Assignee
LITTLE DAVID A
US·9 granted patents·1 pending application·92 citations·filing 2008–2013
Top patents by PatentIndex Score
10 records- 0189US8313287B2Turbine blade squealer tip rail with fence membersLITTLE DAVID A·Filed 2009·Granted Nov 20, 2012·29 cites·20 claims
- 0286US8419356B2Turbine seal assemblyLITTLE DAVID A·Filed 2009·Granted Apr 16, 2013·25 cites·19 claims
- 0380US9062559B2Movable strut cover for exhaust diffuserLITTLE DAVID A·Filed 2011·Granted Jun 23, 2015·7 cites·17 claims
- 0480US8075256B2Ingestion resistant seal assemblyLITTLE DAVID A·Filed 2009·Granted Dec 13, 2011·18 cites·20 claims
- 0578US9109608B2Compressor airfoil tip clearance optimization systemLITTLE DAVID A·Filed 2011·Granted Aug 18, 2015·5 cites·14 claims
- 0664US10100737B2Impingement cooling arrangement having a snap-in plateLITTLE DAVID A·Filed 2013·Granted Oct 16, 2018·2 cites·9 claims
- 0759US8257025B2Combustion turbine including a diffuser section with cooling fluid passageways and associated methodsLITTLE DAVID A·Filed 2008·Granted Sep 4, 2012·6 cites·17 claims
- 0848US9291063B2Mid-section of a can-annular gas turbine engine with an improved rotation of air flow from the compressor to the turbineLITTLE DAVID A·Filed 2012·Granted Mar 22, 2016·0 cites·15 claims
- 0948US2010251689A1Multiple stage gas turbine engineLITTLE DAVID A·Filed 2010·Application pending·0 cites
- 1043US9476355B2Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor sectionLITTLE DAVID A·Filed 2012·Granted Oct 25, 2016·0 cites·15 claims
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