Patents by Inventor Stephen G. Dame
Stephen G. Dame 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: 11364992Abstract: Described herein is an example method for aligning an aircraft with a centerline of a runway during takeoff. The method includes accessing a first image captured by a first camera mounted on a first side of the aircraft; accessing a second image captured by a second camera mounted on a second side of the aircraft that is opposite the first side; determining a first angle between a first marked line on the runway in the first image and a first reference line in the first image; determining a second angle between a second marked line on the runway in the second image and a second reference line in the second image; and based on the first angle and the second angle, moving a control surface of the aircraft such that the aircraft moves closer to the centerline of the runway.Type: GrantFiled: October 23, 2018Date of Patent: June 21, 2022Assignee: The Boeing CompanyInventor: Stephen G. Dame
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Patent number: 10906458Abstract: A vehicle includes an interior cabin, and a stowage bin control system. The stowage bin control system includes a plurality of stowage bin assemblies within the interior cabin. The plurality of stowage bin assemblies are configured to be selectively moved between an open position and a closed position. A master control device is separate and distinct from the plurality of stowage bin assemblies. The master control device is communicatively coupled to at least one of the plurality of stowage bin assemblies through wireless connections and is configured to operate the at least one of the plurality of stowage bin assemblies.Type: GrantFiled: June 15, 2017Date of Patent: February 2, 2021Assignee: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Patent number: 10864849Abstract: A stowage bin assembly of a vehicle includes one or more interior light-emitting elements that are configured to illuminate a baggage retaining chamber of the stowage bin assembly. The stowage bin assembly is within an interior cabin of the vehicle.Type: GrantFiled: June 15, 2017Date of Patent: December 15, 2020Assignee: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Patent number: 10793277Abstract: A stowage bin control system and method for a vehicle includes at least one stowage bin assembly that are configured to be selectively moved between an open position and a closed position, and a master control device that is separate and distinct from the stowage bin assemblies. The master control device is communicatively coupled to the stowage bin assemblies and is configured to operate the stowage bin assemblies.Type: GrantFiled: June 15, 2017Date of Patent: October 6, 2020Assignee: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Patent number: 10672208Abstract: A stowage bin assembly includes a latch that is configured to selectively lock and unlock the stowage bin assembly, and a sensor in communication with the latch. The sensor is configured to be engaged to lock, unlock, open, and/or close the stowage bin assembly without the latch or the sensor being touched.Type: GrantFiled: June 15, 2017Date of Patent: June 2, 2020Assignee: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Patent number: 10647429Abstract: A stowage bin assembly is within an interior cabin of a vehicle. The stowage bin assembly includes a weight sensor that is configured to detect the weight of the stowage bin assembly, and a stowage bin control unit in communication with the weight sensor. The stowage bin control unit is configured to automatically close the stowage bin assembly in response to a weight of the stowage bin assembly being within a predetermined range of a maximum weight threshold.Type: GrantFiled: June 15, 2017Date of Patent: May 12, 2020Assignee: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Publication number: 20200122820Abstract: Described herein is an example method for aligning an aircraft with a centerline of a runway during takeoff. The method includes accessing a first image captured by a first camera mounted on a first side of the aircraft; accessing a second image captured by a second camera mounted on a second side of the aircraft that is opposite the first side; determining a first angle between a first marked line on the runway in the first image and a first reference line in the first image; determining a second angle between a second marked line on the runway in the second image and a second reference line in the second image; and based on the first angle and the second angle, moving a control surface of the aircraft such that the aircraft moves closer to the centerline of the runway.Type: ApplicationFiled: October 23, 2018Publication date: April 23, 2020Inventor: Stephen G. Dame
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Publication number: 20180261026Abstract: A stowage bin assembly includes a latch that is configured to selectively lock and unlock the stowage bin assembly, and a sensor in communication with the latch. The sensor is configured to be engaged to lock, unlock, open, and/or close the stowage bin assembly without the latch or the sensor being touched.Type: ApplicationFiled: June 15, 2017Publication date: September 13, 2018Applicant: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Publication number: 20180257784Abstract: A stowage bin assembly is within an interior cabin of a vehicle. The stowage bin assembly includes a weight sensor that is configured to detect the weight of the stowage bin assembly.Type: ApplicationFiled: June 15, 2017Publication date: September 13, 2018Applicant: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Publication number: 20180257783Abstract: A stowage bin control system and method for a vehicle includes at least one stowage bin assembly that are configured to be selectively moved between an open position and a closed position, and a master control device that is separate and distinct from the stowage bin assemblies. The master control device is communicatively coupled to the stowage bin assemblies and is configured to operate the stowage bin assemblies.Type: ApplicationFiled: June 15, 2017Publication date: September 13, 2018Applicant: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Publication number: 20180257555Abstract: A stowage bin assembly of a vehicle includes one or more interior light-emitting elements that are configured to illuminate a baggage retaining chamber of the stowage bin assembly. The stowage bin assembly is within an interior cabin of the vehicle.Type: ApplicationFiled: June 15, 2017Publication date: September 13, 2018Applicant: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Publication number: 20180257554Abstract: A vehicle includes an interior cabin, and a stowage bin control system. The stowage bin control system includes a plurality of stowage bin assemblies within the interior cabin. The plurality of stowage bin assemblies are configured to be selectively moved between an open position and a closed position. A master control device is separate and distinct from the plurality of stowage bin assemblies. The master control device is communicatively coupled to at least one of the plurality of stowage bin assemblies through wireless connections and is configured to operate the at least one of the plurality of stowage bin assemblies.Type: ApplicationFiled: June 15, 2017Publication date: September 13, 2018Applicant: THE BOEING COMPANYInventors: Richard K. Simms, Stephen G. Dame, Mark L. Cloud, Todd D. Smith
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Publication number: 20170332148Abstract: A distributed digital projection system is disclosed which includes a plurality of smart projectors coupled to a head end server computer via a network. Each smart projector has a first network interface coupled to the network. Each smart projector is configured to receive commands and digital content, to process the received commands, and to convert the received digital content into a projection light signal for output. Each smart projector may include a second network interface to allow a daisy-chain network configuration. The head end server computer is configured to issue commands and to forward digital content to each of the at least one smart projectors, the commands specifying at least a time for display of the digital content. The digital content is stored on either network attached storage device coupled to the network or on a storage device directly coupled to or integrated with the head end server computer.Type: ApplicationFiled: May 12, 2016Publication date: November 16, 2017Inventors: James A. Fullerton, Stephen G. Dame, Yakentim M. Ibrahim
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Patent number: 9794346Abstract: A method for monitoring systems of a vehicle may include determining relevant information used by at least one of a plurality of wireless networked computers based on at least a function performed by the at least one wireless networked computer with respect to an associated one of a multiplicity of components of the systems of the vehicle. The method may also include formulating a customized information message for the at least one of the plurality of wireless networked computers based on at least the relevant information used and the function performed by the at least one wireless networked computer. The method may further include transmitting the customized information message to the at least one of the plurality of wireless networked computers.Type: GrantFiled: December 11, 2012Date of Patent: October 17, 2017Assignee: The Boeing CompanyInventors: David Followell, Kevin Swearingen, Jeanne C. Maggiore, Bradley Mitchell, Erik B. Fries, Stephen G. Dame
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Patent number: 9571378Abstract: A system, method, and apparatus for a synchronized wireless data concentrator are provided for facilitating a precisely synchronized system of nodes in a wireless sensor network for airborne data systems. The wireless data concentrator contains a plurality of IEEE 802.15.4 radio/micro-processor subsystems, which are connected to a local host microprocessor, which is in turn connected to an aircraft data network. The airplane data network also contains a precision clock source and a plurality of specialized network switches, which have a low-jitter data-path routing capability.Type: GrantFiled: June 28, 2011Date of Patent: February 14, 2017Assignee: THE BOEING COMPANYInventor: Stephen G. Dame
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Patent number: 9521678Abstract: Embodiments described herein provide for a four-channel Wireless Data Concentrator (WDC) for a data network of an aircraft. One embodiment of a WDC includes a Printed Circuit Board (PCB), and a controller. The controller is electrically coupled to a top surface of the PCB and is proximate to a centerline of the PCB. The WDC further includes four Radio Frequency (RF) transceivers electrically coupled to the top surface of the PCB that are disposed orthogonally to each other around the controller. Each RF transceiver communicates with at least one wireless sensor that measures an environment of the aircraft. The WDC further includes four inverted-F PCB trace antennas fabricated along the top surface of the PCB. Each inverted-F PCB trace antenna is electrically coupled to one of the RF transceivers and is disposed orthogonally to each other around the controller.Type: GrantFiled: March 12, 2015Date of Patent: December 13, 2016Assignee: The Boeing CompanyInventors: Stephen G. Dame, Yakentim M. Ibrahim
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Publication number: 20160270052Abstract: Embodiments described herein provide for a four-channel Wireless Data Concentrator (WDC) for a data network of an aircraft. One embodiment of a WDC includes a Printed Circuit Board (PCB), and a controller. The controller is electrically coupled to a top surface of the PCB and is proximate to a centerline of the PCB. The WDC further includes four Radio Frequency (RF) transceivers electrically coupled to the top surface of the PCB that are disposed orthogonally to each other around the controller. Each RF transceiver communicates with at least one wireless sensor that measures an environment of the aircraft. The WDC further includes four inverted-F PCB trace antennas fabricated along the top surface of the PCB. Each inverted-F PCB trace antenna is electrically coupled to one of the RF transceivers and is disposed orthogonally to each other around the controller.Type: ApplicationFiled: March 12, 2015Publication date: September 15, 2016Inventors: Stephen G. Dame, Yakentim M. Ibrahim
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Patent number: 9083549Abstract: A structure and a first panel are operably disposed with respect to the structure. A first plurality of nodes is disposed within the first panel, including a first plurality of power distribution network nodes in a first power distribution network, and wherein the first plurality of nodes further comprises a first group of nodes. A second panel is operably disposed with respect to the structure. A second plurality of nodes is disposed within the second panel, including a second plurality of power distribution network nodes in a second power distribution network isolated from the first power distribution network. The second plurality of nodes further comprises a second group of nodes. A bus guardian, separate from the two panels, electrically connects the first panel and the second panel. The bus guardian is configured to network the first group of nodes and the second group of nodes in a network.Type: GrantFiled: July 2, 2014Date of Patent: July 14, 2015Assignee: The Boeing CompanyInventor: Stephen G. Dame
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Publication number: 20150003229Abstract: A structure and a first panel are operably disposed with respect to the structure. A first plurality of nodes is disposed within the first panel, including a first plurality of power distribution network nodes in a first power distribution network, and wherein the first plurality of nodes further comprises a first group of nodes. A second panel is operably disposed with respect to the structure. A second plurality of nodes is disposed within the second panel, including a second plurality of power distribution network nodes in a second power distribution network isolated from the first power distribution network. The second plurality of nodes further comprises a second group of nodes. A bus guardian, separate from the two panels, electrically connects the first panel and the second panel. The bus guardian is configured to network the first group of nodes and the second group of nodes in a network.Type: ApplicationFiled: July 2, 2014Publication date: January 1, 2015Inventor: Stephen G. Dame
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Patent number: 8797842Abstract: A structure and a first panel are operably disposed with respect to the structure. A first plurality of nodes is disposed within the first panel, including a first plurality of power distribution network nodes in a first power distribution network, and wherein the first plurality of nodes further comprises a first group of nodes. A second panel is operably disposed with respect to the structure. A second plurality of nodes is disposed within the second panel, including a second plurality of power distribution network nodes in a second power distribution network isolated from the first power distribution network. The second plurality of nodes further comprises a second group of nodes. A bus guardian, separate from the two panels, electrically connects the first panel and the second panel. The bus guardian is configured to network the first group of nodes and the second group of nodes in a network.Type: GrantFiled: March 10, 2011Date of Patent: August 5, 2014Assignee: The Boeing CompanyInventor: Stephen G. Dame