Patents by Inventor Samson Souksamrane

Samson Souksamrane 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).

  • Systems and methods for curing complex fiber-reinforced composite structures
    Patent number: 9827697
    Abstract: Systems and methods for curing complex fiber-reinforced composite structures utilize two distinct heat sources. A first heat source is utilized for heating a complex fiber-reinforced composite structure from within an internal portion of the complex fiber-reinforced composite structure. A second heat source is utilized for heating the complex fiber-reinforced composite structure from an external surface of the complex fiber-reinforced composite structure.
    Type: Grant
    Filed: August 29, 2014
    Date of Patent: November 28, 2017
    Assignee: The Boeing Company
    Inventors: Allan Tien, Samson Souksamrane, Sahrudine Apdalhaliem
  • SYSTEMS AND METHODS FOR CURING COMPLEX FIBER-REINFORCED COMPOSITE STRUCTURES
    Publication number: 20160059449
    Abstract: Systems and methods for curing complex fiber-reinforced composite structures utilize two distinct heat sources. A first heat source is utilized for heating a complex fiber-reinforced composite structure from within an internal portion of the complex fiber-reinforced composite structure. A second heat source is utilized for heating the complex fiber-reinforced composite structure from an external surface of the complex fiber-reinforced composite structure.
    Type: Application
    Filed: August 29, 2014
    Publication date: March 3, 2016
    Applicant: The Boeing Company
    Inventors: Allan Tien, Samson Souksamrane, Sahrudine Apdalhaliem
  • LAMINATED I-BLADE STRINGER
    Publication number: 20150217850
    Abstract: A blade stringer for a composite panel having an inside surface includes a proximal section, comprising a web attached to and extending approximately perpendicularly from the inside surface of the panel, and a free distal end. The web has a thickness and a height, and includes a plurality of continuous composite plies. The free distal end has a plurality of local plies interleaved and co-cured with the continuous plies, the distal end defining a bulb having a thickness that is greater than the web thickness and less than about a third of the web height.
    Type: Application
    Filed: February 6, 2014
    Publication date: August 6, 2015
    Applicant: The Boeing Company
    Inventors: Allan Tien, David C. Reusch, Marcus C. Hart, Samson Souksamrane