Boom Technology has a total of 20 patents globally, out of which 1 have been granted. Of these 20 patents, more than 85% patents are active. The United States of America is where Boom Technology has filed the maximum number of patents, followed by Israel and India. Parallelly, United States of America seems to be the main focused R&D centre and also is the origin country of Boom Technology.
Boom Technology (Boom Supersonic) was founded in 2014. Boom Technology, doing business as Boom Supersonic, is engaged in the production of commercial aircraft. The is making supersonic passenger travel into reality by making a supersonic airliner
Do read about some of the most popular patents of Boom Technology which have been covered by us in this article and also you can find Boom Technology patents information, the worldwide patent filing activity and its patent filing trend over the years, and many other stats over Boom Technology patent portfolio.
How many patents does Boom Technology have?
Boom Technology has a total of 20 patents globally. These patents belong to 9 unique patent families. Out of 20 patents, 17 patents are active.How Many Patents Did Boom Technology 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 | Boom Technology Applications Filed | Boom Technology Patents Granted |
2022 | 12 | – |
2021 | 5 | – |
2020 | 1 | 1 |
2017 | 2 | – |
How many Boom Technology patents are Alive/Dead?
Worldwide PatentsHow Many Patents did Boom Technology File in Different Countries?
Boom Technology filled all their patents in United States of America.Where are Research Centers of Boom Technology Patents Located?
The Research Centers of Boom Technology Patents is the United States of America.What Percentage of Boom Technology US Patent Applications Were Granted?
Boom Technology (Excluding its subsidiaries) has filed 7 patent applications at USPTO so far (Excluding Design and PCT applications). Out of these 1 have been granted leading to a grant rate of 100%. Below are the key stats of Boom Technology patent prosecution at the USPTO.Which Law Firms Filed Most US Patents for Boom Technology?
Law Firm | Total Applications | Success Rate |
Perkins Coie Llp | 7 | 100% |
List of Boom Technology patents
Boom Technology Patents | Title |
US10793266B2 | Commercial Supersonic Aircraft And Associated Systems And Methods |
US20230056909A1 | Variable Noise Reduction Systems For Supersonic Aircraft, And Associated Methods |
US20230104383A1 | Automated Test Cards For Performing In-Flight Testing On Aircraft, And Associated Systems And Methods |
US20230112668A1 | Dissimilarly Shaped Aircraft Nozzles With Tandem Mixing Devices, And Associated Systems And Methods |
US20220325678A1 | Lobed Mixer Nozzles For Supersonic And Subsonic Aircraft, And Associated Systems And Methods |
US20220165164A1 | Real Time Sonic Boom Warning System |
US20210300542A1 | Commercial Supersonic Aircraft And Associated Systems And Methods |
US20210300543A1 | Commercial Supersonic Aircraft And Associated Systems And Methods |
US20210139142A1 | Commercial Supersonic Aircraft And Associated Systems And Methods |
WO2023023279A1 | Variable Noise Reduction Systems For Supersonic Aircraft, And Associated Methods |
WO2023114402A1 | Telemetry Visualization System For Fast Display Of Aircraft Data And Associated Systems And Methods |
WO2023081293A1 | Smart Routing For Aircraft Flight Planning And Associated Systems And Methods |
WO2023059650A1 | Automated Test Cards For Performing In-Flight Testing On Aircraft, And Associated Systems And Methods |
WO2023064215A1 | Dissimilarly Shaped Aircraft Nozzles With Tandem Mixing Devices, And Associated Systems And Methods |
WO2022216932A1 | Lobed Mixer Nozzles For Supersonic And Subsonic Aircraft, And Associated Systems And Methods |
WO2022216468A1 | Lobed Mixer Nozzles For Supersonic And Subsonic Aircraft, And Associated Systems And Methods |
WO2023055887A3 | Retractable Chevrons For Aircraft Nozzles, And Associated Systems And Methods |
US20210300544A1 | Commercial Supersonic Aircraft And Associated Systems And Methods |
WO2022115261A1 | Real Time Sonic Boom Warning System |
WO2018089934A1 | Commercial Supersonic Aircraft And Associated Systems And Methods |