Patents by Inventor Gary A. Kinstler

Gary A. Kinstler 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: 9090360
    Abstract: A cryogenically cooled radiation shield device and method are provided to shield an area, such as the capsule of a space vehicle, from radiation. A cryogenically cooled radiation shield device may include at least one first coil comprised of a superconducting material extending about an area to be shielded from radiation. The cryogenically cooled radiation shield device also includes a first conduit extending about the area to be shielded from radiation. The at least one first coil is disposed within the first conduit. The cryogenically cooled radiation shield device also includes a second conduit extending about the area to be shielded from radiation. The first conduit is disposed within the second conduit. The cryogenically cooled radiation shield device also includes a first cryogen liquid disposed within the first conduit and a second cryogen liquid, different than the first cryogen liquid, disposed within the second conduit exterior of the first conduit.
    Type: Grant
    Filed: August 18, 2014
    Date of Patent: July 28, 2015
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Publication number: 20150144739
    Abstract: A cryogenically cooled radiation shield device and method are provided to shield an area, such as the capsule of a space vehicle, from radiation. A cryogenically cooled radiation shield device may include at least one first coil comprised of a superconducting material extending about an area to be shielded from radiation. The cryogenically cooled radiation shield device also includes a first conduit extending about the area to be shielded from radiation. The at least one first coil is disposed within the first conduit. The cryogenically cooled radiation shield device also includes a second conduit extending about the area to be shielded from radiation. The first conduit is disposed within the second conduit. The cryogenically cooled radiation shield device also includes a first cryogen liquid disposed within the first conduit and a second cryogen liquid, different than the first cryogen liquid, disposed within the second conduit exterior of the first conduit.
    Type: Application
    Filed: August 18, 2014
    Publication date: May 28, 2015
    Inventor: Gary A. Kinstler
  • Patent number: 8809824
    Abstract: A cryogenically cooled radiation shield device and method are provided to shield an area, such as the capsule of a space vehicle, from radiation. A cryogenically cooled radiation shield device may include at least one first coil comprised of a superconducting material extending about the area to be shielded. The cryogenically cooled radiation shield device also includes a first inner conduit extending about the area to be shielded from radiation. The at least one first coil is disposed within the first inner conduit. The cryogenically cooled radiation shield device also includes a first outer conduit extending about the area to be shielded from radiation. The first inner conduit is disposed within the first outer conduit. The cryogenically cooled radiation shield device also includes a first cryogen liquid disposed within the first inner conduit and a second cryogen liquid, different than the first cryogen liquid, disposed within the first outer conduit.
    Type: Grant
    Filed: December 13, 2010
    Date of Patent: August 19, 2014
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 8575580
    Abstract: A method and device of shielding an area from radiation are provided. A radiation shield device may include first and second shells at least partially surrounding the area with the second shell being spaced apart from and further away from the area than the first shell. Both the first and second shells include a plurality of coils that are arranged in paired coil groupings and that encircle the area to be shielded from radiation. The coil groupings of the first shell may be configured to support current flow in an opposite direction to that in which the paired coil groupings of the second shell are configured to support current flow. As such, each coil grouping of the first shell has north and south poles that are correspondingly oppositely positioned from the north and south poles of the paired coil grouping of the second shell.
    Type: Grant
    Filed: December 13, 2010
    Date of Patent: November 5, 2013
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 8451860
    Abstract: Switchless deterministic data bus networks and interfaces are disclosed. In one embodiment, a network includes a switchless shared bandwidth data bus; a plurality of nodes in communication with the shared bandwidth data bus; and a deterministic transport layer hosted on each node of the plurality of nodes, the deterministic transport layer providing message scheduling and flow control, the message scheduling using a bandwidth allocation and physical layer prioritization access protocol for scheduling a packet.
    Type: Grant
    Filed: February 8, 2007
    Date of Patent: May 28, 2013
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 8405057
    Abstract: A cryogenically cooled radiation shield device as well as an associated method are provided in order to shield an area, such as a space vehicle capsule, from radiation. The radiation shield device may have embedded cryogen storage. The radiation shield device may include inner and outer coil shells that extend about the area to be shielded. Each coil shell includes coils formed of a superconductive material and disposed within respective first conduits. The radiation shield device may also include a first storage tank configured to store a first cryogen liquid and disposed in fluid communication with the first conduits. The first storage tank is disposed between the inner and outer coil shells. The radiation shield device may further include a second conduit at least partially surrounding the inner and outer coil shells that is at least partially filled with a second cryogen liquid, different than the first cryogen liquid.
    Type: Grant
    Filed: April 22, 2011
    Date of Patent: March 26, 2013
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 8261044
    Abstract: The distributed data handling and processing resources system of the present invention includes a) a number of data handling and processing resource nodes that collectively perform a desired data handling and processing function, each data handling and processing resource node for providing a data handling/processing subfunction; and, b) a low latency, shared bandwidth databus for interconnecting the data handling and processing resource nodes. In the least, among the data handling and processing resource nodes, is a processing unit (PU) node for providing a control and data handling/processing subfunction; and, an input/output (I/O) node for providing a data handling/processing subfunction for data collection/distribution to an external environment. The present invention preferably uses the IEEE-1394b databus due to its unique and specialized low latency, shared bandwidth characteristics.
    Type: Grant
    Filed: December 19, 2007
    Date of Patent: September 4, 2012
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 8210481
    Abstract: There is provided a radiation shield device for providing radiation protection to an area, such as a spacecraft including, for example, a manned vehicle. The radiation shield device comprises a magnetic field generator, such as a solenoid, of superconductive material that provides a magnetic field around the area to shield the area from radiation. The solenoid preferably defines an axial length that is substantially smaller than a diameter of the solenoid. A thermal control system, comprising a limited amount of coolant or a refrigeration cycle, is included to control a temperature of the superconductive material during operation of the magnetic field generator. A magnetic shield device is also provided between the magnetic field generator and the area to be shielded from radiation to substantially shield the area from the magnetic field generated by the magnetic field generator.
    Type: Grant
    Filed: August 19, 2008
    Date of Patent: July 3, 2012
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 8050176
    Abstract: A bus management tool that allows communication to be maintained between a group of nodes operatively connected on two busses in the presence of radiation by transmitting periodically a first message from one to another of the nodes on one of the busses, determining whether the first message was received by the other of the nodes on the first bus, and when it is determined that the first message was not received by the other of the nodes, transmitting a recovery command to the other of the nodes on a second of the of busses. Methods, systems, and articles of manufacture consistent with the present invention also provide for a bus recovery tool on the other node that re-initializes a bus interface circuit operatively connecting the other node to the first bus in response to the recovery command.
    Type: Grant
    Filed: March 30, 2004
    Date of Patent: November 1, 2011
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 7685442
    Abstract: A bus management tool that allows communication to be maintained between a group of nodes operatively connected on two busses in the presence of radiation by transmitting periodically a first message from one to another of the nodes on one of the busses, determining whether the first message was received by the other of the nodes on the first bus, and when it is determined that the first message was not received by the other of the nodes, transmitting a recovery command to the other of the nodes on a second of the of busses. Methods, systems, and articles of manufacture consistent with the present invention also provide for a bus recovery tool on the other node that re-initializes a bus interface circuit operatively connecting the other node to the first bus in response to the recovery command.
    Type: Grant
    Filed: April 26, 2007
    Date of Patent: March 23, 2010
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 7558903
    Abstract: Various methods and systems provide interfaces between legacy data buses such as MIL-STD 1553 buses and wideband wireless data links such as links compatible with IEEE 802.11 or IEEE 802.16e. One technique for interfacing a legacy bus to a wideband wireless data communication link involves providing a hybrid bus controller/remote interface unit as an interface between the two data communication architectures. In operation, the legacy interface suitably receives data intended for a legacy node from a wireless radio module that is compatible with a designated broadband wireless data communication protocol. The legacy data is converted in the legacy interface/remote interface unit to at least one legacy word having a legacy format for transmission on the legacy data bus.
    Type: Grant
    Filed: October 4, 2006
    Date of Patent: July 7, 2009
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Publication number: 20090084903
    Abstract: There is provided a radiation shield device for providing radiation protection to an area, such as a spacecraft including, for example, a manned vehicle. The radiation shield device comprises a magnetic field generator, such as a solenoid, of superconductive material that provides a magnetic field around the area to shield the area from radiation. The solenoid preferably defines an axial length that is substantially smaller than a diameter of the solenoid. A thermal control system, comprising a limited amount of coolant or a refrigeration cycle, is included to control a temperature of the superconductive material during operation of the magnetic field generator. A magnetic shield device is also provided between the magnetic field generator and the area to be shielded from radiation to substantially shield the area from the magnetic field generated by the magnetic field generator.
    Type: Application
    Filed: August 19, 2008
    Publication date: April 2, 2009
    Applicant: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 7484691
    Abstract: There is provided a radiation shield device for providing radiation protection to an area, such as a manned vehicle. The radiation shield device comprises a magnetic field generator, such as a solenoid, of superconductive material that provides a magnetic field around the area to shield the area from radiation. The magnetic field generator preferably comprises at least one trapezoidal portion to provide substantially isotropic protection to the area. A thermal control system, comprising a limited amount of coolant or a refrigeration cycle, is included to control a temperature of the superconductive material during operation of the magnetic field generator. A magnetic shield device may also be provided between the magnetic field generator and the area to be shielded from radiation to substantially shield the area from the magnetic field generated by the magnetic field generator.
    Type: Grant
    Filed: June 30, 2005
    Date of Patent: February 3, 2009
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 7464901
    Abstract: There is provided a radiation shield device for providing radiation protection to an area, such as a manned vehicle. The radiation shield device comprises a magnetic field generator, such as a solenoid, of superconductive material that provides a magnetic field around the area to shield the area from radiation. The solenoid preferably defines an axial length that is substantially smaller than a diameter of the solenoid. A thermal control system, comprising a limited amount of coolant or a refrigeration cycle, is included to control a temperature of the superconductive material during operation of the magnetic field generator. A magnetic shield device is also provided between the magnetic field generator and the area to be shielded from radiation to substantially shield the area from the magnetic field generated by the magnetic field generator.
    Type: Grant
    Filed: January 28, 2005
    Date of Patent: December 16, 2008
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Publication number: 20080192772
    Abstract: Switchless deterministic data bus networks and interfaces are disclosed. In one embodiment, a network includes a switchless shared bandwidth data bus; a plurality of nodes in communication with the shared bandwidth data bus; and a deterministic transport layer hosted on each node of the plurality of nodes, the deterministic transport layer providing message scheduling and flow control, the message scheduling using a bandwidth allocation and physical layer prioritization access protocol for scheduling a packet.
    Type: Application
    Filed: February 8, 2007
    Publication date: August 14, 2008
    Applicant: THE BOEING COMPANY
    Inventor: Gary A. Kinstler
  • Publication number: 20080098059
    Abstract: The distributed data handling and processing resources system of the present invention includes a) a number of data handling and processing resource nodes that collectively perform a desired data handling and processing function, each data handling and processing resource node for providing a data handling/processing subfunction; and, b) a low latency, shared bandwidth databus for interconnecting the data handling and processing resource nodes. In the least, among the data handling and processing resource nodes, is a processing unit (PU) node for providing a control and data handling/processing subfunction; and, an input/output (I/O) node for providing a data handling/processing subfunction for data collection/distribution to an external environment. The present invention preferably uses the IEEE-1394b databus due to its unique and specialized low latency, shared bandwidth characteristics.
    Type: Application
    Filed: December 19, 2007
    Publication date: April 24, 2008
    Inventor: Gary Kinstler
  • Patent number: 7346010
    Abstract: The hybrid data bus includes client nodes and an IEEE-1394b-based network operably associated with those client nodes. At least one of the client nodes is a legacy-based client node that utilizes a non-deterministic network bus type for network interfacing. An IEEE-1394b-based network is operably associated with the client nodes via at least one network interface bridge (NIB). The IEEE-1394b-based network provides a deterministic data passing capability between the legacy-based client node and at least one other of the client nodes.
    Type: Grant
    Filed: January 10, 2003
    Date of Patent: March 18, 2008
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Patent number: 7337255
    Abstract: The distributed data handling and processing resources system of the present invention includes a) a number of data handling and processing resource nodes that collectively perform a desired data handling and processing function, each data handling and processing resource node for providing a data handling/processing subfunction; and, b) a low latency, shared bandwidth databus for interconnecting the data handling and processing resource nodes. In the least, among the data handling and processing resource nodes, is a processing unit (PU) node for providing a control and data handling/processing subfunction; and, an input/output (I/O) node for providing a data handling/processing subfunction for data collection/distribution to an external environment. The present invention preferably uses the IEEE-1394b databus due to its unique and specialized low latency, shared bandwidth characteristics.
    Type: Grant
    Filed: June 12, 2002
    Date of Patent: February 26, 2008
    Assignee: The Boeing Company
    Inventor: Gary A. Kinstler
  • Publication number: 20070288773
    Abstract: A bus management tool that allows communication to be maintained between a group of nodes operatively connected on two busses in the presence of radiation by transmitting periodically a first message from one to another of the nodes on one of the busses, determining whether the first message was received by the other of the nodes on the first bus, and when it is determined that the first message was not received by the other of the nodes, transmitting a recovery command to the other of the nodes on a second of the of busses. Methods, systems, and articles of manufacture consistent with the present invention also provide for a bus recovery tool on the other node that re-initializes a bus interface circuit operatively connecting the other node to the first bus in response to the recovery command.
    Type: Application
    Filed: April 26, 2007
    Publication date: December 13, 2007
    Applicant: THE BOEING COMPANY
    Inventor: Gary Kinstler
  • Publication number: 20070255884
    Abstract: Various methods and systems provide interfaces between legacy data buses such as MIL-STD 1553 buses and wideband wireless data links such as links compatible with IEEE 802.11 or IEEE 802.16e. One technique for interfacing a legacy bus to a wideband wireless data communication link involves providing a hybrid bus controller/remote interface unit as an interface between the two data communication architectures. In operation, the legacy interface suitably receives data intended for a legacy node from a wireless radio module that is compatible with a designated broadband wireless data communication protocol. The legacy data is converted in the legacy interface/remote interface unit to at least one legacy word having a legacy format for transmission on the legacy data bus.
    Type: Application
    Filed: October 4, 2006
    Publication date: November 1, 2007
    Inventor: Gary Kinstler