cooling structuresUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 14, 2021·1 cites·15 claims
- 4668US12270545B1T-head bolts or hollow flanged bushing with one thread or grooved end in a multi-liner arrangementRTX CORP·Filed 2024·Granted Apr 8, 2025·0 cites·20 claims
- 4768US12006836B2Cooling arrangement for gas turbine engine componentRAYTHEON TECH CORP·Filed 2022·Granted Jun 11, 2024·0 cites·16 claims
- 4868US11788419B1Airfoil leading edge venturi cooling passageRAYTHEON TECH CORP·Filed 2022·Granted Oct 17, 2023·0 cites·15 claims
- 4968US2024140878A1Method for densification of cmc articleRTX CORP·Filed 2023·Application pending·0 cites
- 5067US11118471B2Variable area vane endwall treatmentsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Sep 14, 2021·3 cites·19 claims
Showing the top 50 of 88 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →