Patents by Inventor Akshay SRINIVASAMURTHY

Akshay SRINIVASAMURTHY 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).

  • Stiffened structural component for an aircraft
    Patent number: 11541982
    Abstract: A stiffened structural component for an aircraft includes a first material sheet with a first surface, and at least one elongate bulge that bulges out in a direction transverse to the first surface in order to stiffen the structural component, wherein each of the at least one bulge comprises two edges that extend along the first surface, wherein a continuous bulging surface extends between the edges, and wherein the bulges are formed integrally into the first material sheet through pressing.
    Type: Grant
    Filed: March 11, 2020
    Date of Patent: January 3, 2023
    Inventors: Chinnarajan Periyasamy, Akshay Srinivasamurthy, Wolfgang Entelmann, Wolfgang Schulze, Jens Rohde
  • Control surface actuation mechanism
    Patent number: 11214354
    Abstract: A control surface actuation mechanism for moving a control surface relative to a fixed aerofoil portion of an aircraft is disclosed including an articulating support, a sliding member on the articulating support and coupled to the control surface, the sliding member arranged to slide relative to the articulating support, a track with a path for attachment on the fixed aerofoil portion, and a rigid connecting element connected to the first track and to the sliding member. The first end of the first rigid connecting element is configured to move passively along the path, as the sliding member is driven to slide relative to the articulating support by an actuator.
    Type: Grant
    Filed: April 19, 2019
    Date of Patent: January 4, 2022
    Assignee: AIRBUS SAS
    Inventors: Jason Kuruvilla, Pradeep Gajakosh, Akshay Srinivasamurthy, Rakshith Raghavan Belur, Sumit Kumar Malik, Gayathri Swaminathan, Vinayak Ramachandra Patil, Avinash Kumar Yadav
  • Stiffened Structural Component For An Aircraft
    Publication number: 20200307756
    Abstract: A stiffened structural component for an aircraft includes a first material sheet with a first surface, and at least one elongate bulge that bulges out in a direction transverse to the first surface in order to stiffen the structural component, wherein each of the at least one bulge comprises two edges that extend along the first surface, wherein a continuous bulging surface extends between the edges, and wherein the bulges are formed integrally into the first material sheet through pressing.
    Type: Application
    Filed: March 11, 2020
    Publication date: October 1, 2020
    Applicants: Airbus Operations GmbH, Airbus Operations SAS
    Inventors: Chinnarajan Periyasamy, Akshay Srinivasamurthy, Wolfgang Entelmann, Wolfgang Schulze, Jens Rohde
  • A CONTROL SURFACE ACTUATION MECHANISM
    Publication number: 20190329865
    Abstract: A control surface actuation mechanism for moving a control surface relative to a fixed aerofoil portion of an aircraft is disclosed including an articulating support, a sliding member on the articulating support and coupled to the control surface, the sliding member arranged to slide relative to the articulating support, a track with a path for attachment on the fixed aerofoil portion, and a rigid connecting element connected to the first track and to the sliding member. The first end of the first rigid connecting element is configured to move passively along the path, as the sliding member is driven to slide relative to the articulating support by an actuator.
    Type: Application
    Filed: April 19, 2019
    Publication date: October 31, 2019
    Inventors: Jason KURUVILLA, Pradeep GAJAKOSH, Akshay SRINIVASAMURTHY, Rakshith Raghavan BELUR, Sumit Kumar MALIK, Gayathri SWAMINATHAN, Vinayak Ramachandra PATIL, Avinash Kumar YADAV