Patents by Inventor Abraham Oonnoonny

Abraham Oonnoonny 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).

  • Aircraft fuselage and structural cable for aircraft fuselage
    Patent number: 11148780
    Abstract: A wide body aircraft is discussed having a fuselage with a first structural element, a second structural element, a wide-body fuselage section, and a plurality of tension members. Each of the first structural element and the second structural element may be arranged to traverse a longitudinal length of the wide-body fuselage section. The wide-body fuselage section may comprise a set of side-by-side fuselage subassemblies, where the set of side-by-side fuselage subassemblies can be coupled to one another via the first structural element and the second structural element. The plurality of tension members can be arranged to manage tension between the first structural element and the second structural element. The plurality of tension members can be configured to remain flexible under a compression load, while managing tension therebetween.
    Type: Grant
    Filed: December 21, 2017
    Date of Patent: October 19, 2021
    Assignee: Aurora Flight Sciences Corporation
    Inventor: Abraham Oonnoonny
  • Aircraft Fuselage and Structural Cable for Aircraft Fuselage
    Publication number: 20190193831
    Abstract: A wide body aircraft is discussed having a fuselage with a first structural element, a second structural element, a wide-body fuselage section, and a plurality of tension members. Each of the first structural element and the second structural element may be arranged to traverse a longitudinal length of the wide-body fuselage section. The wide-body fuselage section may comprise a set of side-by-side fuselage subassemblies, where the set of side-by-side fuselage subassemblies can be coupled to one another via the first structural element and the second structural element. The plurality of tension members can be arranged to manage tension between the first structural element and the second structural element. The plurality of tension members can be configured to remain flexible under a compression load, while managing tension therebetween.
    Type: Application
    Filed: December 21, 2017
    Publication date: June 27, 2019
    Inventor: Abraham Oonnoonny