Inventor · disambiguated record
Nicholas Francis Martin
Also filed as: MARTIN JR NICHOLAS F · MARTIN JR NICHOLAS FRANCIS · MARTIN NICHOLAS F · MARTIN NICHOLAS FRANCIS
27 granted patents·9 pending applications·481 citations·filing 2002–2019
97Inventor score
Files withGEN ELECTRIC16SIEMENS AG10SIEMENS ENERGY INC3BRUNELLI MARCO CLAUDIO PIO2MARTIN NICHOLAS F2
Top patents by PatentIndex Score
36 records- 0197US9151175B2Turbine abradable layer with progressive wear zone multi level ridge arraysSIEMENS AG·Filed 2014·Granted Oct 6, 2015·25 cites·19 claims
- 0296US7114911B2Variable camber and stagger airfoil and methodGEN ELECTRIC·Filed 2004·Granted Oct 3, 2006·86 cites·16 claims
- 0395US10507518B2Hybrid component with cooling channels and corresponding processSIEMENS AG·Filed 2016·Granted Dec 17, 2019·9 cites·10 claims
- 0495US8939711B2Outer rim seal assembly in a turbine engineLEE CHING-PANG·Filed 2013·Granted Jan 27, 2015·15 cites·15 claims
- 0595US8939716B1Turbine abradable layer with nested loop groove patternSIEMENS AG·Filed 2014·Granted Jan 27, 2015·19 cites·19 claims
- 0693US9920646B2Turbine abradable layer with compound angle, asymmetric surface area ridge and groove patternSIEMENS AG·Filed 2015·Granted Mar 20, 2018·7 cites·18 claims
- 0793US9249680B2Turbine abradable layer with asymmetric ridges or groovesSIEMENS ENERGY INC·Filed 2014·Granted Feb 2, 2016·16 cites·20 claims
- 0891US9759073B1Turbine airfoil having near-wall cooling insertSIEMENS ENERGY INC·Filed 2016·Granted Sep 12, 2017·6 cites·10 claims
- 0991US6814543B2Method and apparatus for bucket natural frequency tuningGEN ELECTRIC·Filed 2002·Granted Nov 9, 2004·71 cites·23 claims
- 1084US9957818B2Removably attachable snubber assemblySIEMENS ENERGY INC·Filed 2015·Granted May 1, 2018·4 cites·16 claims
- 1181US11298742B2Hybrid component with cooling channels and corresponding processSIEMENS AG·Filed 2019·Granted Apr 12, 2022·0 cites·6 claims
- 1281US9017012B2Ring segment with cooling fluid supply trenchBRUNELLI MARCO CLAUDIO PIO·Filed 2011·Granted Apr 28, 2015·13 cites·19 claims
- 1380US9260979B2Outer rim seal assembly in a turbine engineSIEMENS AG·Filed 2014·Granted Feb 16, 2016·5 cites·18 claims
- 1480US7121803B2Compressor blade with dovetail slotted to reduce stress on the airfoil leading edgeGEN ELECTRIC·Filed 2004·Granted Oct 17, 2006·28 cites·22 claims
- 1579US7374396B2Bolt-on radial bleed manifoldGEN ELECTRIC·Filed 2005·Granted May 20, 2008·18 cites·19 claims
- 1676US7165944B2Compressor blade with dovetail slotted to reduce stress on the airfoil leading edgeGEN ELECTRIC·Filed 2005·Granted Jan 23, 2007·15 cites·39 claims
- 1776US7090462B2Compressor bleed air manifold for blade clearance controlGEN ELECTRIC·Filed 2004·Granted Aug 15, 2006·22 cites·20 claims
- 1876US7024744B2Frequency-tuned compressor stator blade and related methodGEN ELECTRIC·Filed 2004·Granted Apr 11, 2006·32 cites·17 claims
- 1974US6902376B2Compressor blade with dovetail slotted to reduce stress on the airfoil leading edgeGEN ELECTRIC·Filed 2002·Granted Jun 7, 2005·20 cites·20 claims
- 2072US7104759B2Compressor blade platform extension and methods of retrofitting blades of different blade anglesGEN ELECTRIC·Filed 2004·Granted Sep 12, 2006·19 cites·13 claims
- 2169US10767504B2Flexible damper for turbine bladesSIEMENS AG·Filed 2016·Granted Sep 8, 2020·1 cites·13 claims
- 2269US6769877B2Undercut leading edge for compressor blades and related methodGEN ELECTRIC·Filed 2002·Granted Aug 3, 2004·25 cites·13 claims
- 2356US7195453B2Compressor stator floating tip shroud and related methodGEN ELECTRIC·Filed 2004·Granted Mar 27, 2007·16 cites·10 claims
- 2455US11260641B2Apparatus for reticulation of adhesive and methods of use thereofAMERICAN HONDA MOTOR·Filed 2019·Granted Mar 1, 2022·1 cites·21 claims
- 2555US7661924B2Method and apparatus for assembling turbine enginesGEN ELECTRIC·Filed 2007·Granted Feb 16, 2010·4 cites·16 claims
- 2651US7686576B2Method and apparatus for assembling gas turbine enginesGEN ELECTRIC·Filed 2006·Granted Mar 30, 2010·3 cites·17 claims
- 2745US2006198726A1Apparatus for eliminating compressor stator vibration induced by tip leakage vortex burstingGEN ELECTRIC·Filed 2005·Application pending·0 cites
- 2840US2009123275A1Apparatus for eliminating compressor stator vibration induced by TIP leakage vortex burstingGEN ELECTRIC·Filed 2008·Application pending·0 cites
- 2939US2019136700A1Ceramic matrix composite tip shroud assembly for gas turbinesSIEMENS AG·Filed 2016·Application pending·0 cites
- 3036US2018135432A1Turbine airfoil with internal cooling channelsSIEMENS AG·Filed 2015·Application pending·0 cites
- 3136US2018179901A1Turbine blade with contoured tip shroudSIEMENS AG·Filed 2015·Application pending·0 cites
- 3236US2011033311A1Turbine Airfoil Cooling System with Pin Fin Cooling ChambersMARTIN NICHOLAS F·Filed 2009·Application pending·0 cites
- 3334US2007107218A1Formed tenons for gas turbine stator vanesGEN ELECTRIC·Filed 2005·Application pending·0 cites
- 3432US8657577B2Gas turbine with securing plate between blade base and diskMARTIN NICHOLAS F·Filed 2009·Granted Feb 25, 2014·1 cites·6 claims
- 3531US2014286751A1Cooled turbine ring segments with intermediate pressure plenumsBRUNELLI MARCO CLAUDIO PIO·Filed 2013·Application pending·0 cites
- 3629US2004213672A1Undercut leading edge for compressor blades and related methodFiled 2003·Application pending·0 cites
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