Inventor · disambiguated record
Anthony J. Rawlinson
Also filed as: RAWLINSON ANTHONY · RAWLINSON ANTHONY J · RAWLINSON ANTHONY JOHN
8 granted patents·7 pending applications·59 citations·filing 2003–2019
84Inventor score
Top patents by PatentIndex Score
15 records- 0194US9797261B2Internal cooling of engine componentsROLLS ROYCE PLC·Filed 2015·Granted Oct 24, 2017·21 cites·16 claims
- 0278US8714918B2Turbine stage shroud segmentTIBBOTT IAN·Filed 2011·Granted May 6, 2014·7 cites·8 claims
- 0366US10337342B2Stator assembly for a gas turbine engineROLLS ROYCE PLC·Filed 2017·Granted Jul 2, 2019·1 cites·8 claims
- 0462US9068472B2Endwall component for a turbine stage of a gas turbine engineRAWLINSON ANTHONY J·Filed 2012·Granted Jun 30, 2015·3 cites·9 claims
- 0561US7080972B2AerofoilROLLS ROYCE PLC·Filed 2003·Granted Jul 25, 2006·21 cites·7 claims
- 0652US8240994B2Cooling arrangementIRELAND PETER T·Filed 2008·Granted Aug 14, 2012·4 cites·11 claims
- 0745US2014178207A1Turbine bladeROLLS ROYCE PLC·Filed 2013·Application pending·0 cites
- 0844US2015159488A1Turbine rotor blade of a gas turbine and method for cooling a blade tip of a turbine rotor blade of a gas turbineROLLS ROYCE DEUTSCHLAND·Filed 2014·Application pending·0 cites
- 0943US8540480B2Aerofoil having a plurality cooling air flowsRAWLINSON ANTHONY J·Filed 2009·Granted Sep 24, 2013·2 cites·14 claims
- 1042US2020224875A1Double-wall geometryROLLS ROYCE PLC·Filed 2019·Application pending·0 cites
- 1137US2012251295A1Gas turbine engine componentTURNER LYNNE H·Filed 2012·Application pending·0 cites
- 1237US2005232770A1Flow control arrangementROLLS ROYCE PLC·Filed 2005·Application pending·0 cites
- 1336US2012057961A1Turbine stage shroud segmentTIBBOTT IAN·Filed 2011·Application pending·0 cites
- 1435US9200535B2Aerofoil blade or vaneROLLS ROYCE PLC·Filed 2012·Granted Dec 1, 2015·0 cites·11 claims
- 1535US2018128117A1Self-sealing impingement cooling tube for a turbine vaneROLLS ROYCE PLC·Filed 2017·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →