Patents Assigned to Lockheed Martins Corporation
  • Publication number: 20170115361
    Abstract: A system for magnetic detection of an external magnetic field is disclosed. The system includes a nitrogen vacancy (NV) diamond material comprising a plurality of NV centers, a magnetic field generator that generates a magnetic field, a radio frequency (RF) excitation source that provides RF excitation, an optical excitation source that provides optical excitation, an optical detector that receives an optical signal emitted by the NV diamond material, and a controller. The controller is configured to calculate a control magnetic field, control the magnetic field generator to generate the control magnetic field, receive a light detection signal from the optical detector based on the optical signal due to the sum of the generated control magnetic field and the external magnetic field, store measurement data based on the received light detection signal, and calculate a vector of the external magnetic field based on the stored measurement data.
    Type: Application
    Filed: January 6, 2017
    Publication date: April 27, 2017
    Applicant: Lockheed Martin Corporation
    Inventors: Peter G. Kaup, Arul Manickam
  • Patent number: 9632168
    Abstract: Aspects of the disclosed subject matter involve airborne-based systems, methods, and computer program products for optimizing a laser-based visual disruption countermeasure scan pattern. The scan pattern can be comprised of a plurality of lasers each with their own scan pattern and may be used to disrupt an optical system of a weapon or an individual. Based on the scan patterns and/or data used to generate the scan patterns, the shape or intensity of the scan pattern or patterns can be modified.
    Type: Grant
    Filed: June 19, 2012
    Date of Patent: April 25, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Stephen C. Moraites, Carl R. Herman
  • Patent number: 9633323
    Abstract: An integrated modeling and analysis system (IMAS) receives documents containing information relating to an overall operations system from a number of integrated product teams (IPTs). The IMAS creates a model architecture of the overall system the information received from the participating IPTs. The IMAS automatically imports the information without any interaction from support personnel. A discrete event modeling (DES) application in communication with the IMAS creates a DES model based on the model architecture in the IMAS. The DES application runs a simulation on the model generating statistical data relating to the overall system for analysis. The statistical data generates output reports in a format compatible with the analysis tools of the user. The IMAS includes a customizable user interface which allows a stakeholder to link and control the modeling information received from all other participating IPTs. Prior simulations and results can be archived for later reference.
    Type: Grant
    Filed: March 14, 2013
    Date of Patent: April 25, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Richard G. Fairbrother, Kimberly Z. Homsher, Dennis J. Genaw, Michael A. Leonardo
  • Patent number: 9632315
    Abstract: Head-mounted displays (100) are disclosed which include a frame (107), an image display system (110) supported by the frame (107), and a Fresnel lens system (115) supported by the frame (107). The HMD (100) can employ a reflective optical surface, e.g., a free-space, ultra-wide angle, reflective optical surface (a FS/UWA/RO surface) (120), supported by the frame (107), with the Fresnel lens system (115) being located between the image display system (110) and the reflective optical surface (120). The Fresnel lens system (115) can include at least one curved Fresnel lens element (820). Fresnel lens elements (30) for use in HMDs are also disclosed which have facets (31) separated by edges (32) which lie along radial lines (33) which during use of the HMD pass through a center of rotation (34) of a nominal user's eye (35) or through the center of the eye's lens (36) or are normal to the surface of the eye's cornea.
    Type: Grant
    Filed: August 17, 2011
    Date of Patent: April 25, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: David Alan Smith, Gary E. Wiese, Glenn Clark Cuddihy, Gregory A. Harrison
  • Publication number: 20170110015
    Abstract: Methods and configurations are disclosed for exploiting characteristic magnetic signature of electrical power transmission and distribution lines for navigation.
    Type: Application
    Filed: January 21, 2016
    Publication date: April 20, 2017
    Applicant: Lockheed Martin Corporation
    Inventor: Stephen M. SEKELSKY
  • Patent number: 9625712
    Abstract: A method of deploying a space based occulter is provided. The occulter comprises a base portion and a blanket section extending radially from the base portion. A plurality of starlight blocking petals are attached to the base portion and attached to the blanket section, the petals extending radially from the base portion, each of the petals being hingedly connected to an adjacent petal.
    Type: Grant
    Filed: July 8, 2013
    Date of Patent: April 18, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Domenick Joseph Tenerelli, Sean Patrick McCully, David Putnam
  • Patent number: 9624966
    Abstract: A mechanical joint is provided comprising a bracket having a first elongated opening formed therein. An alignment guide comprising a second elongated opening formed therein is configured to rotatably attach to the bracket and is moveable between a first, floating position, and a second, non-floating position. In the first position the first elongated opening of the bracket and the second elongated opening of the alignment guide are axially aligned with one another and define a single elongated opening. In the second position the first elongated opening of the bracket and the second elongated opening of the alignment guide are partially aligned with one another and define a generally circular opening. The alignment guide is configured to slideably attach to a moveable end of a linear actuator.
    Type: Grant
    Filed: December 20, 2013
    Date of Patent: April 18, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Michael R. Obleman, Blake A. Carnahan, Michael James Avery, Todd Charles Gloo
  • Patent number: 9619687
    Abstract: An article identifier or code including at least one photo-responsive dye and a method of encoding or embedding information in same. A reader device for decoding or extracting information in an article identifier or code and verifying or authenticating that information and the associated extraction and authentication methods.
    Type: Grant
    Filed: January 15, 2014
    Date of Patent: April 11, 2017
    Assignee: LOCKHEED MARTIN CORPORATION
    Inventors: Christian Adams, Richard Allen Vaughn, Joe M. Wright
  • Patent number: 9616459
    Abstract: A method for coating a surface of a material involves contacting a surface of a material with a surface activator containing a fluoride-containing compound and an organic solvent to form an activated surface, contacting the activated surface with a protective reagent to form an initial coated surface, and contacting the initial coated surface with a thinning agent containing a fluoride-containing compound and a surfactant to from a final coated surface, wherein the final coated surface is coated with a protective coating that is covalently bonded to the surface of the material.
    Type: Grant
    Filed: November 21, 2014
    Date of Patent: April 11, 2017
    Assignee: LOCKHEED MARTIN CORPORATION
    Inventors: Linda Ann Lohmeier, Franklin Charles Basile, Wayne Powell, Dennis W. Surface
  • Patent number: 9620861
    Abstract: Embodiments are directed to a multi-fractal pattern antenna, system and method of making multi-fractal pattern antennas. The antenna comprises a fractal antenna pattern having at least one resonant frequency and having a plurality of joined-chevron fractal segments arranged as a function of at least one resonant frequency. Each joined-chevron fractal segment comprising a first chevron comprising a first V-shaped fractal element having a first leg, second leg and a first vertex where the first leg and second leg are separated by a first angle. Each joined-chevron fractal segment comprising a second chevron joined to the first chevron to form a joined-chevron fractal segment and comprising a second V-shaped fractal element having a third leg, fourth leg and a second vertex where the third leg and the fourth leg are separated by a second angle. A set of the plurality of joined-chevron fractal segment approximates a staircase shape.
    Type: Grant
    Filed: June 1, 2015
    Date of Patent: April 11, 2017
    Assignee: LOCKHEED MARTIN CORPORATION
    Inventor: Johnny E. Banks
  • Patent number: 9622356
    Abstract: An assembly and method for mounting an electronic package to a printed circuit board (PCB) in which a gasket is shaped to fit tightly around and under a perimeter edge of an electronic package. The electronic package may be carried by the PCB and comprise electrical package contacts on an underside of the package, which contact PCB contacts on the PCB. The gasket may be disposed between the underside of the package and the PCB substrate and surround the contacts, and may be shaped to fit around and under a perimeter edge of the package to protect the contacts from contamination.
    Type: Grant
    Filed: July 17, 2013
    Date of Patent: April 11, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Tom Rovere, James K. Lake, Rick Micha, Paul Coyne
  • Patent number: 9615992
    Abstract: A system including a compressible element configured to compress a muscle in a limb of a user, a controller configured to control a sequence, rate or amount of compression of the compressible element, and a generator configured to move a working fluid to compress the compressible element as controlled by the controller. The sequence, rate or amount of compression of the compressible element is established to reduce an amount of effort expended by a heart of a user to move a volume of blood. Another system and a method are also disclosed.
    Type: Grant
    Filed: July 30, 2013
    Date of Patent: April 11, 2017
    Assignee: LOCKHEED MARTIN CORPORATION
    Inventors: Edward Henry Allen, Adam C. Salamon
  • Patent number: 9610546
    Abstract: Perforated graphene sheets can be used in forming separation membranes. Separation membranes of the present disclosure, which can be used in gas separation processes in some embodiments, can include one or more layers of perforated graphene and one or more layers of another membrane material. Methods for separating a gas mixture can include contacting a gas mixture with the separation membranes, and transiting one or more of the gases through the perforated graphene so as to affect separation.
    Type: Grant
    Filed: September 16, 2015
    Date of Patent: April 4, 2017
    Assignee: LOCKHEED MARTIN CORPORATION
    Inventors: Steven W. Sinton, Peter V. Bedworth, Padraig Moloney, Jacob L. Swett
  • Patent number: 9614589
    Abstract: A system includes a transmitting device and a receiving device. The transmitting device includes a first processor configured to transmit data to a transmitter and the transmitter. The transmitter is configured to transmit the data via a magnetic field. The receiving device includes a magnetometer configured to detect the magnetic field and a second processor configured to decipher the data from the detected magnetic field.
    Type: Grant
    Filed: January 21, 2016
    Date of Patent: April 4, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Jon C. Russo, Gregory S. Bruce, David N. Coar, Wilbur Lew, Julie L. Miller
  • Patent number: 9611024
    Abstract: Systems and methods for measuring a volume of a ballonet are provided. In some aspects, the system may include a plurality of sensors configured to transmit a plurality of signals toward an interior surface of the ballonet and to receive the plurality of signals reflected off of the interior surface of the ballonet, a distance calculating module configured to calculate a plurality of distances from the plurality of sensors to the interior surface of the ballonet using the received plurality of signals, and a mapping module configured to create a three-dimensional surface using the calculated plurality of distances. The system may further include a measurement module configured to calculate the volume of the ballonet using the three-dimensional surface.
    Type: Grant
    Filed: August 3, 2011
    Date of Patent: April 4, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Douglas H. Greiner, Brian T. Holm-Hansen, John P. Morehead
  • Patent number: 9609752
    Abstract: An interconnect structure and method for manufacturing the same includes a substrate and a copper trace line defined on a surface of the substrate. The copper trace line includes a transmission line and a contact pad. The copper trace line is plated with a layer of metal which will oxidize if exposed to the atmosphere. The layer of metal is further plated with a layer of gold. The gold layer is selectively applied to the transmission line and the contact pad to define a gap on the transmission line at the contact pad. The metal layer is exposed in the gap. An oxide layer is formed on the metal layer in the gap. The oxide layer and the substrate surround the contact pad define a barrier to spread of solder.
    Type: Grant
    Filed: March 14, 2014
    Date of Patent: March 28, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Daniel L. Blass, Jack V. Ajoian
  • Publication number: 20170082371
    Abstract: A one-piece heat exchanger manufactured using an additive manufacturing process is described. The heat exchanger includes a plurality of channels formed therein. At least some of the plurality of channels may be configured to provide structural support to the heat exchanger to reduce its weight. Different coolant media may be used in a first set and a second set of the plurality of channels to provide different types of cooling in an integrated one-piece heat exchanger structure.
    Type: Application
    Filed: September 21, 2015
    Publication date: March 23, 2017
    Applicant: Lockheed Martin Corporation
    Inventors: David L. Vos, Ryan M. Alderfer, Randall J. Stutzman
  • Publication number: 20170082372
    Abstract: A one-piece heat exchanger manufactured using an additive manufacturing process is described. The heat exchanger includes a plurality of channels formed therein. At least some of the plurality of channels may be configured to provide structural support to the heat exchanger to reduce its weight. Different coolant media may be used in a first set and a second set of the plurality of channels to provide different types of cooling in an integrated one-piece heat exchanger structure.
    Type: Application
    Filed: September 21, 2015
    Publication date: March 23, 2017
    Applicant: Lockheed Martin Corporation
    Inventors: David L. Vos, Ryan M. Alderfer, Matthew Daniel Miller
  • Patent number: 9598165
    Abstract: A gas barrier material includes an atomic sheet, such as graphene and/or an analog of graphene. The gas barrier material can be arranged as part of a component, such as a container or other vessel, to limit the flow or permeation of gas through the component. Where the component is a container or part of a container, the gas barrier material may be formulated and arranged to limit or prevent gas ingress or egress with respect to the internal volume of the container. The atomic sheet offers improved gas barrier properties compared to traditional polymeric barrier materials and is particularly useful in applications where it is desired to limit permeation of small gas molecules such as helium, such as airships or other lighter than air vehicles.
    Type: Grant
    Filed: October 3, 2013
    Date of Patent: March 21, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Steven Edward Bullock, Jaime Ballester
  • Patent number: 9600765
    Abstract: A computerized classifier system that forms convex hulls containing all training experiences for each target class (e.g. threat/non-threat) is disclosed. The intersection of convex hulls for each pair of classes defines a region of ambiguity in feature space. Measurement of feature vector(s) outside an ambiguous region of feature space leads to a class decision while measurement of feature vector(s) within an ambiguous region of feature space defined by convex hulls causes a transition to a new feature space with new features. In particular embodiments, measured feature data includes estimated motion states and electrical lengths of a given object, and range, velocity and acceleration image data from second phase differences for debris mitigation.
    Type: Grant
    Filed: March 21, 2016
    Date of Patent: March 21, 2017
    Assignee: Lockheed Martin Corporation
    Inventors: Richard N. Pedersen, Mark A. Friesel, Paul D. Mountcastle