Patents by Inventor Anand PUNTAMBEKAR

Anand PUNTAMBEKAR 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).

  • Apparatus and method for determining aircraft tire pressure
    Patent number: 11667162
    Abstract: An apparatus configured to determine the pressure of an aircraft tire at a reference temperature. The apparatus includes a processing system configured to: obtain a measured tire pressure and a measured temperature associated with the measured tire pressure; and determine a tire pressure at the reference temperature by adjusting the measured tire pressure using a predetermined temperature characteristic, a square root of the measured temperature and a square root of the reference temperature. The predetermined temperature characteristic is a gradient of the relationship between square root of temperature and tire pressure.
    Type: Grant
    Filed: October 29, 2021
    Date of Patent: June 6, 2023
    Assignee: AIRBUS SAS
    Inventor: Anand Puntambekar
  • APPARATUS AND METHOD FOR DETERMINING AIRCRAFT TIRE PRESSURE
    Publication number: 20220185039
    Abstract: An apparatus configured to determine the pressure of an aircraft tire at a reference temperature. The apparatus includes a processing system configured to: obtain a measured tire pressure and a measured temperature associated with the measured tire pressure; and determine a tire pressure at the reference temperature by adjusting the measured tire pressure using a predetermined temperature characteristic, a square root of the measured temperature and a square root of the reference temperature. The predetermined temperature characteristic is a gradient of the relationship between square root of temperature and tire pressure.
    Type: Application
    Filed: October 29, 2021
    Publication date: June 16, 2022
    Inventor: Anand PUNTAMBEKAR
  • AIRCRAFT STRUCTURE HAVING CABLES LOCATED IN STRINGERS
    Publication number: 20160129985
    Abstract: An aircraft structure having cables located in stringers is disclosed. According to one embodiment, the aircraft structure includes a stringer having a hollow channel. Further, one or more cables are located within the hollow channel. In one example, the one or more cables are capable of carrying a number of signals.
    Type: Application
    Filed: November 4, 2015
    Publication date: May 12, 2016
    Inventors: Kishore Prasan MOHANTY, Anand PUNTAMBEKAR, Sivananda KAMSALA