Abstract: A thermal management system includes at least one vapor compression system (VCS) that is configured to cool portions of the vehicle. The VCS circulates a fluid therethrough to cool the portions of the vehicle through heat exchange. At least one reverse air cycle machine (RACM) couples to VCS through a first heat exchanger. The RACM is configured to receive ram air. The RACM expands the ram air. Heat from the fluid circulating through the VCS is transferred to the expanded ram air through the first heat exchanger.

Abstract: A thermal management system includes at least one vapor control system (VCS) that is configured to cool portions of the vehicle. The VCS circulates a fluid therethrough to cool the portions of the vehicle through heat exchange. At least one reverse air control machine (RACM) couples to VCS through a first heat exchanger. The RACM is configured to receive ram air. The RACM expands the ram air. Heat from the fluid circulating through the VCS is transferred to the expanded ram air through the first heat exchanger.

Abstract: A method and apparatus comprising a view generator. The view generator is configured to identify a position of a mobile display device relative to an exterior of a vehicle. The view generator is further configured to identify image data from a sensor system for the vehicle that corresponds to a field of view of the mobile display device from the position of the mobile display device relative to the vehicle. The view generator is further configured to display an external view for the vehicle on the mobile display device using the image data.

Abstract: Systems and methods for detection of clear air turbulence are provided. One system includes an image capture device suitable to capture one or more images of an optical phenomenon caused by non-horizontally oriented ice crystals. The system also includes a computer processor configured to receive the one or more images from the image capture device, analyze the one or more images by comparing one or more characteristics of the one or more images to one or more threshold values, and determine based on the comparing, an occurrence of clear air turbulence.

Abstract: A Marman clamp is disclosed. The Marman clamp includes a release mechanism with either pins or tubes formed with a shape memory alloy. The release mechanism opens and closes the clamp depending on the temperature of the pins or tubes. The temperature of the pins or tubes may be based on whether a space vehicle including the clamp is in a direct line of sight of radiation from the sun. Alternatively, a heat source may control the temperature of the pins or tubes. The Marman clamp may also open and close as a result of an independent force applied to the release mechanism.

Abstract: An upper joint of a wing assembly of an aircraft includes an outboard upper wing panel, a center upper wing panel, a rib, and an upper joint assembly operatively interconnecting the outboard upper wing panel, the center upper wing panel, and the rib. For a substantial fore/aft span of the upper joint, a first subset of a plurality of center upper stringers is operatively coupled to the upper joint assembly, and a second subset of the plurality of center upper stringers terminates without being directly coupled to the upper joint assembly.

Abstract: Apparatuses include first and second monolithic members that are coupled together, that are configured to move relative to each other, and that are configured so that they cannot be decoupled from each other without destruction of one or both of the two monolithic members. Apparatuses further include a third monolithic member configured to be selectively coupled to at least one of the first monolithic member and the second monolithic member. Methods of forming and using such apparatuses also are disclosed. Some monolithic members are formed utilizing an additive manufacturing process so that they are restricted from being decoupled from each other. Some apparatuses define clamps. Some clamps are used to precisely align laser projection alignment targets for use with laser projection alignment systems.

Abstract: In one aspect, methods of making a carbon coating are described herein. In some implementations, a method of making a carbon coating comprises applying a first adhesive material to a substrate surface to provide an adhesive surface; rolling a carbon source over the adhesive surface to provide a carbon layer on the adhesive surface; and rolling an adhesive roller over the carbon layer to remove some but not all of the carbon of the carbon layer to provide the carbon coating.

Abstract: Techniques are disclosed for systems and methods to provide a magnetic materials additive manufacturing system (MMAMS) configured to form compact magnetic structures and/or devices. A MMAMS includes a controller and one or more dispensers configured to dispense magnetic material matrix in a high resolution pattern in order to form the compact magnetic structures and/or devices. The MMAMS receives a magnetic device design including a magnetic structure to be formed from a magnetic material matrix, where the magnetic material matrix is configured to be used in the MMAMS. The MMAMS receives magnetic material matrix and dispenses the magnetic material matrix to form the magnetic structure.

Abstract: A method, apparatus, and computer program product for identifying air data for an aircraft. The lift for the aircraft is identified. The number of surface positions for the aircraft is identified. The angle of attack during flight of the aircraft is identified. A synthetic dynamic pressure is computed from the lift, the number of surface positions, and the angle of attack.

Abstract: A method for locating an interferer is provided. The method includes determining, from one of a time difference of arrival (TDOA) signature and a frequency difference of arrival (FDOA) signature between a first signal received at a satellite at a first location and a second signal received at the same satellite at a second location, a first curve on which the interferer lies, determining, from direction of arrival information generated using signals received from the interferer at a plurality of elements of a linear array on the satellite, a second curve on which the interferer lies, and determining, based on an intersection between the first and second curves, the location of the interferer.

Abstract: A method for registering existing vector data associated with a first image of a location to a second image of the location is provided. Typically the images are separated by an increment of time. The method is implemented by at least one computing device including at least one processor in communication with a memory. The method includes receiving, by the at least one computing device, the existing vector data associated with the first image of the location, receiving, by the at least one computing device, a plurality of controls for registering the first image to the second image, applying, by the at least one computing device, the plurality of controls to the existing vector data to generate updated vector data, and storing, in the memory, the updated vector data associated with the second image.

Abstract: Described herein is a composite panel that includes a first layer made from an electrically non-conductive material. The composite panel also includes a resistance heater printed onto the first layer. Further, the composite panel includes a second layer adjacent the resistance heater, the resistance heater being positioned between the first layer and the second layer. The second layer is made from an electrically non-conductive material.

Abstract: A method and apparatus for assisting movement of a bin into a closed position. An assistance system associated with the bin may be activated in response to a manipulation of a switch associated with the bin. The assistance system may comprise a biasing system and a switch. The biasing system may be configured to generate a force in a direction towards a closed position for the bin. A switch may be connected to the biasing system and configured to activate the biasing system when a selected amount of weight is present in the bin. The force in the direction towards the closed position for the bin may be generated in response to activating the assistance system.

Abstract: Systems and methods provide sloped landing exceedance warning and avoidance. One system includes a surface slope determination system configured to measure a plurality of distances between an aircraft and a surface. The system also includes an inertial navigation system configured to sense aircraft attitude information. A flight control system is communicatively coupled to the surface slope determination system and the inertial navigation system. The flight control system is configured to estimate a slope angle of the surface. The flight control system is also configured to determine one or more approach characteristics based on the slope angle and the aircraft attitude information. The flight control system is additionally configured to identify a warning condition and perform one or more avoidance measures when one or more of the approach characteristics exceeds a predetermined threshold. A pilot cuing device also generates a notification when the warning condition is identified.

Abstract: A system is provided for panoptic visualization of a 3D representation of a complex system. The system includes a visualization engine configured to receive a digital 3D model of a complex system and produce a plurality of electronic document components including 2D images depicting elements of the complex system. The system also includes a data extractor configured to generate 2D derivatives of the 3D model, and communicate the 2D derivatives for inclusion in a panoptic visualization document collection. The data extractor may be configured to receive a document component including a 2D image depicting an element of the complex system, and extract from the 3D model, information identifying a spatial, design or functional relationship between the respective element and one or more other elements of the complex system. The data extractor may then be configured to provide the extracted information in metadata associated with the document component.

Abstract: Disclosed is a multi-port power amplifier (“MPA”) having an input hybrid matrix (“IHM”), an output hybrid matrix (“OHM”), and a plurality of high-power amplifier (“HPA”) chains. The MPA may include a plurality of adjustable delay modules (“ADMs”) in signal communication with the IHM and the plurality of HPA chains. Each adjustable delay module (“ADM”) of the plurality of ADMs may be in signal communication with the IHM and a corresponding HPA chain of the plurality of HPA chains.

Abstract: An airfoil, a flap mechanism and an associated method are provided to controllably actuate a flap positioned proximate the trailing edge of an airfoil body. The flap mechanism includes a carrier beam hingedly connected to an airfoil body and also pivotally connected to a flap proximate the trailing edge of the airfoil body. The flap mechanism further includes an actuator, a first plurality of links and a second plurality of links. The first plurality of links is operably connected to the airfoil body, the actuator and the carrier beam. The first plurality of links causes the carrier beam to be rotated with respect to the airfoil body in response to actuation by the actuator. The second plurality of links is responsive to rotation of the carrier beam with respect to the airfoil body. The second plurality of links causes the flap to be rotated with respect to the carrier beam.

Abstract: A method of fabricating a composite assembly may include providing a first laminate and a second laminate respectively formed of first and second composite plies, and having a respective first and second cured section and a respective first and second uncured section. The method may further include interleaving the first composite plies in the first uncured section with the second composite plies in the second uncured section to form an interfacial region. The method may additionally include curing the interfacial region to join the first laminate to the second laminate and form a unitized composite assembly.

Abstract: Systems and methods are provided for controlling flexible tracks. One embodiment is a system for conveying plies of laminate to a forming device. The system includes a flexible track assembly comprising a first portion of track and a second portion of track, each of the portions defining a groove dimensioned to receive a slider that transports a ply, the second portion arranged to transport the ply into the forming device. The track assembly also includes a guide in which ends of the portions are disposed. The system further includes a retraction line that applies a contracting force that biases the end of the second portion towards contact with the end of the first portion, the retraction line being extendable to enable the second portion to separate from the first portion, thereby accommodating extension of the track assembly in response to forces applied by the forming device during forming.