Patents by Inventor Sarabpal-Singh BHATIA

Sarabpal-Singh BHATIA 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: 11958597
    Abstract: An aircraft wing assembly including a wing (3) and a wing tip device (4) at the tip of the wing (3), the wing tip device (4) having front and rear spars (14, 13), wherein the wing tip device (4) has a cross-brace spar (18) that links the front and rear spars and is oriented such that it is oblique to the front and rear spars (14, 13).
    Type: Grant
    Filed: March 23, 2023
    Date of Patent: April 16, 2024
    Assignee: AIRBUS OPERATIONS LIMITED
    Inventors: Sarabpal-Singh Bhatia, Samuel Phillips
  • Publication number: 20230249800
    Abstract: An aircraft wing assembly including a wing (3) and a wing tip device (4) at the tip of the wing (3), the wing tip device (4) having front and rear spars (14, 13), wherein the wing tip device (4) has a cross-brace spar (18) that links the front and rear spars and is oriented such that it is oblique to the front and rear spars (14, 13).
    Type: Application
    Filed: March 23, 2023
    Publication date: August 10, 2023
    Inventors: Sarabpal-Singh BHATIA, Samuel PHILLIPS
  • Patent number: 11643183
    Abstract: An aircraft (1) having a wing (3) and a wing tip device (4) at the tip of the wing (3), the wing tip device (4) having front and rear spars (14, 13), wherein the wing tip device (4) has a cross-brace spar (18) that links the front and rear spars and is oriented such that it is oblique to the front and rear spars (14, 13).
    Type: Grant
    Filed: June 13, 2018
    Date of Patent: May 9, 2023
    Assignee: Airbus Operations Limited
    Inventors: Sarabpal-Singh Bhatia, Samuel Phillips
  • Publication number: 20180362143
    Abstract: An aircraft (1) having a wing (3) and a wing tip device (4) at the tip of the wing (3), the wing tip device (4) having front and rear spars (14, 13), wherein the wing tip device (4) has a cross-brace spar (18) that links the front and rear spars and is oriented such that it is oblique to the front and rear spars (14, 13).
    Type: Application
    Filed: June 13, 2018
    Publication date: December 20, 2018
    Inventors: Sarabpal-Singh BHATIA, Samuel PHILLIPS