Aerion has a total of 36 patents globally, out of which 13 have been granted. Of these 36 patents, more than 5% patents are active. Europe is where Aerion has filed the maximum number of patents, followed by Germany and Canada. Parallelly, United States of America seems to be the main focused R&D centre and also is the origin country of Aerion.
Aerion was founded in the year 2002. The Company designs, develops and sells supersonic aircraft. The Company specializes in new generation and manufacturing of supersonic aircrafts.
Do read about some of the most popular patents of Aerion which have been covered by us in this article and also you can find Aerion patents information, the worldwide patent filing activity and its patent filing trend over the years, and many other stats over Aerion patent portfolio.
How many patents does the founder and the CEO of Aerion have?
The founder Richard Tracy has 0 patent and Robert M. Bass has 0 patent.
How many patents does Aerion have?
Aerion has a total of 36 patents globally. These patents belong to 36 unique patent families. Out of 36 patents, 2 patents are active.
How Many Patents did Aerion File Every Year?
Are you wondering why there is a drop in patent filing for the last two years? It is because a patent application can take up to 18 months to get published. Certainly, it doesn’t suggest a decrease in the patent filing.
| Year of Patents Filing or Grant | Aerion Applications Filed | Aerion Patents Granted |
| 2019 | – | 1 |
| 2018 | 1 | – |
| 2017 | – | 1 |
| 2016 | 1 | 4 |
| 2014 | 1 | – |
| 2012 | 5 | 1 |
| 2011 | 3 | – |
| 2010 | 3 | 3 |
| 2009 | – | 1 |
| 2007 | 13 | – |
How many Aerion patents are Alive/Dead?
How Many Patents did Aerion File in Different Countries?
Countries in which Aerion Filed Patents
| Country | Patents |
| Europe | 4 |
| Germany | 3 |
| Canada | 3 |
| Austria | 3 |
| Hong Kong (S.A.R.) | 2 |
| Russia | 2 |
| Spain | 2 |
| Australia | 1 |
| United States Of America | 1 |
| Japan | 1 |
| China | 1 |
Where are Research Centres of Aerion Patents Located?
List of Aerion Patents
| Aerion Patents | Title |
| US10296672B2 | Generating Inviscid And Viscous Fluid-Flow Simulations Over An Aircraft Surface Using A Fluid-Flow Mesh |
| AT853311T | Ultrasonic Aircraft Engine |
| EP1169224B1 | Aircraft Wing And Fuselage Contours |
| EP1583690B1 | Laminar Flow Wing For Transonic Cruise |
| EP2081821B1 | Supersonic Aircraft |
| EP2084061B1 | Supersonic Aircraft Jet Engine |
| CN101547829A | Highly Efficient Supersonic Laminar Flow Wing |
| WO2008105847A3 | Supersonic Aircraft Jet Engine |
| WO2008115207A3 | Highly Efficient Supersonic Laminar Flow Wing |
| WO2010114604A1 | Jet Nozzle Plug With Varying Non-Circular Cross Sections |
| WO2011087475A9 | Laminar Flow Wing Optimized For Supersonic And High Subsonic Cruise Aircraft |
| WO2012021360A4 | Aircraft Emergency And Backup Secondary Power Apparatus |
| WO2012092502A1 | Generating Inviscid And Viscous Fluid-Flow Simulations Over An Aircraft Surface |
| WO2012112408A1 | Laminar Flow Wing Optimized For Transonic Cruise Aircraft |
| WO2012125497A1 | Generating A Simulated Fluid Flow Over An Aircraft Surface Using Anisotropic Diffusion |
| WO2012129440A3 | Predicting Transition From Laminar To Turbulent Flow Over A Surface |
| WO2012129526A3 | Generating Inviscid And Viscous Fluid Flow Simulations Over A Surface Using A Quasi-Simultaneous Technique |
| WO2012141770A3 | Laminar Flow Wing Optimized For Transonic And Supersonic Cruise Aircraft |
| WO2016205088A1 | Cockpit Seat Armrest Avionics Cursor Control Device |
| WO2019006268A1 | Computing Techniques For Three-Dimensional Modeling And Design Analysis |
| DE60025476T2 | Airplane Wing And Fuselage Contours |
| DE602007049183T2 | Ultrasonic Aircraft Engine |
| DE60331004D1 | Laminar Flow Wing For Semisonic Cruise |
| AT455034T | Laminar Flow Wing For Transonic Cruise |
| AT772553T | Supersonic Aircraft |
| ES2564078T3 | Highly Efficient Supersonic Laminar Flow Wing |
| ES2617754T3 | Supersonic Aircraft Jet Engine |
| CA2634307C | Aircraft Wing And Fuselage Contours |
| CA2503270A1 | Laminar Flow Wing For Transonic Cruise |
| CA2665852A1 | Highly Efficient Supersonic Laminar Flow Wing |
| RU2454354C2 | Supersonic Aircraft Jet Engine |
| HK1045288A1 | Aircraft Wing And Fuselage Contours |
| HK1137705A | Highly Efficient Supersonic Laminar Flow Wing |
| RU2011150806A | Jet Engine Of Supersonic Aircraft |
| AU2003287542B2 | Laminar Flow Wing For Transonic Cruise |
| JP2010506797A | High Performance Supersonic Laminar Airfoil |
What are Aerion‘ key innovation segments?
What Technologies are Covered by Aerion?
The chart below distributes patents filed by Aerion