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).
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Patent number: 11378132Abstract: 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: GrantFiled: August 7, 2019Date of Patent: July 5, 2022Assignee: THE BOEING COMPANYInventors: Mark R. Meyer, Ben P. Hu
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Patent number: 11053983Abstract: 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: GrantFiled: January 19, 2018Date of Patent: July 6, 2021Assignee: The Boeing CompanyInventors: Mark R. Meyer, Tyler S. Gregson
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Publication number: 20210044196Abstract: 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: ApplicationFiled: August 7, 2019Publication date: February 11, 2021Inventors: Mark R. Meyer, Ben P. Hu
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Publication number: 20190226529Abstract: 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: ApplicationFiled: January 19, 2018Publication date: July 25, 2019Inventors: Mark R. Meyer, Tyler S. Gregson
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Publication number: 20170261040Abstract: 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: ApplicationFiled: May 18, 2017Publication date: September 14, 2017Applicant: The Boeing CompanyInventors: Pradip K. Saha, Mark R. Meyer, Mark E. Bice
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Patent number: 9695877Abstract: 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: GrantFiled: July 28, 2014Date of Patent: July 4, 2017Assignee: The Boeing CompanyInventors: Pradip K. Saha, Mark R. Meyer, Mark E. Bice
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Publication number: 20160025146Abstract: 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: ApplicationFiled: July 28, 2014Publication date: January 28, 2016Applicant: The Boeing CompanyInventors: Pradip K. Saha, Mark R. Meyer, Mark E. Bice
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Patent number: 6789359Abstract: 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: GrantFiled: December 10, 2001Date of Patent: September 14, 2004Assignee: Merrill Millwork, Inc.Inventors: William H. Bauman, Mark R. Meyer
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Publication number: 20030106269Abstract: 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: ApplicationFiled: December 10, 2001Publication date: June 12, 2003Inventors: William H. Bauman, Mark R. Meyer
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Patent number: 5644777Abstract: 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: GrantFiled: March 4, 1992Date of Patent: July 1, 1997Assignee: Rockwell International CorporationInventors: Mark R. Meyer, Lee A. Johnson