Patents Assigned to Lockheed Martin
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Patent number: 10896482Abstract: The disclosure is directed to systems and methods for image capturing technologies and, more particularly, to a slice scan imaging system and respective processes to achieve high quality images. The method can be implemented in a computing device, which includes: capturing multiple lines of an image in a single slice; capturing multiple slices; stitching together the multiple slices by aligning common features of the images of a previous slice with a successive slice; and blending together the stitched together multiple slices.Type: GrantFiled: March 16, 2018Date of Patent: January 19, 2021Assignee: Lockheed Martin CorporationInventors: Alexander M. Elhage, Michael Riess
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Patent number: 10889067Abstract: A manufacturing system includes a tension-wound system having a feedstock system and a shape fixture. The tension-wound system is configured to feed a feedstock from the feedstock system and to wind the feedstock under tension in successive layers around the shape fixture to allow the feedstock to form a component having a shape represented by the shape fixture. The manufacturing system includes a solid-state joining tool configured to additively join the successive layers of the feedstock. In a spiral tension-winding process, with a continuously-fed strip of aluminum feedstock around a piece of tooling, the feedstock can be friction stir welded and additively joined in successive layers to produce a large, near-net structure.Type: GrantFiled: April 11, 2016Date of Patent: January 12, 2021Assignee: LOCKHEED MARTIN CORPORATIONInventors: Michael R. Eller, Randy J. Brown
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Patent number: 10892724Abstract: A distributed power amplifier includes radio frequency (RF) input and output terminals. A first field effect transistor (FET) is coupled at a first gate terminal to the RF input terminal and at a first drain terminal to the RF output terminal. The first FET has a first periphery and a first source terminal electrically connected to ground potential. A second FET has a second periphery smaller than the first periphery. The second FET has a second gate terminal electrically coupled to the first gate terminal through a first inductor, a second drain terminal electrically coupled to the first drain terminal through a second inductor, and a second source terminal electrically connected to the ground potential. A drain voltage terminal, which excludes a resistive element, is electrically coupled to a drain bias network through which a drain bias voltage is applied to the first drain terminal and the second drain terminal.Type: GrantFiled: January 29, 2019Date of Patent: January 12, 2021Assignee: Lockheed Martin CorporationInventor: Roland Cadotte, Jr.
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Patent number: 10884525Abstract: A system comprising a device including a chromakeyed tactile touch-sensitive surface (TTSS) and touch-sensitive input (TSI) circuit to sense touch applied to the TTSS by a hand. A processor registers a location of a chromakey mask, the device, and a virtual portal location within a virtual reality (VR) scene including virtual pixels of virtual user-interactive simulator (VUIS) controls. The processor detects and isolates, within the mask, first pixels having a non-chromakey color overlapping the chromakey mask and second pixels matching a color of the chromakey mask. The first pixels are preserved to form a pass-through image. A composite mixed reality scene is formed with the VR scene and preserved pixels registered to the VR scene. Those VUIS controls corresponding to the preserved pixels are omitted from the VR scene and remaining virtual pixels of the VUIS controls overlap and link to the TSI circuit.Type: GrantFiled: April 23, 2019Date of Patent: January 5, 2021Assignee: LOCKHEED MARTIN CORPORATIONInventors: Brett A. Vonsik, Howell B. Hollis, Brittany V. Henthorn, Joshua D. Kitain, Shawn M. Muir
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Patent number: 10885664Abstract: A method of monitoring a location of a component of an aircraft includes acquiring an image of the component during flight by an imaging device disposed at a selected location relative to the aircraft and oriented along a selected direction relative to an aircraft structure, identifying a position of the component within the image, estimating a distance in the image between the component and a reference location depicted in the image, and estimating an actual location of the component based on the distance in the image. Estimating the actual location includes correlating the distance in the image with an actual distance between the component and the reference location.Type: GrantFiled: September 27, 2019Date of Patent: January 5, 2021Assignee: LOCKHEED MARTIN CORPORATIONInventor: Timothy Schmidt
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Patent number: 10886453Abstract: System for storing and using energy quantum mechanically includes an electronic device that produces heat while operating. A quantum heat engine can be in thermal contact with and electrically connected to the electronic device. The heat produced by the electronic device can dissipate to the quantum heat engine. The quantum heat engine can induce a current to bias the electronic device. Methods for storing and using memory resource to convert heat into electrical work, coherence capacitors, methods for quantum energy storage, and quantum heat engines, are also disclosed.Type: GrantFiled: April 3, 2017Date of Patent: January 5, 2021Assignees: Lockheed Martin Corporation, Sabanci UniversityInventors: Edward Henry Allen, Inanc Adagideli, Anthony W. Jacomb-Hood
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Patent number: 10883830Abstract: A system can include an inertial measurement unit, a magnetometer configured to measure a magnetic field, and a processing system having an ORSE filter. The processing system can be configured to determine an estimated position based on a change in velocity or angular rate based on data received from the inertial measurement unit, determine a difference between the measured magnetic field from the magnetometer and the expected magnetic field measurement, and determine a state estimate using the ORSE filter by updating a time propagation of state and covariance with a measurement update of the state and covariance. The processing system can be configured to transform a change in velocity, a change in angulate rate, and the measured magnetic field to an Earth-centered inertial reference frame for the ORSE filter.Type: GrantFiled: January 15, 2019Date of Patent: January 5, 2021Assignee: LOCKHEED MARTIN CORPORATIONInventor: Jeffrey B. Boka
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Patent number: 10866413Abstract: In one embodiment, an electronic assembly includes a flexible circuit board formed into a curved shape that is configured to be substantially concentric with a viewer's eye. The electronic assembly further includes a plurality of facets coupled to a side of curved shape of the flexible circuit board that is configured to face the viewer's eye. Each facet has a planar face, one or more emitters configured to emit light towards the viewer's eye, and one or more receptors configured to detect the emitted light after it has been reflected back towards the electronic assembly from a retina of the viewer's eye. Each face is normal to a line pointing towards a center area of the viewer's eye when the curved shape is substantially concentric with the viewer's eye. Each facet is individually addressable such that the plurality of facets are configurable to detect a center of gaze of the viewer.Type: GrantFiled: December 3, 2018Date of Patent: December 15, 2020Assignee: Lockheed Martin CorporationInventors: Mark A. Lamkin, Kyle Martin Ringgenberg, Jordan David Lamkin
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Patent number: 10865112Abstract: Modified substrates are provided having nano- or microscale wells, tracks, channels, pores or perforations. Also provided are methods of making the same.Type: GrantFiled: December 13, 2018Date of Patent: December 15, 2020Assignee: Lockheed Martin CorporationInventors: Scott E. Heise, Han Liu, Jacob L. Swett, Michael J. Hiltabidle
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Patent number: 10858096Abstract: A rotor blade assembly of an aircraft. The rotor blade assembly includes a blade attachment assembly rotatable with respect to a rotor hub assembly of the aircraft about a blade fold axis, and a pitch control assembly. The pitch control assembly includes a horn mount attachable to the rotor hub assembly, and a teeter bar hingedly attached to the horn mount at an interface, the interface defining a pitch control fold axis. The pitch control assembly is foldable about the pitch control fold axis when the pitch control fold axis is aligned with the blade fold axis.Type: GrantFiled: May 29, 2019Date of Patent: December 8, 2020Assignee: LOCKHEED MARTIN CORPORATIONInventors: David N. Schmaling, David H. Hunter, Andrew C. Goodwin
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Patent number: 10848238Abstract: A communication device includes a session and mobility management block configured to interface with a mobility management entity (MME) of an evolved packet core (EPC) of an evolved packet system (EPS). An access non-LTE air interface circuit is configured to communicate with an access network gateway. An EPS inter-working functional block including mapping and coordination logic is configured to map and coordinate a plurality of functionalities associated with the access non-LTE air interface circuit into corresponding functionalities associated with the session and mobility management block.Type: GrantFiled: December 18, 2017Date of Patent: November 24, 2020Assignee: Lockheed Martin CorporationInventors: Suresh K. Iyer, Dilip S. Gokhale
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Patent number: 10838250Abstract: In one embodiment, an electronic display assembly includes a circuit board, a first microlens layer on a first side of the circuit board, and a second microlens layer on an opposite side of the circuit board from the first microlens layer. The first microlens layer includes a first plurality of microlenses, and the second microlens layer includes a second plurality of microlenses. The electronic display assembly further includes an image sensor layer adjacent to the first microlens layer and a display layer adjacent to the second microlens array. The image sensor layer includes sensor pixels for detecting incoming light through the first microlenses, and the display layer includes display pixels for emitting light through the second microlenses. The electronic display assembly emulates transparency by emitting light from the second microlenses at angles that correspond to angles of the incoming light detected through the first microlenses.Type: GrantFiled: February 7, 2018Date of Patent: November 17, 2020Assignee: Lockheed Martin CorporationInventors: Mark A. Lamkin, Kyle Martin Ringgenberg, Jordan David Lamkin
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Patent number: 10838057Abstract: A Doppler radar system includes a Doppler radar processor, a memory in communication with radar processor and a transmit/receive controller. The memory includes computer readable instructions that cause the Doppler radar processor to transmit a radar signal toward the airborne object at a frequency; receive reflected radar signals off of the airborne object, including frequencies produced as a result of Doppler effect due to relative motion between features of the airborne object and the radar system; and Fourier transform the received signals into the frequency domain. Peak frequencies and their harmonic frequency families are sorted and identified. The logarithm of the Fourier transform is calculated to generate a quefrency cepstrum. To identify features producing cyclic, periodic Doppler frequency patterns, peak quefrencies and rahmonic families associated with a quefrency peak are sorted and identified. The rotational state of the airborne object based on the identified quefrency families is determined.Type: GrantFiled: October 16, 2017Date of Patent: November 17, 2020Assignee: Lockheed Martin CorporationInventors: Tod M. Schuck, David B. Reese, Mark A. Friesel
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Patent number: 10838021Abstract: The present disclosure relates to apparatuses and methods to utilize techniques to simultaneously measure Ramsey pulses on a plurality of axes of the magneto-optical defect center material with defect centers. When measuring simultaneously, there is potentially no relative sensitivity loss relative to scalar measurements. Therefore, Ramsey pulses on a plurality of axes of a magneto-optical defect material with defect centers are measured while bypassing the sensitivity loss incurred with sequential measurement techniques. The axes are interrogated simultaneously while allowing for isolation of the individual responses from the signal detected from the magneto-optical defect center material. In some embodiments, the system utilizes a special Ramsey pulse sequence pair or a ‘shifted magnetometry adapted cancellation’ (SMAC) pair to detect and measure the magnetic field acting on the system.Type: GrantFiled: July 10, 2018Date of Patent: November 17, 2020Assignee: LOCKHEED MARTIN CORPORATIONInventors: Arul Manickam, Peter G. Kaup, Jon C. Russo
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Patent number: 10833347Abstract: Parasitic reactions, such as production of hydrogen and oxidation by oxygen, can occur under the operating conditions of flow batteries and other electrochemical systems. Such parasitic reactions can undesirably impact operating performance by altering the pH and/or state of charge of one or both electrolyte solutions in a flow battery. Electrochemical balancing cells can allow rebalancing of electrolyte solutions to take place. Electrochemical balancing cells suitable for placement in fluid communication with both electrolyte solutions of a flow battery can include: a first chamber containing a first electrode, a second chamber containing a second electrode, a third chamber disposed between the first chamber and the second chamber, an ion-selective membrane forming a first interface between the first chamber and the third chamber, and a bipolar membrane forming a second interface between the second chamber and the third chamber.Type: GrantFiled: July 11, 2019Date of Patent: November 10, 2020Assignee: Lockheed Martin Energy, LLCInventors: Steven Y. Reece, John Goeltz, Joseph Johannes Henricus Pijpers, Paravastu Badrinarayanan
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Patent number: 10833340Abstract: The present invention relates to methods and apparatuses for determining the ratio of oxidized and reduced forms of a redox couple in solution, each method comprising: (a) contacting a first stationary working electrode and a first counter electrode to the solution; (b) applying a first potential at the first working electrode and measuring a first constant current; (c) applying a second potential at the first working electrode and measuring a second constant current; wherein the sign of the first and second currents are not the same; and wherein the ratio of the absolute values of the first and second currents reflects the ratio of the oxidized and reduced forms of the redox couple in solution.Type: GrantFiled: October 31, 2014Date of Patent: November 10, 2020Assignee: Lockheed Martin Energy, LLCInventors: Evan R. King, Kean Duffey, Adam Morris-Cohen, John Goeltz, Steven Y. Reece
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Patent number: 10833900Abstract: A receiver signal is sampled at a sampling rate equivalent to a chip rate at which chips of a known signal are timed. The resulting receiver signal samples are segmented into receiver signal segments, which are filtered by respective matched filters that are matched to known signal segments segmented from the known signal. Indexes are assigned to elements of the resulting filter response sequences to define an array thereof. Frequency transforms are computed of elements of the filter response sequences in respective columns of the array. Indexes are assigned to elements of the resulting frequency response sequences to define another array thereof. Channel effects imparted on a radio signal are jointly estimated from characteristics of the other array at which at least one local maximum is located.Type: GrantFiled: December 17, 2019Date of Patent: November 10, 2020Assignee: Lockheed Martin CorporationInventors: Liang C. Chu, John Robert Barry, Derrick A. Chu
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Patent number: 10822110Abstract: Some embodiments include a countermeasure assistance system that, in response to detecting a threat to an aircraft, calculates and presents via a user interface an instruction to assist a pilot in evading the threat. For example, the system may determine a direction to which the aircraft should be turned to present a beam of the aircraft toward the threat, which may assist in evading a radar-enabled threat. The system may calculate a shortest turn to present the beam to the threat. The system may additionally display information regarding a position, nature, and degree of the threat, including through formatting of at least a portion of a user interface for displaying information regarding the threat. The system may additionally calculate and display an intervisibility zone for the threat and for the aircraft's current position to further assist the pilot in navigating to an area at which the threat may be evaded.Type: GrantFiled: September 8, 2016Date of Patent: November 3, 2020Assignee: Lockheed Martin CorporationInventor: Steven D. Colby
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Patent number: 10827608Abstract: A method for making conformal non-planar multi-layer circuitry is described. The method can include providing a substrate having a non-planar surface and depositing a first conformal dielectric layer on the substrate, the first conformal dielectric layer conforming to the non-planar surface of the substrate and having a non-planar surface. The method can also include applying a first conformal circuitry layer on the first conformal dielectric layer. The method can include depositing a second conformal dielectric layer on the first conformal circuitry layer, the second conformal dielectric layer conforming to a non-planar surface of the first conformal circuitry layer, and applying a second conformal circuitry layer on the second conformal dielectric layer. Successive layers can be sequentially deposited.Type: GrantFiled: March 12, 2019Date of Patent: November 3, 2020Assignee: Lockheed Martin CorporationInventors: Stephen Gonya, Kenn Twigg, Jim Patterson
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Patent number: 10819041Abstract: An antenna system includes an antenna array including a number of antenna elements disposed on a substrate. Each antenna element includes a radiation layer, a ground plane layer, a feed layer and an additional ground plane layer. The ground plane layer includes a ground plane conductive layer that has a number of slots. The feed layer includes a feed structure to excite the slots. A dual polarization feature of the antenna array is realized via the slots, and the slots are separated by the ground plane conductive layer.Type: GrantFiled: August 3, 2018Date of Patent: October 27, 2020Assignee: Lockheed Martin CorporationInventors: Andrew Jason Kee, Arun Kumar Bhattacharyya