Patents Assigned to Lockheed Martin Corporation
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Publication number: 20130186601Abstract: A wickless heat pipe including a first tube and a second tube. The first tube may form a first shape extending longitudinally in a first direction. The second tube may form a second shape extending longitudinally in a second direction different from the first direction. The first tube and the second tube intersect at at least one location. The two tubes may intersect at a right angle or an oblique angle. The first and second tube may intersect at a plurality of locations. The tubes may be formed from a metal plate used as a thermal ground plane.Type: ApplicationFiled: January 18, 2013Publication date: July 25, 2013Applicant: Lockheed Martin CorporationInventors: Robert J. Monson, Brian Van Lear
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Patent number: 8493273Abstract: An antenna array comprises two or more antenna elements. Each of the two or more antenna elements is configured to scan within a field of view. Each of the two or more antenna elements is further configured to transmit or receive a signal. The antenna array also comprises a metamaterial lens coupled to the two or more antenna elements. The metamaterial lens is configured to distribute the signal according to a sinc-like distribution over an aperture of the antenna array.Type: GrantFiled: March 19, 2012Date of Patent: July 23, 2013Assignee: Lockheed Martin CorporationInventor: Erik Lier
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Patent number: 8493651Abstract: An apparatus and method that provides management and cooling of an optical fiber by looping the optical fiber around the inner surface of a heat-conductive cylinder and around the outer surface of the heat-conductive cylinder, such that the optical fiber enters and exits the heat-conductive cylinder on substantially the same plane. Some embodiments use a continuous groove on the inside and outside of the cylinder for guiding and managing the optical fiber. Some embodiments use a plurality of protruding fiber guides for guiding and managing the optical fiber. Some embodiments use an integrated tube for guiding and managing the optical fiber. In some embodiments, the optical fiber looped on the inner surface and outer surface are spaced apart substantially equally. In some other embodiments, the optical fiber loops are spaced further apart for portions of the fiber carrying higher power.Type: GrantFiled: November 23, 2010Date of Patent: July 23, 2013Assignee: Lockheed Martin CorporationInventors: Yongdan Hu, Eric C. Eisenberg, Aleksandra Shepsis
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Patent number: 8494981Abstract: A system, method, and computer-readable instructions for real-time characters with learning capabilities. A plurality of rules are defined in a rules-based system, each of the rules defining a condition that determines a behavior of a virtual agent when the rule is triggered by the condition being satisfied so that upon triggering of multiple rules at the same time, each of the behaviors of the multiple rules whose conditions were satisfied are combined into a resultant behavior for the virtual agent. This resultant behavior is compared with a desired behavior to providing feedback in the form of rewards or punishments to each of the multiple rules based on their corresponding contribution to the resultant behavior as compared to the desired behavior.Type: GrantFiled: June 21, 2010Date of Patent: July 23, 2013Assignee: Lockheed Martin CorporationInventors: Gregory A. Harrison, Thomas Wonneberger, Jason Tr Smith, David S. Maynard, Eric W. Worden
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Patent number: 8493715Abstract: An apparatus for holding a flight data recorder in an aircraft includes a housing that defines a compartment enclosing the flight data recorder and a flotation device attached to the flight data recorder. If the aircraft crashes into a body of water and become submerged, one or more releasable fasteners holding the compartment's cover in place are triggered thereby removing the cover over an opening in the compartment and ejecting the flotation device and the flight data recorder out of the compartment. The floatation device then floats the flight data recorder to the surface of the water where it can be located by the rescuers.Type: GrantFiled: April 21, 2010Date of Patent: July 23, 2013Assignee: Lockheed Martin CorporationInventor: Marc T. Angelucci
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Patent number: 8495738Abstract: A method, a network node, and a set of instructions are disclosed. A network interface 260 may have a precedent network address to represent the network node 104 in the network 100. A processor 210 may recognize an address hop trigger. The processor 210 may change to a successor network address to represent the network node 104 in the network 100.Type: GrantFiled: October 21, 2011Date of Patent: July 23, 2013Assignee: Lockheed Martin CorporationInventors: James B. Burnham, Neil R. Lofland, Michael Hegarty, Robert W. Hale
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Patent number: 8495736Abstract: A method and apparatus that provides information assurance attributes through a data providence architecture is disclosed. The method may include receiving a message having a data provenance wrapper, examining each data provenance record of the message and any attachments for discrepancies, identifying any discrepancies in the examination of each data provenance record of the message and any attachments; calculating a degree of trust based on any discrepancies identified in the examination of each data provenance record of the message and any attachments, and outputting the degree of trust to the user.Type: GrantFiled: January 5, 2010Date of Patent: July 23, 2013Assignee: Lockheed Martin CorporationInventors: Stephen J. Dill, Bruce Barnett, Andrew Crapo, Abha Moitra
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Patent number: 8490620Abstract: A solar trough includes a light receiver for transporting a fluid to be heated by the solar trough, at least one rail partially or fully disposed in a trench, a parabolic light collector slidably mounted on the at least one rail, and a drive unit for rotating the parabolic light collector within the trench. Further, a solar trough system made up of a plurality of the solar troughs.Type: GrantFiled: October 23, 2008Date of Patent: July 23, 2013Assignee: Lockheed Martin CorporationInventors: Koeunyi Bae, Stephen A. Monforto, Alan E. Taber, David S. Munsky
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Publication number: 20130182886Abstract: A computerized method for intelligently distributing computer processing of mail piece scan images across a plurality of mail piece scan image processors. The method can include receiving a mail piece scan image from a mail piece scan image job requestor and selecting one of a plurality of scan mail piece scan image processors to process said mail piece scan image. The mail piece scan image can be transmitted to said one of a plurality of plurality of mail piece scan image processors and a mail piece scan image processing result can be received from said one of a plurality of plurality of mail piece scan image processors. Post-processing operations can be performed based on said mail piece scan image processing result. The mail piece scan image processing result can be transmitted to said mail piece scan image processing requestor.Type: ApplicationFiled: January 17, 2012Publication date: July 18, 2013Applicant: Lockheed Martin CorporationInventors: Chad Coleman, Keith Quinn, Edward Ovando
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Publication number: 20130182888Abstract: A nontransitory computer readable medium having stored thereon software instructions that, when executed by a computer, cause the computer to perform operations. The operations can include intercepting a request for manual processing of a mail piece image. The request can be transmitted by an originating MPE having failed to resolve the mail piece image. The request can be ignored and the mail piece scan image can be forwarded to an automated mail recognition system (AMRS). If the AMRS successfully resolved the image, a response, including a plurality of addressing data corresponding to the mail piece scan image, can be received from the AMRS. If the AMRS successfully resolved the image, at least a portion of the plurality of addressing data can be transmitted to the originating MPE. If the AMRS did not successfully resolve the image, the request can be forwarded to a manual mail recognition processing system.Type: ApplicationFiled: January 17, 2012Publication date: July 18, 2013Applicant: Lockheed Martin CorporationInventor: Edward Ovando
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Publication number: 20130182889Abstract: A computerized method for retrofitting a legacy manual mail recognition processing system (MRPS) with an automated MRPS without substantial changes to the configuration of the legacy manual MRPS includes detecting a request by a keyer desk software component to display a mail piece scan image on a computer display connected to the keyer desk computer. The image can at least temporarily be prevented from being displayed on the computer display and the image can be read from memory. Automated recognition processing can be performed on the image to resolve the image and create an automated recognition processing results data. If said automated recognition processing was successful the automated recognition processing results data can be sent to the keyer desk software component and the image can be permanently prevented from being displayed on the computer display. Otherwise, the image can be displayed to the human user for manual processing.Type: ApplicationFiled: January 17, 2012Publication date: July 18, 2013Applicant: Lockheed Martin CorporationInventor: Edward Ovando
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Publication number: 20130185801Abstract: A system for secure data processing can include an electronic data storage device and a field programmable gate array coupled to the electronic data storage device. The field programmable gate array can be configured to include a data storage section for performing a data storage operation and a data retrieval section for performing a data retrieval operation. The data storage operation can include obtaining a seed value and retrieving one or more algebraic operations based on the seed value. The storage operation can also include processing input data according to the one or more algebraic operations to generate pseudorandom output data, prepending the seed value to the output data and storing the output data in the electronic data storage device.Type: ApplicationFiled: January 17, 2012Publication date: July 18, 2013Applicant: Lockheed Martin CorporationInventors: Walter S. Richter, Daniel J. Moch, Ricky R. Martin, Michael Hochdoerfer, Max Smirnoff, Thomas J. Hanley
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Publication number: 20130181525Abstract: A pulse generator system and method, including an inductive storage device configured to perform a charging process using a high current received from a first power supply; and a switch that is powered by a second power supply and configured to receive a step signal through a gate driver for controlling a repetition rate of the inductive storage device charging process and a pulse repetition frequency (PRF) of an output pulse.Type: ApplicationFiled: January 18, 2012Publication date: July 18, 2013Applicant: Lockheed Martin CorporationInventors: Raymond A. de Jesus, J. Patrick Roney, Joshua Wiehn
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Publication number: 20130184978Abstract: A system and method to improve efficiency in aircraft maneuvers meant to accommodate time-related constraints in air traffic. Information related to flight performance and atmospheric conditions is gathered onboard an aircraft, then transmitted to an air traffic control center. In the event of a delay or any other event which necessitates an alteration in an aircraft trajectory, the data is sent to a decision support tool to compute and provide alternative trajectories, preferably including operator-preferred trajectories, within air traffic constraints. Air traffic controllers can then offer an alternative trajectory to an aircraft that is more efficient, cost effective, and/or preferable to the aircraft operator.Type: ApplicationFiled: March 6, 2013Publication date: July 18, 2013Applicants: LOCKHEED MARTIN CORPORATION, GENERAL ELECTRIC COMPANYInventors: GENERAL ELECTRIC COMPANY, LOCKHEED MARTIN CORPORATION
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Patent number: 8484976Abstract: A fluidic effector provides enhanced plume mixing for an aircraft engine. Air jet injectors are located on both the external and internal cowl surfaces and angled in opposite directions to induce large scale vortices in the exhaust plume. The vortices mix actuation air with the exhaust plume to produce ejector action. The plume mixes out quickly, thereby lowering jet noise and jet exhaust temperature. The injectors have orientations and injection rates that are adjustable to allow variable mixing rates for use at different flight and engine conditions.Type: GrantFiled: June 12, 2008Date of Patent: July 16, 2013Assignee: Lockheed Martin CorporationInventors: Bradley C. Leland, David M. Wells
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Patent number: 8488784Abstract: An encryption technique that creates a unique encryption key or fingerprint based on unique physical and electrical characteristics of a target electronic assembly to be protected. The encryption key can be constructed by exploiting the manufacturing variances present in all electronic elements including active elements and passive elements. Active elements include, for example: oscillators/clocks, internal I/O controllers, external I/O controllers, memory, processors, and digital power converters. Passive elements include, for example: internal I/O interconnects, external I/O interconnects, memory buses, and power buses. The encryption key can also include one or more environmental condition thresholds.Type: GrantFiled: November 9, 2011Date of Patent: July 16, 2013Assignee: Lockheed Martin CorporationInventors: Howard J. Schantz, Rick C. Stevens
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Patent number: 8485251Abstract: Systems and methods of enhancing crude oil flow radiate electromagnetic energy in the form of focused far field electromagnetic energy into a permeable formation containing the crude oil so as to cause the oil to decrease in viscosity without a substantial change in temperature of the crude oil, increasing the ability of the oil to flow within the formation toward the well and enabling recovery from the reservoir.Type: GrantFiled: August 20, 2009Date of Patent: July 16, 2013Assignee: Lockheed Martin CorporationInventors: Vincent Benischek, Michael Currie, Rajneeta Basantkumar, Gennady Lyasko
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Patent number: 8485566Abstract: A door for mission critical enclosures, for example, cabinets containing sensitive items, such as electronics that may be exposed to high stress environments, for example shock and vibration. The door structure described provides improved mounting and lock features that can allow easy access while maintaining rigid structural needs and integrity. A door assembly for a cabinet generally includes a door that can be fitted directly, or indirectly, to an enclosure through an adapter frame. Generally, the door has fitting structures that operate as interlocking, tight fitting key sets. The fittings provide suitable detent features. An actuatable lock mechanism respectively locks and unlocks the door. The actuatable lock mechanism includes a ramped locking bolt that can engage a ramped surface of the cabinet or adapter frame to facilitate locking and unlocking of the door.Type: GrantFiled: July 1, 2009Date of Patent: July 16, 2013Assignee: Lockheed Martin CorporationInventors: Jeffrey M. Borning, Scott M. Ralston, David J. Shelander, Nathan E. Stremick, John A. Holst
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Patent number: 8489865Abstract: A command chain system includes plurality of processing elements, a memory, and a chain engine. The chain engine is in communication with the memory and accesses instructions in the memory. The chain engine accesses a subroutine stored in the memory. The chain engine sends a command to a specialized hardware. The chain engine performs an action determined by one or more of the operation-code portion, the skip portion, and the loop-count portion of the instruction.Type: GrantFiled: April 15, 2010Date of Patent: July 16, 2013Assignee: Lockheed Martin CorporationInventors: Joshua W. Rensch, Marlon O. Gunderson, James V. Hedin
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Patent number: 8486305Abstract: A method of fabricating copper nanoparticles includes heating a copper salt solution that includes a copper salt, an N,N-dialkylethylenediamine, and a C6-C18 alkylamine in an organic solvent to a temperature between about 30° C. to about 50° C.; heating a reducing agent solution that includes a reducing agent, an N,N-dialkylethylenediamine, and a C6-C18 alkylamine in an organic solvent to a temperature between about 30° C. to about 50° C.; and adding the heated copper salt solution to the heated reducing agent solution, thereby producing copper nanoparticles. A composition includes copper nanoparticles, a C6-C18 alkylamine and an N,N?-dialkylethylenediamine ligand. Such copper nanoparticles in this composition have a fusion temperature between about 100° C. to about 200° C. A surfactant system for the stabilizing copper nanoparticles includes an N,N?-dialkylethylenediamine and a C6-C18 alkylamine.Type: GrantFiled: June 10, 2010Date of Patent: July 16, 2013Assignee: Lockheed Martin CorporationInventors: Alfred A. Zinn, Paul P. Lu