Inventor · disambiguated record
Andrew D. Burdick
Also filed as: BURDICK ANDREW · BURDICK ANDREW D
15 granted patents·1 pending application·172 citations·filing 1998–2019
91Inventor score
Top patents by PatentIndex Score
16 records- 0196US6155928AModular portable gaming simulator systems and methodsCOCA COLA CO·Filed 1998·Granted Dec 5, 2000·116 cites·26 claims
- 0293US10247419B2Combustor liner panel with a multiple of heat transfer ribs for a gas turbine engine combustorUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 2, 2019·7 cites·13 claims
- 0391US9803559B2Variable vane and seal arrangementUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 31, 2017·6 cites·18 claims
- 0484US9217371B2Mid-turbine frame with tensioned spokesFARAH JORGE I·Filed 2012·Granted Dec 22, 2015·9 cites·18 claims
- 0575US10012090B2Airfoil cooling apparatusUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 3, 2018·2 cites·19 claims
- 0673US10865652B2Method and device for piston seal anti-rotationUNITED TECHNOLOGIES CORP·Filed 2019·Granted Dec 15, 2020·1 cites·9 claims
- 0768US10215043B2Method and device for piston seal anti-rotationUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 26, 2019·1 cites·9 claims
- 0861US7739872B2Cooled dual wall liner closeoutUNITED TECHNOLOGIES CORP·Filed 2005·Granted Jun 22, 2010·10 cites·14 claims
- 0954US7770399B2Gas turbine engine nozzle liner with thermally compliant attachment bracketsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Aug 10, 2010·4 cites·16 claims
- 1050US7685825B2Axially split nozzle liner for convergent nozzleUNITED TECHNOLOGIES CORP·Filed 2006·Granted Mar 30, 2010·3 cites·20 claims
- 1149US10494929B2Cooled airfoil structureUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 3, 2019·0 cites·17 claims
- 1248US9995171B2Cooling passages for a mid-turbine frameUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jun 12, 2018·0 cites·10 claims
- 1345US10598036B2Assembly for sealing a gap between components of a turbine engineUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 24, 2020·0 cites·20 claims
- 1445US10458339B2Gas turbine engine case flow blocking coversUNITED TECHNOLOGIES CORP·Filed 2016·Granted Oct 29, 2019·0 cites·24 claims
- 1542US2019040796A1Gas turbine engine cooling arrangementUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
- 1637US5961425AJump rope deviceRENSSELAER POLYTECH INST·Filed 1998·Granted Oct 5, 1999·13 cites·14 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →