Assignee
AERION CORP
US·14 granted patents·100 citations·filing 2003–2018
Top patents by PatentIndex Score
14 records- 0196US10724472B1High flow plug nozzle apparatus and method of using the sameAERION CORP·Filed 2017·Granted Jul 28, 2020·18 cites·12 claims
- 0285US7837142B2Supersonic aircraft jet engineAERION CORP·Filed 2007·Granted Nov 23, 2010·20 cites·16 claims
- 0384US7967241B2Supersonic aircraft jet engine installationAERION CORP·Filed 2010·Granted Jun 28, 2011·12 cites·3 claims
- 0480US10296672B2Generating inviscid and viscous fluid-flow simulations over an aircraft surface using a fluid-flow meshAERION CORP·Filed 2014·Granted May 21, 2019·5 cites·20 claims
- 0577US8935140B2Generating inviscid and viscous fluid-flow simulations over a surface using a fluid-flow meshAERION CORP·Filed 2013·Granted Jan 13, 2015·4 cites·20 claims
- 0667US9348956B2Generating a simulated fluid flow over a surface using anisotropic diffusionAERION CORP·Filed 2013·Granted May 24, 2016·2 cites·20 claims
- 0762US7004428B2Lift and twist control using trailing edge control surfaces on supersonic laminar flow wingsAERION CORP·Filed 2004·Granted Feb 28, 2006·18 cites·3 claims
- 0853US7946535B2Highly efficient supersonic laminar flow wingAERION CORP·Filed 2007·Granted May 24, 2011·4 cites·15 claims
- 0951US11386245B2Computing techniques for three-dimensional modeling and design analysisAERION CORP·Filed 2018·Granted Jul 12, 2022·0 cites·29 claims
- 1051US9494482B2Predicting transition from laminar to turbulent flow over a surface using mode-shape parametersAERION CORP·Filed 2013·Granted Nov 15, 2016·0 cites·36 claims
- 1151US8371124B2Jet nozzle plug with varying, non-circular cross sectionsAERION CORP·Filed 2009·Granted Feb 12, 2013·3 cites·8 claims
- 1250US7000870B2Laminar flow wing for transonic cruiseAERION CORP·Filed 2003·Granted Feb 21, 2006·8 cites·15 claims
- 1346US6857599B2Highly swept canard with low sweep wing supersonic aircraft configurationAERION CORP·Filed 2003·Granted Feb 22, 2005·6 cites·14 claims
- 1444US9418202B2Predicting transition from laminar to turbulent flow over a surfaceAERION CORP·Filed 2013·Granted Aug 16, 2016·0 cites·25 claims
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Counts cover granted patents and pending applications in the PatentIndex corpus. How scoring works →