Patents by Inventor Marco GABALDO

Marco GABALDO has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Engine for hypersonic aircrafts with supersonic combustor
    Patent number: 10927793
    Abstract: Described is a propulsion system (1) for hypersonic aircraft, having an air inlet (10) of a fluid (110), a containment duct (20) and an exhaust nozzle (30). The propulsion system (1) comprises a bypass duct (40) for a flow (100) of fluid (110), an air-breathing engine (22) and a rocket (23) configured for processing respective flows (22a, 23a) of fluid (110). The bypass duct (40), the air-breathing engine (22) and the rocket (23) are operatively associated with each other in such a way as to generate a thermodynamic-fluid interaction in a same portion of space (33) between the respective flows (40a, 22a, 23a) processed in an operating configuration of the propulsion system (1) and wherein the portion of space (33) is inside the containment duct (20).
    Type: Grant
    Filed: April 3, 2015
    Date of Patent: February 23, 2021
    Inventors: Marco Gabaldo, Jose Eduardo Mautone Barros
  • ENGINE FOR HYPERSONIC AIRCRAFTS WITH SUPERSONIC COMBUSTOR
    Publication number: 20180119644
    Abstract: Described is a propulsion system (1) for hypersonic aircraft, having an air inlet (10) of a fluid (110), a containment duct (20) and an exhaust nozzle (30). The propulsion system (1) comprises a bypass duct (40) for a flow (100) of fluid (110), an air-breathing engine (22) and a rocket (23) configured for processing respective flows (22a, 23a) of fluid (110). The bypass duct (40), the air-breathing engine (22) and the rocket (23) are operatively associated with each other in such a way as to generate a thermodynamic-fluid interaction in a same portion of space (33) between the respective flows (40a, 22a, 23a) processed in an operating configuration of the propulsion system (1) and wherein the portion of space (33) is inside the containment duct (20).
    Type: Application
    Filed: April 3, 2015
    Publication date: May 3, 2018
    Inventors: Jose Eduardo MAUTONE BARROS, Marco GABALDO