Inventor · disambiguated record
David P. Houston
Also filed as: HOUSTON DAVID P · HOUSTON DAVID PAUL
23 granted patents·9 pending applications·520 citations·filing 1992–2019
96Inventor score
Files withUNITED TECHNOLOGIES CORP23HOUSTON DAVID P3BRIDGES JOSEPH W1FISK BENJAMIN T1HAYFORD RICHARD K1
Top patents by PatentIndex Score
32 records- 0198US10288010B2Geared turbofan gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2017·Granted May 14, 2019·18 cites·30 claims
- 0297US10288011B2Geared turbofan gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2017·Granted May 14, 2019·8 cites·29 claims
- 0395US10151204B2Airfoil including loose damperUNITED TECHNOLOGIES CORP·Filed 2016·Granted Dec 11, 2018·8 cites·21 claims
- 0495US9739206B2Geared turbofan gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 22, 2017·7 cites·31 claims
- 0594US9394793B1Turbomachine bladeUNITED TECHNOLOGIES CORP·Filed 2013·Granted Jul 19, 2016·38 cites·20 claims
- 0689US9885242B2Turbomachine bladeUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 6, 2018·8 cites·20 claims
- 0788US9249668B2Airfoil with break-way, free-floating damper memberFISK BENJAMIN T·Filed 2012·Granted Feb 2, 2016·12 cites·19 claims
- 0888US5924699ATurbine blade platform sealUNITED TECHNOLOGIES CORP·Filed 1996·Granted Jul 20, 1999·103 cites·30 claims
- 0986US9267380B2Airfoil including loose damperHOUSTON DAVID P·Filed 2012·Granted Feb 23, 2016·8 cites·12 claims
- 1081US5827047ATurbine blade damper and sealUNITED TECHNOLOGIES CORP·Filed 1996·Granted Oct 27, 1998·91 cites·53 claims
- 1180US9828944B2Geared turbofan gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2017·Granted Nov 28, 2017·1 cites·30 claims
- 1280US5785499ATurbine blade damper and sealUNITED TECHNOLOGIES CORP·Filed 1996·Granted Jul 28, 1998·76 cites·18 claims
- 1378US10234359B2Gas turbine engine with lifing calculations based upon actual usageUNITED TECHNOLOGIES CORP·Filed 2016·Granted Mar 19, 2019·2 cites·27 claims
- 1475US10077663B2Gas turbine engine rotor stack assemblyMALMBORG ERIC W·Filed 2011·Granted Sep 18, 2018·5 cites·18 claims
- 1575US9080449B2Gas turbine engine seal assembly having flow-through tubeBRIDGES JOSEPH W·Filed 2011·Granted Jul 14, 2015·7 cites·21 claims
- 1675US9074482B2Airfoil support method and apparatusPROPHETER-HINCKLEY TRACY A·Filed 2012·Granted Jul 7, 2015·4 cites·17 claims
- 1774US10982551B1Turbomachine bladeUNITED TECHNOLOGIES CORP·Filed 2018·Granted Apr 20, 2021·2 cites·22 claims
- 1873US6095755AGas turbine engine airfoils having increased fatigue strengthUNITED TECHNOLOGIES CORP·Filed 1996·Granted Aug 1, 2000·52 cites·31 claims
- 1970US10570755B2Fan blade rootUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 25, 2020·2 cites·8 claims
- 2065US2019024610A1Geared turbofan gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 2162US2017335796A1Geared turbofan gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 2260US5313786AGas turbine blade damperUNITED TECHNOLOGIES CORP·Filed 1992·Granted May 24, 1994·40 cites·7 claims
- 2360US2018245541A1Geared turbofan gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 2458US10704989B2Gas turbine engine with lifing calculations based upon actual usageUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 7, 2020·0 cites·21 claims
- 2555US2015345426A1Geared turbofan gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 2655US2017268428A1Geared turbofan gas turbine engine architectureHOUSTON DAVID P·Filed 2017·Application pending·0 cites
- 2753US5284421ARotor blade with platform support and damper positioning meansUNITED TECHNOLOGIES CORP·Filed 1992·Granted Feb 8, 1994·28 cites·10 claims
- 2850US10072507B2Redundant airfoil attachmentUNITED TECHNOLOGIES CORP·Filed 2012·Granted Sep 11, 2018·0 cites·13 claims
- 2943US2013192266A1Geared turbofan gas turbine engine architectureUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 3039US2013052021A1Rotor asymmetryHAYFORD RICHARD K·Filed 2011·Application pending·0 cites
- 3137US2013142640A1Alternate shroud width to provide mistuning on compressor stator clustersHOUSTON DAVID P·Filed 2011·Application pending·0 cites
- 3234US2013224028A1Component blending tool assemblyKORN NATHAN D·Filed 2012·Application pending·0 cites
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