Patents by Inventor Mark R. Meyer

Mark R. Meyer 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: 11378132
    Abstract: A torque tube assembly includes a torque tube, and a fitting attached to the torque tube by a first EMF joint and by a second EMF joint. The first EMF joint comprises a first plurality of torque lands formed proximate a first end of the torque tube and a first plurality of fitting lands formed proximate a first end of the fitting. The second EMF joint comprises a second plurality of torque lands formed distal to the first end of the torque tube and a second plurality of fitting lands formed distal to the first end of the fitting.
    Type: Grant
    Filed: August 7, 2019
    Date of Patent: July 5, 2022
    Assignee: THE BOEING COMPANY
    Inventors: Mark R. Meyer, Ben P. Hu
  • Patent number: 11053983
    Abstract: Example torque tube assemblies may be used with aircraft high lift devices. An example torque tube assembly includes a torque tube having a first end and a second end opposite the first end. A first fitting is coupled to the first end and a second fitting is coupled to the second end. The first fitting is to be coupled to a first high lift device of an aircraft. The second fitting has a spline section. The torque tube assembly also includes a sliding spline shaft having a channel and a first yoke. The second fitting is slidably received within the channel. The torque tube assembly further includes a spline coupling having a second yoke, which is coupled to the first yoke of the sliding spline shaft to form a U-joint. The spline coupling is to be coupled to a second high lift device of the aircraft.
    Type: Grant
    Filed: January 19, 2018
    Date of Patent: July 6, 2021
    Assignee: The Boeing Company
    Inventors: Mark R. Meyer, Tyler S. Gregson
  • Publication number: 20210044196
    Abstract: A torque tube assembly includes a torque tube, and a fitting attached to the torque tube by a first EMF joint and by a second EMF joint. The first EMF joint comprises a first plurality of torque lands formed proximate a first end of the torque tube and a first plurality of fitting lands formed proximate a first end of the fitting. The second EMF joint comprises a second plurality of torque lands formed distal to the first end of the torque tube and a second plurality of fitting lands formed distal to the first end of the fitting.
    Type: Application
    Filed: August 7, 2019
    Publication date: February 11, 2021
    Inventors: Mark R. Meyer, Ben P. Hu
  • Publication number: 20190226529
    Abstract: Example torque tube assemblies for use with aircraft high lift devices are described herein. An example torque tube assembly includes a torque tube having a first end and a second end opposite the first end. A first fitting is coupled to the first end and a second fitting is coupled to the second end. The first fitting is to be coupled to a first high lift device of an aircraft. The second fitting has a spline section. The torque tube assembly also includes a sliding spline shaft having a channel and a first yoke. The second fitting is slidably received within the channel. The torque tube assembly further includes a spline coupling having a second yoke, which is coupled to the first yoke of the sliding spline shaft to form a U-joint. The spline coupling is to be coupled to a second high lift device of the aircraft.
    Type: Application
    Filed: January 19, 2018
    Publication date: July 25, 2019
    Inventors: Mark R. Meyer, Tyler S. Gregson
  • Publication number: 20170261040
    Abstract: One aspect of the present disclosure relates to an apparatus comprising a first end fitting. The first end fitting comprises a tube engagement portion. The tube engagement portion comprises an outer coupling surface. The outer coupling surface comprises a first virtual cross-section. The first virtual cross-section comprises a first transverse inflection point. Each point along the first virtual cross-section has a first virtual tangent line coplanar with the first virtual cross-section.
    Type: Application
    Filed: May 18, 2017
    Publication date: September 14, 2017
    Applicant: The Boeing Company
    Inventors: Pradip K. Saha, Mark R. Meyer, Mark E. Bice
  • Patent number: 9695877
    Abstract: One aspect of the present disclosure relates to an apparatus comprising a first end fitting. The first end fitting comprises a tube engagement portion. The tube engagement portion comprises an outer coupling surface. The outer coupling surface comprises a first virtual cross-section. The first virtual cross-section comprises a first transverse inflection point. Each point along the first virtual cross-section has a first virtual tangent line coplanar with the first virtual cross-section.
    Type: Grant
    Filed: July 28, 2014
    Date of Patent: July 4, 2017
    Assignee: The Boeing Company
    Inventors: Pradip K. Saha, Mark R. Meyer, Mark E. Bice
  • Publication number: 20160025146
    Abstract: One aspect of the present disclosure relates to an apparatus comprising a first end fitting. The first end fitting comprises a tube engagement portion. The tube engagement portion comprises an outer coupling surface. The outer coupling surface comprises a first virtual cross-section. The first virtual cross-section comprises a first transverse inflection point. Each point along the first virtual cross-section has a first virtual tangent line coplanar with the first virtual cross-section.
    Type: Application
    Filed: July 28, 2014
    Publication date: January 28, 2016
    Applicant: The Boeing Company
    Inventors: Pradip K. Saha, Mark R. Meyer, Mark E. Bice
  • Patent number: 6789359
    Abstract: A sill assembly for doors and windows that provides a weep system for channeling water away from the sill assembly. The sill assembly includes an elongated frame member formed with a longitudinally extending upwardly open channel that defines a rear wall, a front wall and a floor that extends laterally and slopes downwardly from the rear wall to the front wall, and a sill that extends laterally from the front wall to a forward edge of the frame member. An end plug is securely mounted to one end of the elongated frame member and has a laterally extending drainage ramp disposed at a location flush with and immediately adjacent to the floor of the channel. The ramp leads to a drainage chamber which in turn has an opening closed by a hinged weep door.
    Type: Grant
    Filed: December 10, 2001
    Date of Patent: September 14, 2004
    Assignee: Merrill Millwork, Inc.
    Inventors: William H. Bauman, Mark R. Meyer
  • Publication number: 20030106269
    Abstract: A sill assembly for doors and windows that provides a weep system for channeling water away from the sill assembly. The sill assembly includes an elongated frame member formed with a longitudinally extending upwardly open channel that defines a rear wall, a front wall and a floor that extends laterally and slopes downwardly from the rear wall to the front wall, and a sill that extends laterally from the front wall to a forward edge of the frame member. An end plug is securely mounted to one end of the elongated frame member and has a laterally extending drainage ramp disposed at a location flush with and immediately adjacent to the floor of the channel. The ramp leads to a drainage chamber which in turn has an opening closed by a hinged weep door.
    Type: Application
    Filed: December 10, 2001
    Publication date: June 12, 2003
    Inventors: William H. Bauman, Mark R. Meyer
  • Patent number: 5644777
    Abstract: An enhanced modular avionics system for communication and processing in an air transport aircraft including a modular avionic cabinet having a first scsi bus for a first processor and associate memory wherein the first scsi bus extends across a first portion of the cabinet and a second scsi bus for connection to a second processor and associate memory which extends across a second portion of the cabinet where the first portion of the cabinet and the second portion of the cabinet together equal the entire cabinet and there is no overlapping between the first portion and the second portion. Also shown is an extended bus which extends the entire length of the cabinet. The extended bus is located a predetermined distance from the top edge of the cabinet, while the first and second buses are located in a parallel line with each other and with the extended bus, the same predetermined distance from the bottom edge of the cabinet.
    Type: Grant
    Filed: March 4, 1992
    Date of Patent: July 1, 1997
    Assignee: Rockwell International Corporation
    Inventors: Mark R. Meyer, Lee A. Johnson