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AERION CORP

Overview
  • Total Patents
    41
  • GoodIP Patent Rank
    195,904
  • Filing trend
    ⇧ 100.0%
About

AERION CORP has a total of 41 patent applications. It increased the IP activity by 100.0%. Its first patent ever was published in 2000. It filed its patents most often in United States, WIPO (World Intellectual Property Organization) and Canada. Its main competitors in its focus markets transport, environmental technology and computer technology are AIRBUS IND, BIRKENSTOCK DAVID and EHJRBAS OPEREJSHNZ S L.

Patent filings per year

Chart showing AERION CORPs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Chase James D 25
#2 Sturdza Peter 15
#3 Tracy Richard R 14
#4 Garzon German Andres 7
#5 Henderson Michael 4
#6 Rajnarayan Dev 3
#7 Rodriguez David L 3
#8 Kroo Ilan 3
#9 Peter Sturdza 3
#10 Pavanaskar Sushrut S 2

Latest patents

Publication Filing date Title
US2019005185A1 Computing Techniques for Three-Dimensional Modeling and Design Analysis
US10724472B1 High flow plug nozzle apparatus and method of using the same
WO2016205088A1 Cockpit seat armrest avionics cursor control device
US2013246024A1 Generating a simulated fluid flow over a surface using anisotropic diffusion
US2013246027A1 Generating inviscid and viscous fluid-flow simulations over a surface using a fluid-flow mesh
US2013282629A1 Predicting transition from laminar to turbulent flow over a surface using mode-shape parameters
WO2012129526A2 Generating inviscid and viscous fluid flow simulations over a surface using a quasi-simultaneous technique
WO2012129440A2 Predicting transition from laminar to turbulent flow over a surface
WO2012112408A1 Laminar flow wing optimized for transonic cruise aircraft
WO2012141770A2 Laminar flow wing optimized for transonic and supersonic cruise aircraft
WO2012021360A1 Aircraft emergency and backup secondary power apparatus
CA2776951A1 Laminar flow wing optimized for supersonic and high subsonic cruise aircraft
US2010139284A1 Jet nozzle plug with varying, non-circular cross sections
US2009206206A1 Highly efficient supersonic laminar flow wing
US2009014597A1 Supersonic aircraft jet engine
US7004428B2 Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings
US6857599B2 Highly swept canard with low sweep wing supersonic aircraft configuration
US7000870B2 Laminar flow wing for transonic cruise
EP1169224A2 Aircraft wing and fuselage contours