Inventor
Daniel David Snook
Inventor
Moore, SC, US
Overview
Patents· 23 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F01Dprimary
F01DNon-positive displacement machines or engines, e.g. steam turbines34%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants26%
F02CGas-turbine plants10%
H04NPictorial communication, e.g. television8%
Y02TClimate change mitigation technologies related to transportation8%
Y10TTechnical subjects covered by former us classification6%
Y10STechnical subjects covered by former uspc cross-reference art collections [xracs] and digests4%
F05BIndexing scheme relating to wind, spring, weight, inertia or like motors, to machines or engines for liquids covered by subclasses f03b, f03d and f03g2%
F16BDevices for fastening or securing constructional elements or machine parts together, e.g. nails, bolts, circlips, clamps, clips or wedges2%
PatentTitleYear
9,127,598'Control method for stoichiometric exhaust gas recirculation power plant'20159,115,595'Clearance control system for a gas turbine'20158,690,530'System and method for supporting a nozzle assembly'20148,453,462'Method of operating a stoichiometric exhaust gas recirculation power plant'20138,347,600'Power plant and method of operation'20138,266,913'Power plant and method of use'20128,266,883'Power plant start-up method and method of venting the power plant'20128,231,329'Turbine blade cooling with a hollow airfoil configured to minimize a distance between a pin array section and the trailing edge of the air foil'20128,096,757'Methods and apparatus for reducing nozzle stress'20128,070,427'Gas turbines having flexible chordal hinge seals'20118,070,431'Fully contained retention pin for a turbine nozzle'20118,057,169'Airfoil core shape for a turbine nozzle'20117,850,425'Outer sidewall retention scheme for a singlet first stage nozzle'20107,837,445'Airfoil shape for a turbine nozzle'20107,476,083'Blade/disk dovetail backcut for blade/disk stress reduction (7FA+e, stage 1)'20097,419,362'Blade/disk dovetail backcut for blade/disk stress reduction (9FA+e, stage 1)'20087,149,250'Video encoding method'20067,063,509'Conical tip shroud fillet for a turbine bucket'20066,893,216'Turbine bucket tip shroud edge profile'20056,857,855'Airfoil shape for a turbine bucket'20056,654,420'Video encoding-method'20036,608,937'Low bit rate video coding method and system'20036,442,204'Video encoding method and system'2002Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
2002–2003Based in Palaiseau, FR· patent location history
2003–2006Based in Paris, FR· patent location history
2005–2015Patents assigned to GEN ELECTRIC (19)· patent assignee history
2005–2014Based in Moore, SC, US· patent location history
2011–2015Patents assigned to SNOOK DANIEL DAVID (9)· patent assignee history
2012–2015Patents assigned to WICHMANN LISA ANNE (5)· patent assignee history
2012–2013Patents assigned to DION OUELLET NOEMIE (4)· patent assignee history
2012–2015Patents assigned to DRAPER SAMUEL DAVID (4)· patent assignee history
2012–2015Based in Greenville, SC, US· patent location history
2015Based in Opelika, AL, US· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| GEN ELECTRIC | 19 | 2005–2015 |
| SNOOK DANIEL DAVIDself | 9 | 2011–2015 |
| WICHMANN LISA ANNE | 5 | 2012–2015 |
| DION OUELLET NOEMIE | 4 | 2012–2013 |
| DRAPER SAMUEL DAVID | 4 | 2012–2015 |
Locations
| Location | Patents | Span |
|---|---|---|
| Moore, SC, US | 13 | 2005–2014 |
| Greenville, SC, US | 5 | 2012–2015 |
| Paris, FR | 2 | 2003–2006 |
| Palaiseau, FR | 2 | 2002–2003 |
| Opelika, AL, US | 1 | 2015 |