Assignee
LAURELLO VINCENT P
US·8 granted patents·100 citations·filing 2010–2013
Top patents by PatentIndex Score
8 records- 0196US8727703B2Gas turbine engineLAURELLO VINCENT P·Filed 2010·Granted May 20, 2014·38 cites·18 claims
- 0293US9157331B2Radial active clearance control for a gas turbine engineLAURELLO VINCENT P·Filed 2011·Granted Oct 13, 2015·18 cites·16 claims
- 0390US8677766B2Radial 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
- 0487US8584469B2Cooling fluid pre-swirl assembly for a gas turbine engineLAURELLO VINCENT P·Filed 2010·Granted Nov 19, 2013·13 cites·20 claims
- 0584US9017013B2Gas turbine engine with improved cooling between turbine rotor disk elementsLAURELLO VINCENT P·Filed 2012·Granted Apr 28, 2015·8 cites·17 claims
- 0672US9032738B2Gas turbine compressor with bleed pathLAURELLO VINCENT P·Filed 2012·Granted May 19, 2015·4 cites·16 claims
- 0767US9068461B2Turbine rotor disk inlet orifice for a turbine engineLAURELLO VINCENT P·Filed 2011·Granted Jun 30, 2015·3 cites·19 claims
- 0864US9494081B2Turbine engine shutdown temperature control system with an elongated ejectorLAURELLO VINCENT P·Filed 2013·Granted Nov 15, 2016·2 cites·16 claims
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