Patents by Inventor Sujith N. Mally

Sujith N. Mally 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: 9697395
    Abstract: Systems, methods, and apparatus for identifying parts with electromagnetic identification (EMID) tags are disclosed. In one or more embodiments, a method involves receiving, with a first antenna(s) on a mobile EMID reader portal, a first signal(s) from an EMID tag(s). The method further involves transmitting, with a second antenna(s) on the mobile EMID reader portal, a second signal(s) to an access point(s). Also, the method involves transmitting, with the access point(s), a third signal(s) to an EMID processing system and a location processing system. In addition, the method involves determining, with the location processing system, the location of the mobile EMID reader portal. Additionally, the method involves transmitting, by the location processing system, the location of the mobile EMID reader portal to the EMID processing system. Further, the method involves associating, by the EMID processing system, the EMID tag(s) with the location of the mobile EMID reader portal.
    Type: Grant
    Filed: July 11, 2014
    Date of Patent: July 4, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Sujith N. Mally, Michael D. McInnis
  • Patent number: 9364880
    Abstract: In one example, an adapter assembly for a system for cold working a portion of a metal layer of a metal/composite structure is provided. The portion being cold worked may surround a hole in a structure that includes the metal layer and a non-metal layer. In some examples, the adapter assembly includes a shim adapter housing including a face wall, having a first aperture that is larger than the hole, and a side wall, extending from the face wall. A cavity is at least partially delimited by the face wall and the side wall. The adapter assembly also includes a shim, dimensioned to fit within the cavity. The shim has a second aperture that is larger than the first aperture. Other embodiments may be described.
    Type: Grant
    Filed: June 14, 2013
    Date of Patent: June 14, 2016
    Assignee: The Boeing Company
    Inventors: Matthew J. Weigel, Jr., Sujith N. Mally
  • Publication number: 20160012263
    Abstract: Systems, methods, and apparatus for identifying parts with electromagnetic identification (EMID) tags are disclosed. In one or more embodiments, a method involves receiving, with a first antenna(s) on a mobile EMID reader portal, a first signal(s) from an EMID tag(s). The method further involves transmitting, with a second antenna(s) on the mobile EMID reader portal, a second signal(s) to an access point(s). Also, the method involves transmitting, with the access point(s), a third signal(s) to an EMID processing system and a location processing system. In addition, the method involves determining, with the location processing system, the location of the mobile EMID reader portal. Additionally, the method involves transmitting, by the location processing system, the location of the mobile EMID reader portal to the EMID processing system. Further, the method involves associating, by the EMID processing system, the EMID tag(s) with the location of the mobile EMID reader portal.
    Type: Application
    Filed: July 11, 2014
    Publication date: January 14, 2016
    Inventors: Sujith N. Mally, Michael D. McInnis
  • Patent number: 8387226
    Abstract: A method and apparatus are present for removing a blind fastener from a structure. A first hole is drilled in a guide located around a center of a head of a core bolt in a body of the blind fastener to form a pilot hole. A second hole is drilled in the pilot hole in the head of the core bolt. The head of the core bolt is separated from the shaft of the core bolt. The core bolt is separated from the body. The core bolt is moved out of the body after the core bolt has been separated from the body. A head of the body is separated from a shaft of the body. The shaft of the body is moved out of the structure.
    Type: Grant
    Filed: December 8, 2008
    Date of Patent: March 5, 2013
    Assignee: The Boeing Company
    Inventors: Matthew J. Weigel, Jr., Sujith N. Mally
  • Patent number: 8294571
    Abstract: A system verifies torquing of pressure fittings in an aircraft wheel well. A strain gauge and an ultra-wide band (UWB) pulse signal generator are placed on a wrench used to torque the fittings. The strain senses the torque applied by the wrench, and the pulse signal generator generates UWB pulse signals indicating the location of the fitting and the torque applied to the fitting. The pulse signals are received by UWB radios within the wheel well, which generate location measurements based on the received pulse signals. A processor automatically calculates the location of the fitting being torqued based on the location measurements, and a display produces a 3-dimensional image of the fittings and their torque status.
    Type: Grant
    Filed: July 13, 2010
    Date of Patent: October 23, 2012
    Assignee: The Boeing Company
    Inventors: Donald W. Coffland, Sujith N. Mally, Russell N. Tice
  • Publication number: 20110164657
    Abstract: A system verifies torquing of pressure fittings in an aircraft wheel well. A strain gauge and an ultra-wide band (UWB) pulse signal generator are placed on a wrench used to torque the fittings. The strain senses the torque applied by the wrench, and the pulse signal generator generates UWB pulse signals indicating the location of the fitting and the torque applied to the fitting. The pulse signals are received by UWB radios within the wheel well, which generate location measurements based on the received pulse signals. A processor automatically calculates the location of the fitting being torqued based on the location measurements, and a display produces a 3-dimensional image of the fittings and their torque status.
    Type: Application
    Filed: July 13, 2010
    Publication date: July 7, 2011
    Applicant: The Boeing Company
    Inventors: Donald W. Coffland, Sujith N. Mally, Russell N. Tice
  • Patent number: 7876216
    Abstract: A system verifies torquing of pressure fittings in an aircraft wheel well. A strain gauge and an ultra-wide band (UWB) pulse signal generator are placed on a wrench used to torque the fittings. The strain senses the torque applied by the wrench, and the pulse signal generator generates UWB pulse signals indicating the location of the fitting and the torque applied to the fitting. The pulse signals are received by UWB radios within the wheel well, which generate location measurements based on the received pulse signals. A processor automatically calculates the location of the fitting being torqued based on the location measurements, and a display produces a 3-dimensional image of the fittings and their torque status.
    Type: Grant
    Filed: June 25, 2008
    Date of Patent: January 25, 2011
    Assignee: The Boeing Company
    Inventors: Donald W. Coffland, Sujith N. Mally, Russell N. Tice
  • Publication number: 20110000064
    Abstract: A method and apparatus are present for removing a blind fastener from a structure. A first hole is drilled in a guide located around a center of a head of a core bolt in a body of the blind fastener to form a pilot hole. A second hole is drilled in the pilot hole in the head of the core bolt. The head of the core bolt is separated from the shaft of the core bolt. The core bolt is separated from the body. The core bolt is moved out of the body after the core bolt has been separated from the body. A head of the body is separated from a shaft of the body. The shaft of the body is moved out of the structure.
    Type: Application
    Filed: December 8, 2008
    Publication date: January 6, 2011
    Inventors: Matthew J. Weigel, JR., Sujith N. Mally
  • Publication number: 20090322516
    Abstract: A system verifies torquing of pressure fittings in an aircraft wheel well. A strain gauge and an ultra-wide band (UWB) pulse signal generator are placed on a wrench used to torque the fittings. The strain senses the torque applied by the wrench, and the pulse signal generator generates UWB pulse signals indicating the location of the fitting and the torque applied to the fitting. The pulse signals are received by UWB radios within the wheel well, which generate location measurements based on the received pulse signals. A processor automatically calculates the location of the fitting being torqued based on the location measurements, and a display produces a 3-dimensional image of the fittings and their torque status.
    Type: Application
    Filed: June 25, 2008
    Publication date: December 31, 2009
    Inventors: Donald W. Coffland, Sujith N. Mally, Russell N. Tice
  • Patent number: 7555820
    Abstract: Various methods and apparatuses for removing blind fasteners, portions of blind fasteners, and/or other fasteners from structural assemblies are described herein. In one embodiment, a blind fastener can have a core bolt extending through a passage in a body. One method for removing the blind fastener from a structural assembly in accordance with one aspect of the invention can include removing a head portion from the core bolt, and driving the remaining portion of the core bolt at least partially through the body in a first direction. The method can further include extracting the body from the bore in a second direction opposite to the first direction. In one embodiment, the body can be extracted from the bore by inserting a tool into the passage and engaging the body, and then pulling the body in the second direction with the tool.
    Type: Grant
    Filed: January 24, 2005
    Date of Patent: July 7, 2009
    Assignee: The Boeing Company
    Inventors: Paul A. McEldowney, Sujith N. Mally
  • Patent number: 7299961
    Abstract: An adjustable depth control device for a fastener driving tool has an attachment member which is used to couple the adjustable depth control device to the fastener driving tool. An adjustment member is coupled to the attachment member to adjust and control a driving depth of the fastener driving tool. A stopping head is formed on a rivet die of the fastener driving tool for keeping the rivet die in a chamber of the fastener driving tool and for limiting a distance the rivet die will travel.
    Type: Grant
    Filed: March 2, 2006
    Date of Patent: November 27, 2007
    Assignee: The Boeing Company
    Inventors: Paul N. Stavig, Jr., Sujith N. Mally, Jeffrey W. Hamilton