Inventor · disambiguated record
Vincent P. Laurello
Also filed as: LAURELLO VINCENT · LAURELLO VINCENT P · LAURELLO VINCENT PAUL
34 granted patents·3 pending applications·885 citations·filing 1977–2015
98Inventor score
Files withMITSUBISHI HEAVY IND LTD10LAURELLO VINCENT P8UNITED TECHNOLOGIES CORP6SIEMENS AG4LEE CHING PANG3
Top patents by PatentIndex Score
37 records- 0197US9151175B2Turbine abradable layer with progressive wear zone multi level ridge arraysSIEMENS AG·Filed 2014·Granted Oct 6, 2015·25 cites·19 claims
- 0296US8727703B2Gas turbine engineLAURELLO VINCENT P·Filed 2010·Granted May 20, 2014·38 cites·18 claims
- 0395US8939711B2Outer rim seal assembly in a turbine engineLEE CHING-PANG·Filed 2013·Granted Jan 27, 2015·15 cites·15 claims
- 0495US8939716B1Turbine abradable layer with nested loop groove patternSIEMENS AG·Filed 2014·Granted Jan 27, 2015·19 cites·19 claims
- 0595US7033138B2Ring segment of gas turbineMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Apr 25, 2006·116 cites·4 claims
- 0695US4236869AGas turbine engine having bleed apparatus with dynamic pressure recoveryUNITED TECHNOLOGIES CORP·Filed 1977·Granted Dec 2, 1980·93 cites·7 claims
- 0794US6773225B2Gas turbine and method of bleeding gas therefromMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Aug 10, 2004·84 cites·4 claims
- 0893US9157331B2Radial active clearance control for a gas turbine engineLAURELLO VINCENT P·Filed 2011·Granted Oct 13, 2015·18 cites·16 claims
- 0990US8677766B2Radial pre-swirl assembly and cooling fluid metering structure for a gas turbine engineLAURELLO VINCENT P·Filed 2010·Granted Mar 25, 2014·14 cites·20 claims
- 1089US4653267AThrust balancing and cooling systemUNITED TECHNOLOGIES CORP·Filed 1985·Granted Mar 31, 1987·54 cites·2 claims
- 1188US8820091B2External cooling fluid injection system in a gas turbine engineTHAM KOK-MUN·Filed 2012·Granted Sep 2, 2014·17 cites·20 claims
- 1288US8578720B2Particle separator in a gas turbine engineEBERT TODD·Filed 2010·Granted Nov 12, 2013·19 cites·20 claims
- 1387US8584469B2Cooling fluid pre-swirl assembly for a gas turbine engineLAURELLO VINCENT P·Filed 2010·Granted Nov 19, 2013·13 cites·20 claims
- 1486US8613199B2Cooling fluid metering structure in a gas turbine engineKIMMEL KEITH D·Filed 2010·Granted Dec 24, 2013·12 cites·19 claims
- 1585US9562475B2Vane carrier temperature control system in a gas turbine engineSIEMENS AG·Filed 2012·Granted Feb 7, 2017·9 cites·15 claims
- 1684US9017013B2Gas turbine engine with improved cooling between turbine rotor disk elementsLAURELLO VINCENT P·Filed 2012·Granted Apr 28, 2015·8 cites·17 claims
- 1784US8272644B1Floating card sealAHO JR WILHO V·Filed 2010·Granted Sep 25, 2012·9 cites·2 claims
- 1884US4553901AStator structure for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1983·Granted Nov 19, 1985·59 cites·10 claims
- 1983US9121298B2Finned seal assembly for gas turbine enginesLEE CHING-PANG·Filed 2012·Granted Sep 1, 2015·9 cites·20 claims
- 2082US6837676B2Gas turbineMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Jan 4, 2005·45 cites·1 claims
- 2180US9260979B2Outer rim seal assembly in a turbine engineSIEMENS AG·Filed 2014·Granted Feb 16, 2016·5 cites·18 claims
- 2278US9062557B2Flow discourager integrated turbine inter-stage U-ringTHAM KOK-MUN·Filed 2011·Granted Jun 23, 2015·7 cites·9 claims
- 2372US9032738B2Gas turbine compressor with bleed pathLAURELLO VINCENT P·Filed 2012·Granted May 19, 2015·4 cites·16 claims
- 2472US6659716B1Gas turbine having thermally insulating ringsMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Dec 9, 2003·28 cites·9 claims
- 2572US4815272ATurbine cooling and thermal controlUNITED TECHNOLOGIES CORP·Filed 1987·Granted Mar 28, 1989·41 cites·2 claims
- 2671US9206904B2Seal including flexible seal stripsLEE CHING-PANG·Filed 2010·Granted Dec 8, 2015·4 cites·19 claims
- 2767US9068461B2Turbine rotor disk inlet orifice for a turbine engineLAURELLO VINCENT P·Filed 2011·Granted Jun 30, 2015·3 cites·19 claims
- 2866US7017349B2Gas turbine and bleeding method thereofMITSUBISHI HEAVY IND LTD·Filed 2003·Granted Mar 28, 2006·22 cites·6 claims
- 2964US9494081B2Turbine engine shutdown temperature control system with an elongated ejectorLAURELLO VINCENT P·Filed 2013·Granted Nov 15, 2016·2 cites·16 claims
- 3063US6786488B2Seal structure, turbine having the same, and leak-preventing seal system for rotating shaftMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Sep 7, 2004·21 cites·6 claims
- 3160US6732530B2Gas turbine compressor and clearance controlling method thereforMITSUBISHI HEAVY IND LTD·Filed 2002·Granted May 11, 2004·18 cites·10 claims
- 3255US4643638AStator structure for supporting an outer air seal in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1983·Granted Feb 17, 1987·23 cites·4 claims
- 3351US4648792AStator vane support assemblyUNITED TECHNOLOGIES CORP·Filed 1985·Granted Mar 10, 1987·22 cites·2 claims
- 3447US6655906B1Axial compressor and gas bleeding method to thrust balance disk thereofMITSUBISHI HEAVY IND LTD·Filed 2002·Granted Dec 2, 2003·9 cites·6 claims
- 3538US2010303608A1Two-shaft gas turbineMITSUBISHI HEAVY IND LTD·Filed 2006·Application pending·0 cites
- 3636US2007271930A1Gas turbine having cooling-air transfer systemMITSUBISHI HEAVY IND LTD·Filed 2006·Application pending·0 cites
- 3734US2018223683A1Gas turbine seal arrangementSIEMENS ENERGY INC·Filed 2015·Application pending·0 cites
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