Inventor · disambiguated record
Kenneth F. Udall
Also filed as: UDALL KENNETH F · UDALL KENNETH FRANKLIN
44 granted patents·4 pending applications·1,375 citations·filing 1993–2016
98Inventor score
Top patents by PatentIndex Score
48 records- 0197US7806363B2Engine mounting assemblyROLLS ROYCE PLC·Filed 2005·Granted Oct 5, 2010·56 cites·17 claims
- 0297US6073439ADucted fan gas turbine engineROLLS ROYCE PLC·Filed 1998·Granted Jun 13, 2000·90 cites·7 claims
- 0396US8430622B2Turbofan gas turbine engineWEBSTER JOHN RICHARD·Filed 2007·Granted Apr 30, 2013·30 cites·11 claims
- 0496US6575694B1Gas turbine engine blade containment assemblyROLLS ROYCE PLC·Filed 2001·Granted Jun 10, 2003·111 cites·26 claims
- 0596US6109022ATurbofan with frangible rotor supportROLLS ROYCE PLC·Filed 1998·Granted Aug 29, 2000·110 cites·9 claims
- 0696US5746391AMounting for coupling a turbofan gas turbine engine to an aircraft structureROLLS ROYCE PLC·Filed 1996·Granted May 5, 1998·256 cites·31 claims
- 0795US6935591B2Mounting arrangement for a gas turbine engineROLLS ROYCE PLC·Filed 2004·Granted Aug 30, 2005·77 cites·9 claims
- 0895US6009701ADucted fan gas turbine engine having a frangible connectionROLLS ROYCE PLC·Filed 1997·Granted Jan 4, 2000·73 cites·9 claims
- 0994US6708925B2Mounting arrangement for a gas turbine engineROLLS ROYCE PLC·Filed 2002·Granted Mar 23, 2004·70 cites·17 claims
- 1090US7086219B2Cowl structure for a gas turbine engineROLLS ROYCE PLC·Filed 2005·Granted Aug 8, 2006·24 cites·2 claims
- 1189US8100638B2Centering deviceUDALL KENNETH F·Filed 2009·Granted Jan 24, 2012·11 cites·20 claims
- 1289US7654075B2Fan static structureROLLS ROYCE PLC·Filed 2006·Granted Feb 2, 2010·29 cites·14 claims
- 1388US9701412B2Aircraft engine mountROLLS ROYCE PLC·Filed 2014·Granted Jul 11, 2017·12 cites·18 claims
- 1488US5409184AMounting for coupling a turbofan gas turbine engine to an aircraft structureROLLS ROYCE PLC·Filed 1994·Granted Apr 25, 1995·94 cites·22 claims
- 1587US8444085B2Support structureSTRETTON RICHARD G·Filed 2011·Granted May 21, 2013·12 cites·11 claims
- 1687US6494032B2Ducted fan gas turbine engine with frangible connectionROLLS ROYCE PLC·Filed 2001·Granted Dec 17, 2002·41 cites·6 claims
- 1786US8123489B2Hollow aerofoil and a method of manufacturing a hollow aerofoilUDALL KENNETH F·Filed 2008·Granted Feb 28, 2012·28 cites·39 claims
- 1885US7845158B2Turbine engine mounting arrangementROLLS ROYCE PLC·Filed 2007·Granted Dec 7, 2010·22 cites·9 claims
- 1984US7143975B2Landing arrangement for an aircraftROLLS ROYCE PLC·Filed 2005·Granted Dec 5, 2006·19 cites·14 claims
- 2080US8434995B2Duct wall for a fan of a gas turbine enginePOOL CLARE L·Filed 2010·Granted May 7, 2013·10 cites·14 claims
- 2180US7527476B2Rotor assembly and annulus filler for gas turbine engine compressorROLLS ROYCE PLC·Filed 2005·Granted May 5, 2009·11 cites·30 claims
- 2279US6892526B2Cowl structure for a gas turbine engineROLLS ROYCE PLC·Filed 2003·Granted May 17, 2005·26 cites·12 claims
- 2377US8511974B2Control mechanismHOOD IAN A·Filed 2010·Granted Aug 20, 2013·10 cites·9 claims
- 2475US8506234B2Duct wall for a fan of a gas turbine engineBROOKS RICHARD V·Filed 2010·Granted Aug 13, 2013·6 cites·5 claims
- 2574US8303187B2Bearing arrangementUDALL KENNETH F·Filed 2009·Granted Nov 6, 2012·4 cites·17 claims
- 2672US7806364B1Containment system for a gas turbine engineROLLS ROYCE PLC·Filed 2007·Granted Oct 5, 2010·6 cites·20 claims
- 2769US9039376B2Support ring for a rotary assemblyROLLS ROYCE PLC·Filed 2012·Granted May 26, 2015·5 cites·15 claims
- 2867US8840114B2Assembly comprising a rotatable componentDIXON JEFFREY A·Filed 2012·Granted Sep 23, 2014·5 cites·14 claims
- 2967US7891167B2Gas turbine engine flow reverserROLLS ROYCE PLC·Filed 2007·Granted Feb 22, 2011·7 cites·30 claims
- 3066US8371802B2Shaft stabiliserROLLS ROYCE PLC·Filed 2009·Granted Feb 12, 2013·8 cites·11 claims
- 3165US6098399ADucted fan gas turbine engineROLLS ROYCE PLC·Filed 1998·Granted Aug 8, 2000·42 cites·8 claims
- 3261US9109733B2Hydraulic fluid transfer couplingUDALL KENNETH F·Filed 2011·Granted Aug 18, 2015·3 cites·16 claims
- 3361US6827548B2Rotor assemblies for gas turbine enginesROLLS ROYCE PLC·Filed 2002·Granted Dec 7, 2004·22 cites·10 claims
- 3460US9809299B2Propeller blade retentionROLLS ROYCE PLC·Filed 2014·Granted Nov 7, 2017·3 cites·24 claims
- 3555US9434467B2Catcher ring arrangementROLLS ROYCE PLC·Filed 2013·Granted Sep 6, 2016·2 cites·13 claims
- 3655US8985946B2Mounting systemUDALL KENNETH F·Filed 2012·Granted Mar 24, 2015·2 cites·12 claims
- 3754US8444084B2Aeroengine mountingUDALL KENNETH F·Filed 2007·Granted May 21, 2013·4 cites·18 claims
- 3854US7597499B2Retention arrangementROLLS ROYCE PLC·Filed 2006·Granted Oct 6, 2009·3 cites·19 claims
- 3952US2013272871A1Turbofan as turbine engineWEBSTER JOHN RICHARD·Filed 2013·Application pending·0 cites
- 4049US7523604B2Thrust reverser mounting structureROLLS ROYCE PLC·Filed 2006·Granted Apr 28, 2009·1 cites·6 claims
- 4146US7229252B2Rotor assembly retaining apparatusROLLS ROYCE PLC·Filed 2004·Granted Jun 12, 2007·12 cites·8 claims
- 4245US9845682B2Fan discROLLS ROYCE PLC·Filed 2015·Granted Dec 19, 2017·0 cites·12 claims
- 4345US2017175571A1Method of manufacturing a metal matrix reinforced composite component and a composite component formed by the methodROLLS ROYCE PLC·Filed 2016·Application pending·0 cites
- 4444US9809317B2Engine mountROLLS ROYCE PLC·Filed 2014·Granted Nov 7, 2017·0 cites·12 claims
- 4541US6971855B2Blade arrangement for gas turbine engineROLLS ROYCE PLC·Filed 2003·Granted Dec 6, 2005·5 cites·17 claims
- 4640US2008245925A1Aircraft configurationROLLS ROYCE PLC·Filed 2007·Application pending·0 cites
- 4738US5370501AFan for a ducted fan gas turbine engineROLLS ROYCE PLC·Filed 1993·Granted Dec 6, 1994·13 cites·6 claims
- 4838US2012315141A1Flow mixerUDALL KENNETH F·Filed 2011·Application pending·0 cites
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