Patents by Inventor Mary Lynn Tall

Mary Lynn Tall 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: 10760446
    Abstract: An airflow mask tool incudes a pressure side mask portion to seal at least a portion of a pressure side of a component having an array of internal passageways and a suction side mask portion to seal at least a portion of a suction side of the component, at least one of the suction side mask portion and the pressure side mask portion comprising at least one opening to expose at least one exit from the array of internal passageways.
    Type: Grant
    Filed: February 9, 2018
    Date of Patent: September 1, 2020
    Assignee: Raytheon Technologies Corporation
    Inventors: Mary Lynn Tall, John D. Laggis, III, Natalie Jean DiStefano
  • Patent number: 10710272
    Abstract: A monolithic airflow testing mold suitable for mating with a workpiece includes a platform portion formed from a first material having a first hardness. The mold further includes a workpiece mating portion surrounding by the platform portion. The mating portion includes a support region abutting the platform portion and formed from a second material having a second hardness, and a sealing surface positioned above the support region and formed from a third material having a third hardness. The sealing surface is configured to mate with and extend into a hollow portion of the workpiece. The first hardness is different from at least one of the second and third hardnesses.
    Type: Grant
    Filed: December 14, 2017
    Date of Patent: July 14, 2020
    Assignee: United Technologies Corporation
    Inventors: Mary Lynn Tall, Matthew A. Mertens
  • 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: 20190249564
    Abstract: An airflow mask tool incudes a pressure side mask portion to seal at least a portion of a pressure side of a component having an array of internal passageways and a suction side mask portion to seal at least a portion of a suction side of the component, at least one of the suction side mask portion and the pressure side mask portion comprising at least one opening to expose at least one exit from the array of internal passageways.
    Type: Application
    Filed: February 9, 2018
    Publication date: August 15, 2019
    Applicant: United Technologies Corporation
    Inventors: Mary Lynn Tall, John D. Laggis, III, Natalie Jean DiStefano
  • 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
  • Publication number: 20190184600
    Abstract: A monolithic airflow testing mold suitable for mating with a workpiece includes a platform portion formed from a first material having a first hardness. The mold further includes a workpiece mating portion surrounding by the platform portion. The mating portion includes a support region abutting the platform portion and formed from a second material having a second hardness, and a sealing surface positioned above the support region and formed from a third material having a third hardness. The sealing surface is configured to mate with and extend into a hollow portion of the workpiece. The first hardness is different from at least one of the second and third hardnesses.
    Type: Application
    Filed: December 14, 2017
    Publication date: June 20, 2019
    Inventors: Mary Lynn Tall, Matthew A. Mertens
  • 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