Patents by Inventor Harshinder Singh

Harshinder Singh 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).

  • AIRCRAFT LIGHTNING STRIKE PROTECTION
    Publication number: 20240083138
    Abstract: A lightning strike protection (LSP) apparatus includes a first layer of fiber glass. The LSP apparatus also includes a second layer positioned on the first layer. The second layer includes carbon nanotubes (CNT). The LSP apparatus also includes a third layer positioned on the second layer. The third layer includes a surfacer. The LSP apparatus also includes a fourth layer positioned on the third layer. The fourth layer also includes the fiber glass. The LSP apparatus also includes a fifth layer positioned on the fourth layer. The fifth layer includes a primer. The LSP apparatus also includes a sixth layer positioned on the fifth layer. The sixth layer includes an outer surface material.
    Type: Application
    Filed: September 14, 2022
    Publication date: March 14, 2024
    Applicant: The Boeing Company
    Inventors: Manojkumar Sabanayagam, Harshinder Singh, Mallikarjun Ghasane, Suhasini Lakshmi Darsiv, Ramalakshmi Rajendiran, Ameya Deshpande
  • Aircraft brake cooling systems and methods
    Patent number: 11441628
    Abstract: Systems and methods for aircraft brake cooling are described. A system may include an air hose configured to intake pressurized air at a first end of the air hose from an aircraft propulsor. A nozzle at a second end of the air hose may be configured to exit the pressurized air through the air hose to a braking system. An actuator may be configured to allow the pressurized air to flow through the air hose or prevent the pressurized air from flowing through the air hose.
    Type: Grant
    Filed: January 29, 2020
    Date of Patent: September 13, 2022
    Assignee: The Boeing Company
    Inventors: Prashant Iyer Ganesh, Harshinder Singh
  • AIRCRAFT BRAKE COOLING SYSTEMS AND METHODS
    Publication number: 20210231184
    Abstract: Systems and methods for aircraft brake cooling are described. A system may include an air hose configured to intake pressurized air at a first end of the air hose from an aircraft propulsor. A nozzle at a second end of the air hose may be configured to exit the pressurized air through the air hose to a braking system. An actuator may be configured to allow the pressurized air to flow through the air hose or prevent the pressurized air from flowing through the air hose.
    Type: Application
    Filed: January 29, 2020
    Publication date: July 29, 2021
    Inventors: Prashant Iyer Ganesh, Harshinder Singh