Patents by Inventor James J. Childress
James J. Childress 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: 10772981Abstract: A method and apparatus for disinfecting a lavatory inside a vehicle in response to a set of criteria being met. A determination is made as to whether a set of criteria for activation of a disinfection system that emits far-ultraviolet radiation to perform a disinfection process inside a lavatory has been met. In response to a determination that the set of criteria has been met, the disinfection system is activated to perform the disinfection process inside the lavatory using the far-ultraviolet radiation.Type: GrantFiled: June 11, 2019Date of Patent: September 15, 2020Assignee: The Boeing CompanyInventors: James J. Childress, Mark L. Cloud, Karen Lee Hills
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Publication number: 20190298875Abstract: A method and apparatus for disinfecting a lavatory inside a vehicle in response to a set of criteria being met. A determination is made as to whether a set of criteria for activation of a disinfection system that emits far-ultraviolet radiation to perform a disinfection process inside a lavatory has been met. In response to a determination that the set of criteria has been met, the disinfection system is activated to perform the disinfection process inside the lavatory using the far-ultraviolet radiation.Type: ApplicationFiled: June 11, 2019Publication date: October 3, 2019Inventors: James J. Childress, Mark L. Cloud, Karen Lee Hills
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Patent number: 10377481Abstract: Systems and methods to launch an aircraft are disclosed. In one embodiment, a system to launch an aircraft comprises a launch arm comprising at least one load cell, an aircraft coupled to the launch arm, and a release mechanism in communication with the at least one load cell, wherein the release mechanism releases the aircraft when the at least one load cell indicates that a load on the launch arm is below a predetermined threshold. Other embodiments may be described.Type: GrantFiled: October 26, 2012Date of Patent: August 13, 2019Assignee: The Boeing CompanyInventors: James J. Childress, Daniel J. Perron
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Patent number: 10363329Abstract: A method and apparatus for disinfecting a lavatory inside a vehicle in response to a set of criteria being met. A determination is made as to whether a set of criteria for activation of a disinfection system that emits far-ultraviolet radiation to perform a disinfection process inside a lavatory has been met. In response to a determination that the set of criteria has been met, the disinfection system is activated to perform the disinfection process inside the lavatory using the far-ultraviolet radiation.Type: GrantFiled: April 3, 2017Date of Patent: July 30, 2019Assignee: The Boeing CompanyInventors: James J. Childress, Mark L. Cloud, Karen Lee Hills
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Publication number: 20170202991Abstract: A method and apparatus for disinfecting a lavatory inside a vehicle in response to a set of criteria being met. A determination is made as to whether a set of criteria for activation of a disinfection system that emits far-ultraviolet radiation to perform a disinfection process inside a lavatory has been met. In response to a determination that the set of criteria has been met, the disinfection system is activated to perform the disinfection process inside the lavatory using the far-ultraviolet radiation.Type: ApplicationFiled: April 3, 2017Publication date: July 20, 2017Inventors: James J. Childress, Mark L. Cloud, Karen Lee Hills
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Patent number: 9623133Abstract: A method and apparatus for disinfecting a lavatory inside a vehicle in response to a set of criteria being met. A determination is made as to whether a set of criteria for activation of a disinfection system that emits far-ultraviolet radiation to perform a disinfection process inside a lavatory has been met. In response to a determination that the set of criteria has been met, the disinfection system is activated to perform the disinfection process inside the lavatory using the far-ultraviolet radiation.Type: GrantFiled: January 30, 2015Date of Patent: April 18, 2017Assignee: THE BOEING COMPANYInventors: James J. Childress, Mark L. Cloud, Karen Lee Hills
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Patent number: 9597859Abstract: A self-sealing bladder may automatically seal a puncture wound formed in a bladder wall thereof, such as due to being perforated by a projectile. Self-sealing bladders may be used in containers, such as fuel tanks, in order to prevent loss of fuel or other fluid from the container. Self-sealing bladders may contain a sealant material contained within one or more localized reservoirs formed within the bladder wall, the sealant material being pressurized within the bladder wall such that a localized reduction in pressure due to a perforation in the bladder wall causes the sealant material to migrate to the perforated site, whereupon the sealant material hardens, thereby sealing the wound. The localized reservoirs may include one or more channels and/or connecting layers extending therefrom and in fluid communication therewith, to facilitate migration of the sealant material away from the localized reservoirs and towards the perforated portion of the bladder wall.Type: GrantFiled: May 27, 2015Date of Patent: March 21, 2017Assignee: The Boeing CompanyInventors: James J. Childress, Mark Stewart Wilenski, Michael Patrick Kozar
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Publication number: 20160347038Abstract: A self-sealing bladder may automatically seal a puncture wound formed in a bladder wall thereof, such as due to being perforated by a projectile. Self-sealing bladders may be used in containers, such as fuel tanks, in order to prevent loss of fuel or other fluid from the container. Self-sealing bladders may contain a sealant material contained within one or more localized reservoirs formed within the bladder wall, the sealant material being pressurized within the bladder wall such that a localized reduction in pressure due to a perforation in the bladder wall causes the sealant material to migrate to the perforated site, whereupon the sealant material hardens, thereby sealing the wound. The localized reservoirs may include one or more channels and/or connecting layers extending therefrom and in fluid communication therewith, to facilitate migration of the sealant material away from the localized reservoirs and towards the perforated portion of the bladder wall.Type: ApplicationFiled: May 27, 2015Publication date: December 1, 2016Applicant: The Boeing CompanyInventors: James J. Childress, Mark Stewart Wilenski, Michael Patrick Kozar
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Publication number: 20160220716Abstract: A method and apparatus for disinfecting a lavatory inside a vehicle in response to a set of criteria being met. A determination is made as to whether a set of criteria for activation of a disinfection system that emits far-ultraviolet radiation to perform a disinfection process inside a lavatory has been met. In response to a determination that the set of criteria has been met, the disinfection system is activated to perform the disinfection process inside the lavatory using the far-ultraviolet radiation.Type: ApplicationFiled: January 30, 2015Publication date: August 4, 2016Inventors: James J. Childress, Mark L. Cloud, Karen Lee Hills
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Patent number: 9266619Abstract: A tank and associated fabrication method are provided which may limit the damage otherwise occasioned by the impact of a ballistic projectile. The tank may include a wall assembly defined between outer and inner walls and a plurality of restraining elements that extend between the walls. The restraining elements may be formed to have a plurality of layers of material that form not only the restraining element, but also portions of the inner and/or outer walls. For example, the tank may include a plurality of cells positioned adjacent to one another with each cell forming portions of two adjacent restraining elements and portions of the inner and/or outer walls. A corresponding method for fabricating a tank including a wall assembly having a plurality of restraining elements is also provided.Type: GrantFiled: April 21, 2014Date of Patent: February 23, 2016Assignee: The Boeing CompanyInventors: James J. Childress, Dan Perron
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Patent number: 9144960Abstract: A device uses magnetic force generated by a magnet to intensify compaction pressure applied to a composite laminate.Type: GrantFiled: February 7, 2013Date of Patent: September 29, 2015Assignee: THE BOEING COMPANYInventors: James J. Childress, Alan W. Baker, Mark Klewiada
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Patent number: 9045218Abstract: Systems and methods to launch an aircraft are disclosed. In one embodiment, a system comprises an electrically powered buoyant aircraft, a control system to maneuver the aircraft and a tether adapted to couple to the aircraft and to a ground-based power supply to provide power to the aircraft while the aircraft is coupled to the tether. The aircraft can disconnect autonomously from the tether in response to a command signal.Type: GrantFiled: March 8, 2013Date of Patent: June 2, 2015Assignee: The Boeing CompanyInventors: James J. Childress, John J. Viniotis
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Publication number: 20140223744Abstract: A tank and associated fabrication method are provided which may limit the damage otherwise occasioned by the impact of a ballistic projectile. The tank may include a wall assembly defined between outer and inner walls and a plurality of restraining elements that extend between the walls. The restraining elements may be formed to have a plurality of layers of material that form not only the restraining element, but also portions of the inner and/or outer walls. For example, the tank may include a plurality of cells positioned adjacent to one another with each cell forming portions of two adjacent restraining elements and portions of the inner and/or outer walls. A corresponding method for fabricating a tank including a wall assembly having a plurality of restraining elements is also provided.Type: ApplicationFiled: April 21, 2014Publication date: August 14, 2014Applicant: THE BOEING COMPANYInventors: James J. Childress, Dan Perron
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Publication number: 20140117153Abstract: Systems and methods to launch an aircraft are disclosed. In one embodiment, a system to launch an aircraft comprises a launch arm comprising at least one load cell, an aircraft coupled to the launch arm, and a release mechanism in communication with the at least one load cell, wherein the release mechanism releases the aircraft when the at least one load cell indicates that a load on the launch arm is below a predetermined threshold. Other embodiments may be described.Type: ApplicationFiled: October 26, 2012Publication date: May 1, 2014Inventors: James J. Childress, Daniel J. Perron
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Patent number: 8701926Abstract: A tank and associated fabrication method are provided which may limit the damage otherwise occasioned by the impact of a ballistic projectile. The tank may include a wall assembly defined between outer and inner walls and a plurality of restraining elements that extend between the walls. The restraining elements may be formed to have a plurality of layers of material that form not only the restraining element, but also portions of the inner and/or outer walls. For example, the tank may include a plurality of cells positioned adjacent to one another with each cell forming portions of two adjacent restraining elements and portions of the inner and/or outer walls. A corresponding method for fabricating a tank including a wall assembly having a plurality of restraining elements is also provided.Type: GrantFiled: June 23, 2008Date of Patent: April 22, 2014Assignee: The Boeing CompanyInventors: James J. Childress, Dan Perron
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Patent number: 8240502Abstract: A method for providing a fuel tank assembly is provided with the fuel tank assembly configured to limit the damage otherwise occasioned by the impact of a ballistic projectile. The fuel tank assembly may include a bladder defined between exterior and interior bladder walls, with the interior bladder wall defining a volume for storing fuel. The exterior bladder wall is at least as rigid than the interior bladder wall. The fuel tank assembly can also include connectors between the exterior and interior bladder walls to at least partially limit expansion of the bladder. The fuel tank assembly can also include an inlet opening into the bladder to permit a pressurized gas to be introduced into the bladder. The fuel tank assembly may also include a valve through the interior bladder wall into the volume for storing fuel to permit at least some of the pressurized gas to be introduced therein.Type: GrantFiled: December 30, 2010Date of Patent: August 14, 2012Assignee: The Boeing CompanyInventors: James J. Childress, Warren A. Davis, II
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Publication number: 20120181288Abstract: A tank and associated fabrication method are provided which may limit the damage otherwise occasioned by the impact of a ballistic projectile. The tank may include a wall assembly defined between outer and inner walls and a plurality of restraining elements that extend between the walls. The restraining elements may be formed to have a plurality of layers of material that form not only the restraining element, but also portions of the inner and/or outer walls. For example, the tank may include a plurality of cells positioned adjacent to one another with each cell forming portions of two adjacent restraining elements and portions of the inner and/or outer walls. A corresponding method for fabricating a tank including a wall assembly having a plurality of restraining elements is also provided.Type: ApplicationFiled: June 23, 2008Publication date: July 19, 2012Inventors: James J. Childress, Dan Perron
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Publication number: 20110094598Abstract: A method for providing a fuel tank assembly is provided with the fuel tank assembly configured to limit the damage otherwise occasioned by the impact of a ballistic projectile. The fuel tank assembly may include a bladder defined between exterior and interior bladder walls, with the interior bladder wall defining a volume for storing fuel. The exterior bladder wall is at least as rigid than the interior bladder wall. The fuel tank assembly can also include connectors between the exterior and interior bladder walls to at least partially limit expansion of the bladder. The fuel tank assembly can also include an inlet opening into the bladder to permit a pressurized gas to be introduced into the bladder. The fuel tank assembly may also include a valve through the interior bladder wall into the volume for storing fuel to permit at least some of the pressurized gas to be introduced therein.Type: ApplicationFiled: December 30, 2010Publication date: April 28, 2011Inventors: James J. Childress, Warren A. Davis, II
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Patent number: 7861884Abstract: A fuel tank assembly are provided which may limit the damage otherwise occasioned by the impact of a ballistic projectile. The fuel tank assembly may include a bladder defined between exterior and interior bladder walls, with the interior bladder wall defining a volume for storing fuel. The exterior bladder wall is at least as or more rigid than the interior bladder wall. The fuel tank assembly can also include connectors between the exterior and interior bladder walls to at least partially limit expansion of the bladder. The fuel tank assembly can also include an inlet opening into the bladder to permit a pressurized gas to be introduced into the bladder. The fuel tank assembly may also include a valve through the interior bladder wall into the volume for storing fuel to permit at least some of the pressurized gas to be introduced therein.Type: GrantFiled: October 8, 2007Date of Patent: January 4, 2011Assignee: The Boeing CompanyInventors: James J. Childress, Warren A. Davis, II
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Publication number: 20090090724Abstract: A fuel tank assembly and associated method are provided which may limit the damage otherwise occasioned by the impact of a ballistic projectile. The fuel tank assembly may include a bladder defined between exterior and interior bladder walls, with the interior bladder wall defining a volume for storing fuel. The exterior bladder wall is at least as or more rigid than the interior bladder wall. The fuel tank assembly can also include connectors between the exterior and interior bladder walls to at least partially limit expansion of the bladder. The fuel tank assembly can also include an inlet opening into the bladder to permit a pressurized gas to be introduced into the bladder. The fuel tank assembly may also include a valve through the interior bladder wall into the volume for storing fuel to permit at least some of the pressurized gas to be introduced therein.Type: ApplicationFiled: October 8, 2007Publication date: April 9, 2009Applicant: The Boeing CompanyInventors: James J. Childress, Warren A. Davis, II