Inventor · disambiguated record
John K. Shigley
Also filed as: RAWDING LEGAL REPRESENTATIVE SHELLEY · SHIGLEY JOHN K
12 granted patents·1 pending application·148 citations·filing 1986–2021
91Inventor score
Top patents by PatentIndex Score
13 records- 0180US5059301AProcess for the preparation of recarburizer cokeCONOCO·Filed 1991·Granted Oct 22, 1991·41 cites·15 claims
- 0270US4720338APremium coking processCONOCO INC·Filed 1986·Granted Jan 19, 1988·18 cites·6 claims
- 0366US6904755B2Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including sameALLIANT TECHSYSTEMS INC·Filed 2004·Granted Jun 14, 2005·7 cites·21 claims
- 0464US6711901B1Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including sameALLIANT TECHSYSTEMS INC·Filed 2001·Granted Mar 30, 2004·19 cites·23 claims
- 0562US5028311ADelayed coking processCONOCO INC·Filed 1990·Granted Jul 2, 1991·25 cites·24 claims
- 0659US11846256B2Liquid rocket engine assemblies and related methodsNORTHROP GRUMMAN SYSTEMS CORP·Filed 2021·Granted Dec 19, 2023·0 cites·17 claims
- 0756US5645219AAddition-polymerization resin systems for fiber-reinforced nozzle ablative componentsTHIOKOL CORP·Filed 1993·Granted Jul 8, 1997·17 cites·30 claims
- 0846US11028802B2Liquid rocket engine assemblies and related methodsNORTHROP GRUMMAN SYSTEMS CORP·Filed 2016·Granted Jun 8, 2021·0 cites·26 claims
- 0944US2004105970A1Low density composite rocket nozzle components and process for making the same from standard density phenolic matrix, fiber reinforced materialsFiled 2003·Application pending·0 cites
- 1043US6235359B1Rocket assembly ablative materials formed from, as a precursor, staple cellulosic fibers, and method of insulating or thermally protecting a rocket assembly with the sameCORDANT TECH INC·Filed 1999·Granted May 22, 2001·9 cites·20 claims
- 1139US6679965B1Low density composite rocket nozzle components and process for making the same from standard density phenolic matrix, fiber reinforced materialsALLIANT TECHSYSTEMS INC·Filed 1998·Granted Jan 20, 2004·8 cites·31 claims
- 1232USRE43867ERocket assembly ablative materials formed from, as a precursor, staple cellulosic fibers, and method of insulating or thermally protecting a rocket assembly with the sameWILSON KENNETH P·Filed 2003·Granted Dec 18, 2012·0 cites·22 claims
- 1331US6479148B1Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the sameCORDANT TECH INC·Filed 1999·Granted Nov 12, 2002·4 cites·19 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →