Inventor
LAURELLO VINCENT P
US25 patents
⚠️ This page may combine multiple inventors who share the name “LAURELLO VINCENT P”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
LAURELLO VINCENT P
8 patentsUS8727703B2May 20, 2014
Gas turbine engine
LAURELLO VINCENT P38 citations93
US9017013B2Apr 28, 2015
Gas turbine engine with improved cooling between turbine rotor disk elements
LAURELLO VINCENT P8 citations84
US9157331B2Oct 13, 2015
Radial active clearance control for a gas turbine engine
LAURELLO VINCENT P18 citations83
US8677766B2Mar 25, 2014
Radial pre-swirl assembly and cooling fluid metering structure for a gas turbine engine
LAURELLO VINCENT P14 citations82
US8584469B2Nov 19, 2013
Cooling fluid pre-swirl assembly for a gas turbine engine
LAURELLO VINCENT P13 citations82
US9032738B2May 19, 2015
Gas turbine compressor with bleed path
LAURELLO VINCENT P4 citations73
US9494081B2Nov 15, 2016
Turbine engine shutdown temperature control system with an elongated ejector
LAURELLO VINCENT P2 citations62
US9068461B2Jun 30, 2015
Turbine rotor disk inlet orifice for a turbine engine
LAURELLO VINCENT P3 citations62
UNITED TECHNOLOGIES CORP
6 patentsUS4553901ANov 19, 1985
Stator structure for a gas turbine engine
UNITED TECHNOLOGIES CORP59 citations96
US4236869ADec 2, 1980
Gas turbine engine having bleed apparatus with dynamic pressure recovery
UNITED TECHNOLOGIES CORP93 citations96
US4815272AMar 28, 1989
Turbine cooling and thermal control
UNITED TECHNOLOGIES CORP41 citations92
US4653267AMar 31, 1987
Thrust balancing and cooling system
UNITED TECHNOLOGIES CORP54 citations92
US4643638AFeb 17, 1987
Stator structure for supporting an outer air seal in a gas turbine engine
UNITED TECHNOLOGIES CORP23 citations82
US4648792AMar 10, 1987
Stator vane support assembly
UNITED TECHNOLOGIES CORP22 citations81
SIEMENS AG
3 patentsUS9151175B2Oct 6, 2015
Turbine abradable layer with progressive wear zone multi level ridge arrays
SIEMENS AG25 citations92
US8939716B1Jan 27, 2015
Turbine abradable layer with nested loop groove pattern
SIEMENS AG19 citations92
US9562475B2Feb 7, 2017
Vane carrier temperature control system in a gas turbine engine
SIEMENS AG9 citations84