Patents by Inventor Andrew W. Sklar

Andrew W. Sklar 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).

  • Publication number: 20230347219
    Abstract: A multi-purpose golf tool includes a golf tee platform arranged on a golf tool body, the golf tee platform configured to receive a golf ball balanced thereon, a first prong extending from the golf tool body opposite the golf tee platform, a second prong extending from the golf tool body opposite the golf tee platform, a curved depression extending perpendicular to the length and formed by the golf tool body and a portion of the first prong and second prong, and a first rounded gap between the first prong and the second prong. The first prong has a first ridge extending perpendicular to the length and abutting the curved depression. The second prong has a second ridge extending perpendicular to the length and abutting the curved depression.
    Type: Application
    Filed: May 1, 2023
    Publication date: November 2, 2023
    Inventor: Andrew W. Sklar
  • Patent number: 11345457
    Abstract: A supersonic aircraft fuselage includes a fuselage body having a first end, a second end, a length extending between the first end and second end, a surface, a first flat plane extending from the first end to a center of the fuselage body along the length on the surface, and a second flat plane extending from the second end to the center of the fuselage body along the length on the surface. The surface includes a curved portion conforming to a Sears-Haack body shape and abutting the first flat plane and second flat plane and extending between the first end and second end. A supersonic aircraft includes a first fuselage, a second fuselage, and a space between the first fuselage and second fuselage. The first fuselage and second fuselage form a Busemann biplane geometry within the space.
    Type: Grant
    Filed: February 12, 2020
    Date of Patent: May 31, 2022
    Inventor: Andrew W. Sklar
  • Publication number: 20210031899
    Abstract: A supersonic aircraft fuselage includes a fuselage body having a first end, a second end, a length extending between the first end and second end, a surface, a first flat plane extending from the first end to a center of the fuselage body along the length on the surface, and a second flat plane extending from the second end to the center of the fuselage body along the length on the surface. The surface includes a curved portion conforming to a Sears-Haack body shape and abutting the first flat plane and second flat plane and extending between the first end and second end. A supersonic aircraft includes a first fuselage, a second fuselage, and a space between the first fuselage and second fuselage. The first fuselage and second fuselage form a Busemann biplane geometry within the space.
    Type: Application
    Filed: February 12, 2020
    Publication date: February 4, 2021
    Inventor: Andrew W. Sklar