Inventor · disambiguated record
Bryan Olver
Also filed as: OLVER BRYAN · OLVER BRYAN W · OLVER BRYAN WILLIAM
33 granted patents·3 pending applications·483 citations·filing 2002–2020
97Inventor score
Top patents by PatentIndex Score
36 records- 0198US7861981B2Protective saddle mount for cable tiePRATT & WHITNEY CANADA·Filed 2008·Granted Jan 4, 2011·69 cites·13 claims
- 0295US7861512B2Turbofan bypass duct air cooled fluid cooler installationPRATT & WHITNEY CANADA·Filed 2006·Granted Jan 4, 2011·97 cites·6 claims
- 0392US10364700B2Method for forming a composite part of a gas turbine enginePRATT & WHITNEY CANADA·Filed 2016·Granted Jul 30, 2019·5 cites·18 claims
- 0490US8979491B2Turbofan mounting arrangementHEYERMAN JEFFREY BERNARD·Filed 2011·Granted Mar 17, 2015·18 cites·15 claims
- 0590US6851267B2Compact quick attach starter-generator installationPRATT & WHITNEY CANADA·Filed 2002·Granted Feb 8, 2005·37 cites·8 claims
- 0689US7377100B2Bypass duct fluid coolerPRATT & WHITNEY CANADA·Filed 2004·Granted May 27, 2008·62 cites·5 claims
- 0788US8171738B2Gas turbine internal manifold mounting arrangementFISH JASON·Filed 2006·Granted May 8, 2012·17 cites·14 claims
- 0886US9784129B2Rear mount assembly for gas turbine enginePRATT & WHITNEY CANADA·Filed 2014·Granted Oct 10, 2017·13 cites·20 claims
- 0982US11466622B2Composite aerospace componentPRATT & WHITNEY CANADA·Filed 2018·Granted Oct 11, 2022·1 cites·16 claims
- 1081US7862293B2Low profile bleed air coolerPRATT & WHITNEY CANADA·Filed 2007·Granted Jan 4, 2011·19 cites·15 claims
- 1180US9068508B2Gas turbine internal manifold mounting arrangementFISH JASON·Filed 2012·Granted Jun 30, 2015·5 cites·16 claims
- 1280US8621839B2Gas turbine engine breather exhaust oil collectorALECU DANIEL T·Filed 2009·Granted Jan 7, 2014·19 cites·15 claims
- 1380US8222165B2Composite fire shieldOLVER BRYAN WILLIAM·Filed 2008·Granted Jul 17, 2012·7 cites·17 claims
- 1480US7013651B2Compact quick attach starter-generator installationPRATT & WHITNEY CANADA·Filed 2004·Granted Mar 21, 2006·21 cites·8 claims
- 1579US8231142B2Fluid conduit coupling with leakage detectionOLVER BRYAN W·Filed 2009·Granted Jul 31, 2012·14 cites·5 claims
- 1678US10753229B2Mounting arrangement for mounting a fluid cooler to a gas turbine engine casePRATT & WHITNEY CANADA·Filed 2016·Granted Aug 25, 2020·2 cites·9 claims
- 1774US6942452B2Grommeted bypass duct penetrationPRATT & WHITNEY CANADA·Filed 2002·Granted Sep 13, 2005·28 cites·16 claims
- 1871US11002148B2Method for forming a composite part of a gas turbine enginePRATT & WHITNEY CANADA·Filed 2019·Granted May 11, 2021·0 cites·8 claims
- 1969US11274602B2Air cooler for gas turbine enginePRATT & WHITNEY CANADA·Filed 2019·Granted Mar 15, 2022·1 cites·13 claims
- 2068US9068476B2Hybrid metal/composite link rod for turbofan gas turbine engineCAULFEILD STEPHEN·Filed 2011·Granted Jun 30, 2015·5 cites·19 claims
- 2168US7854120B2Fuel manifold with reduced lossesPRATT & WHITNEY CANADA·Filed 2006·Granted Dec 21, 2010·10 cites·20 claims
- 2265US9879606B2Method of supplying fuel to an internal fuel manifoldPRATT & WHITNEY CANADA·Filed 2014·Granted Jan 30, 2018·2 cites·15 claims
- 2365US7703286B2Internal fuel manifold and fuel fairing interfacePRATT & WHITNEY CANADA·Filed 2006·Granted Apr 27, 2010·8 cites·8 claims
- 2462US8313293B2Turbofan mounting systemHEYERMAN JEFFREY BERNARD·Filed 2009·Granted Nov 20, 2012·8 cites·17 claims
- 2561US9909501B2Acoustic structure for a gas turbine enginePRATT & WHITNEY CANADA·Filed 2014·Granted Mar 6, 2018·2 cites·19 claims
- 2661US9267435B2Support links with lockable adjustment featurePRATT & WHITNEY CANADA·Filed 2013·Granted Feb 23, 2016·1 cites·8 claims
- 2756US8567202B2Support links with lockable adjustment featureHEYERMAN JEFFREY BERNARD·Filed 2009·Granted Oct 29, 2013·4 cites·9 claims
- 2853US8757540B2Nacelle inlet lipOLVER BRYAN W·Filed 2008·Granted Jun 24, 2014·3 cites·10 claims
- 2951US11111856B2Turbofan engine and core link thereforePRATT & WHITNEY CANADA·Filed 2019·Granted Sep 7, 2021·0 cites·14 claims
- 3048US11530710B2Aircraft pneumatic systemPRATT & WHITNEY CANADA·Filed 2020·Granted Dec 20, 2022·0 cites·7 claims
- 3146US2010278642A1Bypass lip sealPRATT & WHITNEY CANADA·Filed 2010·Application pending·0 cites
- 3245US7320212B2Side-fed shielded internal fuel manifold inlet tubePRATT & WHITNEY CANADA·Filed 2004·Granted Jan 22, 2008·5 cites·12 claims
- 3344US10711625B2Wall construction for gaspath traversing componentPRATT & WHITNEY CANADA·Filed 2013·Granted Jul 14, 2020·0 cites·20 claims
- 3443US2006288687A1Grommeted bypass duct penetrationPRATT & WHITNEY CANADA·Filed 2005·Application pending·0 cites
- 3541US9784132B2Voltage discharge channelling assembly for a gas turbine enginePRATT & WHITNEY CANADA·Filed 2015·Granted Oct 10, 2017·0 cites·16 claims
- 3641US2008053060A1Bypass lip sealPRATT & WHITNEY CANADA·Filed 2006·Application pending·0 cites
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →