Inventor · disambiguated record
Brandon Taylor Overby
Also filed as: OVERBY BRANDON TAYLOR
5 granted patents·6 pending applications·7 citations·filing 2010–2016
68Inventor score
Top patents by PatentIndex Score
11 records- 0172US9353952B2Crossfire tube assembly with tube bias between adjacent combustorsGEN ELECTRIC·Filed 2012·Granted May 31, 2016·4 cites·15 claims
- 0255US8590315B2Extruded fluid manifold for gas turbomachine combustor casingOVERBY BRANDON TAYLOR·Filed 2010·Granted Nov 26, 2013·2 cites·17 claims
- 0353US9441835B2System and method for fuel and steam injection within a combustorGEN ELECTRIC·Filed 2012·Granted Sep 13, 2016·1 cites·25 claims
- 0448US9500367B2Combustion casing manifold for high pressure air delivery to a fuel nozzle pilot systemGEN ELECTRIC·Filed 2013·Granted Nov 22, 2016·0 cites·11 claims
- 0545US10837644B2Tool kit and method for decoupling cross-fire tube assemblies in gas turbine enginesGEN ELECTRIC·Filed 2016·Granted Nov 17, 2020·0 cites·20 claims
- 0643US2014202160A1Gas turbine system with manifoldGEN ELECTRIC·Filed 2013·Application pending·0 cites
- 0738US2014338343A1System for vibration damping of a fuel nozzle within a combustorGEN ELECTRIC·Filed 2013·Application pending·0 cites
- 0838US2014250981A1Seal test fixture for a gas turbine fuel nozzleGEN ELECTRIC·Filed 2013·Application pending·0 cites
- 0934US2013067923A1Combustor and method for conditioning flow through a combustorOVERBY BRANDON TAYLOR·Filed 2011·Application pending·0 cites
- 1032US2013081397A1Forward casing with a circumferential sloped surface and a combustor assembly including sameOVERBY BRANDON TAYLOR·Filed 2011·Application pending·0 cites
- 1130US2013327011A1Method And Apparatus For A Fuel Nozzle Assembly For Use With A CombustorOVERBY BRANDON TAYLOR·Filed 2012·Application pending·0 cites
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