Patents by Inventor Peggy Sansevero

Peggy Sansevero 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: 10688663
    Abstract: An automated airflow inspection system for airfoil blades or vanes includes an operator station for mounting the airfoil and a robotic station for pressure tapping the airfoil. The robotic station includes a vision system and a pressure tapper mounted to a robotic arm. The vision system identifies a pattern of holes of the airfoil blade or vane. The system identifies a hole within the pattern of holes by comparing the pattern of holes to a pre-loaded program associated with the airfoil blade or vane. The system is monitored and controlled by a human to machine interface.
    Type: Grant
    Filed: February 1, 2018
    Date of Patent: June 23, 2020
    Assignee: Raytheon Technologies Corporation
    Inventors: Mary Lynn Tall, Peggy Sansevero
  • Publication number: 20190232497
    Abstract: An automated airflow inspection system for airfoil blades or vanes includes an operator station for mounting the airfoil and a robotic station for pressure tapping the airfoil. The robotic station uses a robotic arm with a mounted vision system and pressure tapper. The system is monitored and controlled by a human to machine interface.
    Type: Application
    Filed: February 1, 2018
    Publication date: August 1, 2019
    Inventors: Mary Lynn Tall, Peggy Sansevero
  • Patent number: 9925876
    Abstract: An airflow testing system for an aerospace component uses a flow master with a first sealing surface, a hollow body, and a metering plate. A desired back pressure across a flow path through the aerospace component is determined, and used to form a metering outlet through the metering plate. The plate is attached to the hollow body in a fluid seal, the flow master is secured to a testing position in a fluid seal, and back pressure across the flow master is sensed while flowing air through the flow master. The difference between desired and sensed back pressure is used to evaluate the airflow testing system.
    Type: Grant
    Filed: August 14, 2015
    Date of Patent: March 27, 2018
    Assignee: United Technologies Corporation
    Inventors: Mary Lynn Tall, Peggy Sansevero
  • Publication number: 20170045392
    Abstract: An airflow testing system for an aerospace component uses a flow master with a first sealing surface, a hollow body, and a metering plate. A desired back pressure across a flow path through the aerospace component is determined, and used to form a metering outlet through the metering plate. The plate is attached to the hollow body in a fluid seal, the flow master is secured to a testing position in a fluid seal, and back pressure across the flow master is sensed while flowing air through the flow master. The difference between desired and sensed back pressure is used to evaluate the airflow testing system.
    Type: Application
    Filed: August 14, 2015
    Publication date: February 16, 2017
    Inventors: Mary Lynn Tall, Peggy Sansevero