Inventor · disambiguated record
Daniel David Snook
Also filed as: SNOOK DANIEL · SNOOK DANIEL D · SNOOK DANIEL DAVID
23 granted patents·9 pending applications·1,016 citations·filing 2000–2012
97Inventor score
Files withGEN ELECTRIC13SNOOK DANIEL DAVID8KONINKL PHILIPS ELECTRONICS NV4BENJAMIN EDWARD D1BENJAMIN JR EDWARD DURELL1
Top patents by PatentIndex Score
32 records- 0199US6654420B1Video encoding-methodKONINKL PHILIPS ELECTRONICS NV·Filed 2000·Granted Nov 25, 2003·361 cites·4 claims
- 0297US8266913B2Power plant and method of useSNOOK DANIEL DAVID·Filed 2011·Granted Sep 18, 2012·76 cites·18 claims
- 0396US8453462B2Method of operating a stoichiometric exhaust gas recirculation power plantWICHMANN LISA ANNE·Filed 2011·Granted Jun 4, 2013·89 cites·17 claims
- 0496US8347600B2Power plant and method of operationGEN ELECTRIC·Filed 2011·Granted Jan 8, 2013·79 cites·20 claims
- 0594US8266883B2Power plant start-up method and method of venting the power plantDION OUELLET NOEMIE·Filed 2011·Granted Sep 18, 2012·79 cites·20 claims
- 0691US6857855B1Airfoil shape for a turbine bucketGEN ELECTRIC·Filed 2003·Granted Feb 22, 2005·67 cites·22 claims
- 0788US6442204B1Video encoding method and systemKONINKL PHILIPS ELECTRONICS NV·Filed 2000·Granted Aug 27, 2002·46 cites·3 claims
- 0886US9115595B2Clearance control system for a gas turbineSNOOK DANIEL DAVID·Filed 2012·Granted Aug 25, 2015·10 cites·17 claims
- 0986US7063509B2Conical tip shroud fillet for a turbine bucketGEN ELECTRIC·Filed 2003·Granted Jun 20, 2006·50 cites·9 claims
- 1084US6893216B2Turbine bucket tip shroud edge profileGEN ELECTRIC·Filed 2003·Granted May 17, 2005·43 cites·16 claims
- 1183US7837445B2Airfoil shape for a turbine nozzleGEN ELECTRIC·Filed 2007·Granted Nov 23, 2010·22 cites·10 claims
- 1282US9127598B2Control method for stoichiometric exhaust gas recirculation power plantSNOOK DANIEL DAVID·Filed 2011·Granted Sep 8, 2015·9 cites·17 claims
- 1376US8231329B2Turbine blade cooling with a hollow airfoil configured to minimize a distance between a pin array section and the trailing edge of the air foilBENJAMIN EDWARD D·Filed 2008·Granted Jul 31, 2012·18 cites·18 claims
- 1473US8096757B2Methods and apparatus for reducing nozzle stressSNOOK DANIEL DAVID·Filed 2009·Granted Jan 17, 2012·6 cites·20 claims
- 1571US8070427B2Gas turbines having flexible chordal hinge sealsSNOOK DANIEL D·Filed 2007·Granted Dec 6, 2011·14 cites·18 claims
- 1664US8070431B2Fully contained retention pin for a turbine nozzleHARTER ARIEL K·Filed 2007·Granted Dec 6, 2011·12 cites·21 claims
- 1764US7419362B2Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 1)GEN ELECTRIC·Filed 2006·Granted Sep 2, 2008·8 cites·12 claims
- 1864US6608937B1Low bit rate video coding method and systemKONINKL PHILIPS ELECTRONICS NV·Filed 2000·Granted Aug 19, 2003·6 cites·2 claims
- 1961US7476083B2Blade/disk dovetail backcut for blade/disk stress reduction (7FA+e, stage 1)GEN ELECTRIC·Filed 2006·Granted Jan 13, 2009·9 cites·12 claims
- 2057US7850425B2Outer sidewall retention scheme for a singlet first stage nozzleGEN ELECTRIC·Filed 2007·Granted Dec 14, 2010·6 cites·20 claims
- 2152US7149250B2Video encoding methodKONINKL PHILIPS ELECTRONICS NV·Filed 2003·Granted Dec 12, 2006·3 cites·2 claims
- 2245US8690530B2System and method for supporting a nozzle assemblySNOOK DANIEL DAVID·Filed 2011·Granted Apr 8, 2014·0 cites·16 claims
- 2345US8057169B2Airfoil core shape for a turbine nozzleBENJAMIN JR EDWARD DURELL·Filed 2008·Granted Nov 15, 2011·3 cites·7 claims
- 2443US2005141611A1Transmission of stuffing information for transmission of layered video streamsFiled 2003·Application pending·0 cites
- 2543US2013160456A1System and method for controlling oxygen emissions from a gas turbineSNOOK DANIEL DAVID·Filed 2011·Application pending·0 cites
- 2640US2012180493A1Apparatus and method for controlling oxygen emissions from a gas turbineSNOOK DANIEL DAVID·Filed 2011·Application pending·0 cites
- 2740US2008101937A1Blade/disk dovetail backcut for blade/disk stress reduction (9FA, stage 1)GEN ELECTRIC·Filed 2006·Application pending·0 cites
- 2839US2012214605A1Gas Turbine Engine Generator System with Torsional Damping CouplingSNOOK DANIEL DAVID·Filed 2011·Application pending·0 cites
- 2938US2008101938A1Blade/disk dovetail backcut for blade/disk stress reduction (7FA, stage 1)GEN ELECTRIC·Filed 2006·Application pending·0 cites
- 3037US2010000219A1Systems and Methods for Supplying Cooling Air to a Gas TurbineGEN ELECTRIC·Filed 2008·Application pending·0 cites
- 3137US2007009349A1Impingement box for gas turbine shroudGEN ELECTRIC·Filed 2005·Application pending·0 cites
- 3236US2011189008A1Retaining ring for a turbine nozzle with improved thermal isolationGEN ELECTRIC·Filed 2010·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →