Patents by Inventor Anmol Dhandhania

Anmol Dhandhania 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).

  • PITOT TUBE SENSING APPARATUS
    Publication number: 20230408720
    Abstract: A pitot tube sensing apparatus and method are disclosed for determining the presence or absence of a foreign object within the pitot tube sensing apparatus, and including a pitot tube having a channel, a pressure sensor coupled to the channel, a capacitor and a system. The capacitor includes two electrodes on opposing sides of the channel. The system measures a parameter indicative of a capacitance between the two electrodes and determines the presence or absence of a foreign object within the channel based on the parameter.
    Type: Application
    Filed: June 20, 2023
    Publication date: December 21, 2023
    Inventor: Anmol DHANDHANIA
  • ROTATION WARNING
    Publication number: 20230166860
    Abstract: A method of warning of early rotation of an aircraft during takeoff is disclosed. An improvement in aircraft performance and passenger comfort can be realised by monitoring for signs of early rotation and warning the pilot of such. By detecting when rotation has been commanded by the pilot, and the aircraft nose has started to lift off the ground, when the speed of the aircraft is below a threshold, early rotation can be determined and an auditory warning can mitigate the impact of that on aircraft performance.
    Type: Application
    Filed: November 29, 2022
    Publication date: June 1, 2023
    Inventor: Anmol DHANDHANIA
  • Split winglet
    Patent number: 10625847
    Abstract: A split winglet has a leading airfoil (LA) comprising a LA leading edge, a LA trailing edge, a LA upper surface, and a LA lower surface. The split winglet also has a trailing airfoil (TA) comprising a TA leading edge, a TA trailing edge, a TA upper surface, and a TA lower surface. The split winglet further has a base connected to each of the LA and the TA, the base being configured for connection to a tip of a main airfoil.
    Type: Grant
    Filed: April 21, 2017
    Date of Patent: April 21, 2020
    Assignee: Textron Innovations Inc.
    Inventor: Anmol Dhandhania
  • Split Winglet
    Publication number: 20180304997
    Abstract: A split winglet has a leading airfoil (LA) comprising a LA leading edge, a LA trailing edge, a LA upper surface, and a LA lower surface. The split winglet also has a trailing airfoil (TA) comprising a TA leading edge, a TA trailing edge, a TA upper surface, and a TA lower surface. The split winglet further has a base connected to each of the LA and the TA, the base being configured for connection to a tip of a main airfoil.
    Type: Application
    Filed: April 21, 2017
    Publication date: October 25, 2018
    Applicant: Bell Helicopter Textron Inc.
    Inventor: Anmol Dhandhania