Patents by Inventor Charuhas M. Soman

Charuhas M. Soman 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).

  • Patent number: 10215281
    Abstract: Disclosed herein is a seal assembly for sealing a gap between a first component and a second component is disclosed. The second component is movable relative to the first component. The seal assembly includes a rub strip and a seal strip. The rub strip includes a seal strip engagement surface having a convex shape. Additionally, the rub strip includes a first component engagement surface that is opposite the seal strip engagement surface and has a concave shape. The seal strip includes a rub strip engagement surface having a convex shape. Furthermore, the seal strip includes a second component engagement surface that is opposite the rub strip engagement surface and has a concave shape. The seal strip engagement surface is harder than the rub strip engagement surface.
    Type: Grant
    Filed: May 4, 2016
    Date of Patent: February 26, 2019
    Assignee: The Boeing Company
    Inventors: Charuhas M. Soman, Keith Townsend, Eric D. Blohm, Richard B. Tanner, Mark J. Herzberg, Ralph E. Hardin
  • Patent number: 9957831
    Abstract: Systems, methods, and devices are configured to implement hydraulic actuators. Devices may include a housing having an internal surface defining an internal cavity that may have a substantially circular cross sectional curvature. The devices may include a rotor that includes a first slot having a substantially circular curvature. The devices may include a first vane disk partially disposed within the first slot of the rotor, where the first vane disk has a substantially circular external geometry. The first vane disk may be mechanically coupled to the rotor via the first slot, and the first vane disk may be configured to form a first seal with the internal surface of the housing. The devices may include a first separator device that may be configured to form a second seal with the internal surface of the housing and a third seal with an external surface of the rotor.
    Type: Grant
    Filed: July 31, 2014
    Date of Patent: May 1, 2018
    Assignee: The Boeing Company
    Inventors: Charuhas M. Soman, Steven P. Walker, Michael K. Klein, John A. Standley
  • Publication number: 20170321804
    Abstract: Disclosed herein is a seal assembly for sealing a gap between a first component and a second component is disclosed. The second component is movable relative to the first component. The seal assembly includes a rub strip and a seal strip. The rub strip includes a seal strip engagement surface having a convex shape. Additionally, the rub strip includes a first component engagement surface that is opposite the seal strip engagement surface and has a concave shape. The seal strip includes a rub strip engagement surface having a convex shape. Furthermore, the seal strip includes a second component engagement surface that is opposite the rub strip engagement surface and has a concave shape. The seal strip engagement surface is harder than the rub strip engagement surface.
    Type: Application
    Filed: May 4, 2016
    Publication date: November 9, 2017
    Inventors: Charuhas M. Soman, Keith Townsend, Eric D. Blohm, Richard B. Tanner, Mark J. Herzberg, Ralph E. Hardin
  • Publication number: 20160032758
    Abstract: Systems, methods, and devices are disclosed for implementing hydraulic actuators. Devices may include a housing having an internal surface defining an internal cavity that may have a substantially circular cross sectional curvature. The devices may include a rotor that includes a first slot having a substantially circular curvature. The devices may include a first vane disk partially disposed within the first slot of the rotor, where the first vane disk has a substantially circular external geometry. The first vane disk may be mechanically coupled to the rotor via the first slot, and the first vane disk may be configured to form a first seal with the internal surface of the housing. The devices may include a first separator device that may be configured to form a second seal with the internal surface of the housing and a third seal with an external surface of the rotor.
    Type: Application
    Filed: July 31, 2014
    Publication date: February 4, 2016
    Applicant: The Boeing Company
    Inventors: Charuhas M. Soman, Steven P. Walker, Michael K. Klein, John A. Standley