Patents by Inventor Mark S. Shander

Mark S. Shander 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: 11203979
    Abstract: Apparatus and system for containing a rupture of a duct. The apparatus includes an air-permeable sheet, such as a wide-weave fiberglass sheet. The air-permeable sheet includes a strap arranged on a first side of the sheet such that it forms diamond-shaped patterns along a longitudinal axis. The strap can be made of a tight-weave fiberglass. Laterally-spaced corners of the diamond-shaped patterns include connection members that can be engaged to affix the strap and the air-permeable sheet around a duct. Various aspects include an air-impermeable air barrier surrounding the wide-weave fiberglass sheet and strap. The air barrier can include a window that directs air from a ruptured duct. Various aspects can be used on a bleed-air duct of an aircraft. The window of the air barrier can be aimed at a temperature sensor. A valve can close the bleed-air duct if the temperature sensor detects a high temperature leak.
    Type: Grant
    Filed: August 24, 2018
    Date of Patent: December 21, 2021
    Assignee: THE BOEING COMPANY
    Inventors: Christopher Wheaton, Mark S. Shander
  • Patent number: 10493930
    Abstract: A solid state primary power switching network for modular equipment centers (MECs) distributing primary power throughout a vehicle. The solid state primary power switching network includes multiple primary power switch network devices (PPSNDs) of a MEC for controlling and distributing primary power to other MECs spatially distribute throughout a vehicle. In one or more configurations, the PPSNDs have a universal structure in that each includes a common power input source and a plurality of common power outputs. In one or more configurations, primary power sources to the vehicle are switched without a perceivably visible break in power.
    Type: Grant
    Filed: June 12, 2017
    Date of Patent: December 3, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Mark S. Shander, N. Evan Lurton, Thomas F. Currier, Todd B. Brouwer, Mark E. Liffring, Jon J. Dhondt, Carolyn Kerr, Robert D. Holley, Lowell W. Schaffner, Eugene V. Solodovnik, Terrance L. Thomas
  • Publication number: 20180363560
    Abstract: Apparatus and system for containing a rupture of a duct. The apparatus includes an air-permeable sheet, such as a wide-weave fiberglass sheet. The air-permeable sheet includes a strap arranged on a first side of the sheet such that it forms diamond-shaped patterns along a longitudinal axis. The strap can be made of a tight-weave fiberglass. Laterally-spaced corners of the diamond-shaped patterns include connection members that can be engaged to affix the strap and the air-permeable sheet around a duct. Various aspects include an air-impermeable air barrier surrounding the wide-weave fiberglass sheet and strap. The air barrier can include a window that directs air from a ruptured duct. Various aspects can be used on a bleed-air duct of an aircraft. The window of the air barrier can be aimed at a temperature sensor. A valve can close the bleed-air duct if the temperature sensor detects a high temperature leak.
    Type: Application
    Filed: August 24, 2018
    Publication date: December 20, 2018
    Inventors: Christopher WHEATON, Mark S. SHANDER
  • Publication number: 20170274847
    Abstract: A solid state primary power switching network for modular equipment centers (MECs) distributing primary power throughout a vehicle. The solid state primary power switching network includes multiple primary power switch network devices (PPSNDs) of a MEC for controlling and distributing primary power to other MECs spatially distribute throughout a vehicle. In one or more configurations, the PPSNDs have a universal structure in that each includes a common power input source and a plurality of common power outputs. In one or more configurations, primary power sources to the vehicle are switched without a perceivably visible break in power.
    Type: Application
    Filed: June 12, 2017
    Publication date: September 28, 2017
    Inventors: Mark S. SHANDER, N. Evan LURTON, Thomas F. CURRIER, Todd B. BROUWER, Mark E. LIFFRING, Jon J. DHONDT, Carolyn KERR, Robert D. HOLLEY, Lowell W. SCHAFFNER, Eugene V. SOLODOVNIK, Terrance L. THOMAS
  • Patent number: 9678488
    Abstract: A system and method for performing build verification of equipment systems after being installed in a partially constructed vehicle portion. After installing one or more of prerequisite equipment systems during a current build stage of a vehicle build plan, the installed equipment systems are tested during the current build stage to determine whether the installed equipment systems are electrically connected correctly.
    Type: Grant
    Filed: November 19, 2013
    Date of Patent: June 13, 2017
    Assignee: The Boeing Company
    Inventors: Jon J. Dhondt, Michael B. McAvoy, Terrance L. Thomas, Mark S. Shander, Alberto Ferrer, Steven M. Walstrom
  • Patent number: 9676351
    Abstract: A solid state primary power switching network for modular equipment centers (MECs) distributing primary power throughout a vehicle. The solid state primary power switching network includes multiple primary power switch network devices (PPSNDs) of a MEC for controlling and distributing primary power to other MECs spatially distribute throughout a vehicle. In one or more configurations, the PPSNDs have a universal structure in that each includes a common power input source and a plurality of common power outputs. In one or more configurations, primary power sources to the vehicle are switched without a perceivably visible break in power.
    Type: Grant
    Filed: October 11, 2013
    Date of Patent: June 13, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Mark S. Shander, N. Evan Lurton, Thomas F. Currier, Todd B. Brouwer, Mark E. Liffring, Jon J. Dhondt, Carolyn Kerr, Robert D. Holley, Lowell W. Schaffner, Eugene Solodovnik, Terrance L. Thomas
  • Patent number: 9561761
    Abstract: A plurality of modular equipment centers (MECs) spatially distributed throughout a vehicle servicing equipment loads. Each MEC independently provides localized power and communication to service the equipment loads. A zone of electrical loads is assigned to and serviced by the nearest MEC. Power and communication data are synchronized in that each equipment load receives power and data from the same MEC. In one embodiment, if a MEC experiences an operational inconsistency, one or more other MECs are assigned the equipment loads of the operationally inconsistent MEC.
    Type: Grant
    Filed: October 11, 2013
    Date of Patent: February 7, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Steven M. Walstrom, Todd B. Brouwer, Thomas F. Currier, Thomas R. Hasenoehrl, Carolyn Kerr, Mark E. Liffring, Lowell W. Schaffner, Mark S. Shander
  • Patent number: 9561867
    Abstract: A composite vehicle architecture without a current return network for reducing lightning threats. A plurality of modular equipment centers (MECs) are spatially distributed throughout the vehicle. Equipment loads within the vehicle are each serviced by the nearest MEC. Twisted and shielded electrical conductor pairs provide secondary power to the equipment loads to minimize the amount of wire throughout the aircraft as well as the return currents on the aircraft.
    Type: Grant
    Filed: October 11, 2013
    Date of Patent: February 7, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Mark E. Liffring, John T. Paterson, Mark S. Shander, Marvin J. Whitney, Ed Woods, Thomas R. Hasenoehrl, Kamiar J. Karimi
  • Patent number: 9561760
    Abstract: A modular truss assembly configured to be placed in small or narrow spaces such as within the floor, sidewall, or crown of a vehicle for mechanically and electrically mounting system components of a modular equipment center (MEC). A plurality of MECs is spatially distributed throughout the vehicle to service equipment loads. The modular truss assembly provides different voltage levels for powering the system components of the MEC and for powering the equipment loads. In one or more configurations, all or part of the modular truss assembly can be removed from the vehicle for repair or replacement.
    Type: Grant
    Filed: October 11, 2013
    Date of Patent: February 7, 2017
    Assignee: THE BOEING COMPANY
    Inventors: Mark S. Shander, Ty A. Larsen, Robert T Johnson, Mark E. Liffring, Margaret Douglas, Christopher M. Severns
  • Patent number: 9511728
    Abstract: A plurality of modular equipment centers (MECs) spatially distributed throughout a vehicle servicing equipment loads. Each MEC independently provides localized power and communication to service the equipment loads and each equipment load is serviced by the nearest MEC. In at least one embodiment, only primary power is distributed across section breaks of the vehicle to minimize the number of connections between section breaks, reduce overall vehicle weight, and to increase vehicle build rate.
    Type: Grant
    Filed: October 11, 2013
    Date of Patent: December 6, 2016
    Assignee: THE BOEING COMPANY
    Inventors: Mark S. Shander, Mark E. Liffring, Todd B. Brouwer, Robert T. Johnson, Carolyn Kerr, John T. Peters, Timothy E. Jackson, Thomas R. Hasenoehrl, Steven M. Walstrom, Arnold W. Nordsieck, Robert L. Springgay
  • Patent number: 9183983
    Abstract: A modular truss assembly for mechanically and electrically mounting system components of a modular equipment center (MEC). A plurality of MECs is spatially distributed throughout the vehicle to service equipment loads. The modular truss assembly provides different voltage levels for powering the system components of the MEC and for powering the equipment loads. In one or more configurations, a MEC incorporate inductive power coupling for powering a line replaceable unit (LRU) in proximity to the modular truss assembly without exposed electrical connections and such that the MEC may forgo power conversion equipment. In one or more configurations, a sensor is embedded in one or more transfer layers of the truss for measuring a power trace embedded in the modular truss assembly.
    Type: Grant
    Filed: October 11, 2013
    Date of Patent: November 10, 2015
    Assignee: THE BOEING COMPANY
    Inventors: Mark E. Liffring, Robert D. Holley, Ty A. Larsen, John T. Paterson, Lowell W. Schaffner, Christopher M. Severns, Thomas R. Hasenoehrl, Mark S. Shander, Seth C. Tai, Ronald C. Yabut
  • Publication number: 20150103457
    Abstract: A solid state primary power switching network for modular equipment centers (MECs) distributing primary power throughout a vehicle. The solid state primary power switching network includes multiple primary power switch network devices (PPSNDs) of a MEC for controlling and distributing primary power to other MECs spatially distribute throughout a vehicle. In one or more configurations, the PPSNDs have a universal structure in that each includes a common power input source and a plurality of common power outputs. In one or more configurations, primary power sources to the vehicle are switched without a perceivably visible break in power.
    Type: Application
    Filed: October 11, 2013
    Publication date: April 16, 2015
    Applicant: The Boeing Company
    Inventors: Mark S. Shander, N. Evan Lurton, Thomas F. Currier, Todd B. Brouwer, Mark E. Liffring, Jon J. Dhondt, Carolyn Kerr, Robert D. Holley, Lowell W. Schaffner, Eugene Solodovnik, Terrance L. Thomas
  • Publication number: 20150103458
    Abstract: A modular truss assembly for mechanically and electrically mounting system components of a modular equipment center (MEC). A plurality of MECs is spatially distributed throughout the vehicle to service equipment loads. The modular truss assembly provides different voltage levels for powering the system components of the MEC and for powering the equipment loads. In one or more configurations, a MEC incorporate inductive power coupling for powering a line replaceable unit (LRU) in proximity to the modular truss assembly without exposed electrical connections and such that the MEC may forgo power conversion equipment. In one or more configurations, a sensor is embedded in one or more transfer layers of the truss for measuring a power trace embedded in the modular truss assembly.
    Type: Application
    Filed: October 11, 2013
    Publication date: April 16, 2015
    Applicant: The Boeing Company
    Inventors: Mark E. Liffring, Robert D. Holley, Ty A. Larsen, John T. Paterson, Lowell W. Schaffner, Christopher M. Severns, Thomas R. Hasenoehrl, Mark S. Shander, Seth C. Tai, Ronald C. Yabut
  • Publication number: 20150102662
    Abstract: A plurality of modular equipment centers (MECs) spatially distributed throughout a vehicle servicing equipment loads. Each MEC independently provides localized power and communication to service the equipment loads. A zone of electrical loads is assigned to and serviced by the nearest MEC. Power and communication data are synchronized in that each equipment load receives power and data from the same MEC. In one embodiment, if a MEC experiences an operational inconsistency, one or more other MECs are assigned the equipment loads of the operationally inconsistent MEC.
    Type: Application
    Filed: October 11, 2013
    Publication date: April 16, 2015
    Applicant: The Boeing Company
    Inventors: Steven M. Walstrom, Todd B. Brouwer, Thomas F. Currier, Thomas R. Hasenoehrl, Carolyn Kerr, Mark E. Liffring, Lowell W. Schaffner, Mark S. Shander
  • Publication number: 20150102660
    Abstract: A modular truss assembly configured to be placed in small or narrow spaces such as within the floor, sidewall, or crown of a vehicle for mechanically and electrically mounting system components of a modular equipment center (MEC). A plurality of MECs is spatially distributed throughout the vehicle to service equipment loads. The modular truss assembly provides different voltage levels for powering the system components of the MEC and for powering the equipment loads. In one or more configurations, all or part of the modular truss assembly can be removed from the vehicle for repair or replacement.
    Type: Application
    Filed: October 11, 2013
    Publication date: April 16, 2015
    Applicant: The Boeing Company
    Inventors: Mark S. Shander, Ty A. Larsen, Robert T. Johnson, Mark E. Liffring, Margaret Douglas, Christopher M. Severns
  • Publication number: 20150102661
    Abstract: A plurality of modular equipment centers (MECs) spatially distributed throughout a vehicle servicing equipment loads. Each MEC independently provides localized power and communication to service the equipment loads and each equipment load is serviced by the nearest MEC. In at least one embodiment, only primary power is distributed across section breaks of the vehicle to minimize the number of connections between section breaks, reduce overall vehicle weight, and to increase vehicle build rate.
    Type: Application
    Filed: October 11, 2013
    Publication date: April 16, 2015
    Applicant: The Boeing Company
    Inventors: Mark S. Shander, Mark E. Liffring, Todd B. Brouwer, Robert T. Johnson, Carolyn Kerr, John T. Peters, Timothy E. Jackson, Thomas R. Hasenoehrl, Steven M. Walstrom, Arnold W. Nordsieck, Robert L. Springgay
  • Publication number: 20150102659
    Abstract: A composite vehicle architecture without a current return network for reducing lightning threats. A plurality of modular equipment centers (MECs) are spatially distributed throughout the vehicle. Equipment loads within the vehicle are each serviced by the nearest MEC. Twisted and shielded electrical conductor pairs provide secondary power to the equipment loads to minimize the amount of wire throughout the aircraft as well as the return currents on the aircraft.
    Type: Application
    Filed: October 11, 2013
    Publication date: April 16, 2015
    Applicant: The Boeing Company
    Inventors: Mark E. Liffring, John T. Paterson, Mark S. Shander, Marvin J. Whitney, Ed Woods, Thomas R. Hasenoehrl, Kamiar J. Karimi
  • Patent number: 7687927
    Abstract: An electrical architecture for an aircraft is provided. The electrical architecture is particularly suitable for relatively small, compact, and lightweight aircraft. In one embodiment, the electrical architecture includes an electrical generator component coupled to the aircraft engine, and an air compression system coupled to the electrical generator component. The electrical generator component is configured to receive mechanical power from the engine and to generate a constant frequency AC electrical power from the engine mechanical power, and the air compression system is configured to receive the constant frequency AC power as an input and, in response thereto, produce a pressurized air output having variable characteristics (for example, a variable flow rate or a variable air pressure).
    Type: Grant
    Filed: November 21, 2007
    Date of Patent: March 30, 2010
    Assignee: The Boeing Company
    Inventors: Mark S. Shander, Richard A. Cote, Michael L. Drake, Howard Carter, III, John T. Peters, Casey Y. K. Ng, Michael S. Hoag, John T. Paterson
  • Publication number: 20090127855
    Abstract: An electrical architecture for an aircraft is provided. The electrical architecture is particularly suitable for relatively small, compact, and lightweight aircraft. In one embodiment, the electrical architecture includes an electrical generator component coupled to the aircraft engine, and an air compression system coupled to the electrical generator component. The electrical generator component is configured to receive mechanical power from the engine and to generate a constant frequency AC electrical power from the engine mechanical power, and the air compression system is configured to receive the constant frequency AC power as an input and, in response thereto, produce a pressurized air output having variable characteristics (for example, a variable flow rate or a variable air pressure).
    Type: Application
    Filed: November 21, 2007
    Publication date: May 21, 2009
    Inventors: Mark S. Shander, Richard A. Cote, Michael L. Drake, Howard Carter, III, John T. Peters, Casey Y.K. Ng, Michael S. Hoag, John T. Paterson
  • Patent number: 6822458
    Abstract: An apparatus and method for simulating arcing events for use in testing arc fault circuit interrupters. The apparatus and method utilizes a plurality of motion sensitive switches, for example, mercury switches or ball-tilt switches, secured within the housing. When the apparatus is moved the switches interrupt a current flow mimicking arcing events.
    Type: Grant
    Filed: April 17, 2003
    Date of Patent: November 23, 2004
    Assignee: The Boeing Company
    Inventor: Mark S. Shander