Patents by Inventor Vinayak RAMACHANDRA PATIL

Vinayak RAMACHANDRA PATIL 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).

  • Fuselage assembly for an aircraft
    Patent number: 11518490
    Abstract: A fuselage assembly for an aircraft including a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system.
    Type: Grant
    Filed: December 11, 2020
    Date of Patent: December 6, 2022
    Assignees: Airbus Operations GmbH, Airbus SAS
    Inventors: Matthias S. Schroeder, Jesus Miguel Batanero Benito, Srivats Srinivasan, Avinash Kumar Yadav, Vinayak Ramachandra Patil, Abhishek Vyas
  • Stiffener for an aircraft assembly
    Patent number: 11312467
    Abstract: A stiffener for an aircraft assembly is disclosed. The stiffener provides structural stability to the aircraft assembly. The stiffener has a first stiffener part having a planar web portion and a second stiffener part arranged with the first stiffener part. The second stiffener part includes a corrugated web portion having a corrugation. The present application also relates to an aircraft assembly, a fuselage for an aircraft, an aircraft and a method of forming a stiffener for an aircraft assembly.
    Type: Grant
    Filed: December 20, 2018
    Date of Patent: April 26, 2022
    Assignees: AIRBUS OPERATIONS GmbH, AIRBUS SAS
    Inventors: Avinash Kumar Yadav, Vinayak Ramachandra Patil, Sven Hardy Werner
  • 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
  • FUSELAGE ASSEMBLY FOR AN AIRCRAFT
    Publication number: 20210094669
    Abstract: A fuselage assembly for an aircraft including a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system.
    Type: Application
    Filed: December 11, 2020
    Publication date: April 1, 2021
    Inventors: Matthias Schroeder, Jesus Miguel Batanero Benito, Srivats Srinivasan, Avinash Kumar Yadav, Vinayak Ramachandra Patil, Abhishek Vyas
  • Fuselage assembly for an aircraft
    Patent number: 10875619
    Abstract: A fuselage assembly for an aircraft including a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system.
    Type: Grant
    Filed: March 26, 2019
    Date of Patent: December 29, 2020
    Assignees: Airbus Operations GmbH, Airbus (S.A.S.)
    Inventors: Matthias S. Schroeder, Jesus Miguel Batanero Benito, Srivats Srinivasan, Avinash Kumar Yadav, Vinayak Ramachandra Patil, Abhishek Vyas
  • 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
  • FUSELAGE ASSEMBLY FOR AN AIRCRAFT
    Publication number: 20190300139
    Abstract: A fuselage assembly for an aircraft including a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system.
    Type: Application
    Filed: March 26, 2019
    Publication date: October 3, 2019
    Inventors: Matthias S. SCHROEDER, Jesus Miguel BATANERO BENITO, Srivats SRINIVASAN, Avinash Kumar YADAV, Vinayak RAMACHANDRA PATIL, Abhishek VYAS
  • STIFFENER FOR AN AIRCRAFT ASSEMBLY
    Publication number: 20190193830
    Abstract: A stiffener for an aircraft assembly is disclosed. The stiffener provides structural stability to the aircraft assembly. The stiffener has a first stiffener part having a planar web portion and a second stiffener part arranged with the first stiffener part. The second stiffener part includes a corrugated web portion having a corrugation. The present application also relates to an aircraft assembly, a fuselage for an aircraft, an aircraft and a method of forming a stiffener for an aircraft assembly.
    Type: Application
    Filed: December 20, 2018
    Publication date: June 27, 2019
    Inventors: Avniash Kumar YADAV, Vinayak RAMACHANDRA PATIL, Sven Hardy WERNER