Abstract: A method for curing a resin includes the steps of placing the resin into a reaction vessel, drawing a vacuum in the reaction vessel, positioning the reaction vessel in a gaseous coupling fluid, and applying ultrasonic energy to the coupling fluid.

Abstract: A method for connecting a wing. A frame for a wing may be positioned relative to a fuselage of an aircraft. The frame may have bays and comprise a front spar, a rear spar, and a number of spars located between the front and rear spars. A first number of skin panels may be on a first side of the frame, and a second number of skin panels may be on a second side of the frame. The first side may be opposite to the second side. Openings may be in the first and second numbers of skin panels. The openings may be in locations such that each bay has an opening and such that the openings may alternate between the first side and the second side between adjacent bays in the bays. The frame may be attached to the fuselage using the openings to access an interior of the frame.

Abstract: A method and apparatus for controlling an air motor. Speed information is received for an operation using an apparatus comprising the air motor having an inlet and an exhaust, and a valve comprising a body with a first port, a second port, and a third port. The first port is connected to the air motor, the second port is configured for connection to an air supply, and the third port is configured to vent air out of the body. A first flow of air is controlled in the body between the first port and the second port and a second flow of air is controlled out of the body through the third port to control a speed of the operation.

Abstract: Two panel-sized fully populated printed wiring board assemblies formed together, with an anisotropic epoxy that provides electrical connection for RF signals and DC supplies without the need for wirebonds, mechanical interconnects or solder balls.

Abstract: An in-flight refueling method may include deploying a fueling hose from a refueling aircraft. The fueling hose may have a drogue. The deployment of the fueling hose may include extending the drogue using a telescoping arm having a ring. The deployment of the fueling hose may also include passing the fueling hose through the ring to deploy the fueling hose. The in-flight refueling method may further include retrieving the fueling hose by drawing the drogue into a wire pitch mounted on the ring and collapsing the drogue in response to drawing the drogue into the wire pitch.

Abstract: A forming tool and method for its use with flat pre-preg composite laminate assemblies which incorporates a mandrel segmented into multiple forming blocks, the forming blocks sized to receive a draped composite laminate assembly with all portions of the composite laminate assembly spaced from a shaping surface on each block. A spline plate engages the shaping surface of the forming blocks to provide a neutral axis for maintaining the entire composite laminate assembly in tension during forming. In the exemplary embodiments, the draped composite laminate assembly is formed to the forming blocks from the flat composite laminate assembly and maintained in contact with the forming blocks using a vacuum bag. The mandrel forming blocks are then displaced to a desired curvature on the spline plate.

Abstract: According to an embodiment, a numerically controlled (NC) processing system includes materials processing installation having a multi-axis kinematic linkage operable to position a tip portion of the linkage along a predetermined process path. The system also includes a processor having a compensation system operable to detect a singular point in the process path and to improve the accuracy tip portion positioning near the singular point.

Abstract: An aircraft system may include an airfoil and a deployable device coupled to the airfoil. The system may further include a shape memory alloy actuator coupled between the airfoil and the deployable device. The actuator may be movable between a first position with the deployable device deployed relative to the airfoil, and a second position with the deployable device stowed relative to the airfoil. The system may additionally include an activatable link positioned between the actuator and the deployable device. The link may have an engaged configuration in which motion of the actuator is transmitted to the deployable device, and a disengaged configuration in which motion of the actuator is not transmitted to the deployable device.

Abstract: A computer-based method for determining a probability that no path exists from a specified starting node to a specified target node within a network of nodes and directional links between pairs of nodes is described. The nodes and directional links form paths of a reliability graph and the method is performed using a computer coupled to a database that includes data relating to the nodes and the directional links The method includes selecting a set of paths, from the set of all paths, between the starting node and the target node that have been determined to be reliable, calculating a reliability of the union of the selected path sets, setting an upper bound for the unreliability of the set of all paths, based on the calculated reliability, selecting a set of minimal cutsets from all such cutsets that lie between the starting node and the target node, calculating the probability of the union of the minimal cutsets, and setting a lower bound for the unreliability of the set of all cutsets.

Abstract: Methods and apparatuses for displaying and receiving tactical and strategic flight guidance information are disclosed. A method in accordance with one aspect of the invention includes displaying at least one first indicator to an operator of the aircraft, with a first indicator corresponding to a first instruction input by the operator for directing a first aircraft behavior and implemented upon receiving an activation instruction from the operator. At least one second indicator corresponding to a second instruction for directing a second aircraft behavior at least proximately the same as the first aircraft behavior is displayed, with the at least one second instruction to be automatically implemented at a future time. The at least one second indicator is at least approximately the same as the at least one first indicator. Indicators can be hierarchically organized to simplify presentation and reduce pilot training time.

Abstract: A computer implemented method, apparatus, and computer program product for planning in a manufacturing process. In one embodiment, a library of standard manufacturing processes is created. The library comprises a plurality of master process objects. In response to generating a manufacturing project, a set of master process objects is selected from the plurality of master process objects in the library. The set of master process objects is associated with the manufacturing project to create a set of process usage objects within the manufacturing project. The set of master process objects in the library of standard manufacturing processes are linked to the manufacturing project without copying the set of master process objects into the manufacturing project. The set of usage process objects in the manufacturing project is populated with information specific to the manufacturing project.

Abstract: The different advantageous embodiments provide an apparatus comprising a number of tires for a vehicle, a number of systems, and a number of processor units. The number of systems is configured to generate data about the number of tires and the vehicle. The number of processor units is configured to monitor the data and manage the health of the number of tires.

Abstract: The different advantageous embodiments provide an apparatus comprising a number of landing gear components for a vehicle, a number of systems, and a number of processor units. The number of systems is configured to generate data about the number of landing gear components and the vehicle. The number of processor units is configured to monitor the data and manage health of the number of landing gear components.

Abstract: A non-pneumatic tire and wheel assembly incorporates a tire tread and a conventional vehicle wheel with an elastomer tire body element molded for engagement intermediate the tread and wheel. The tire body element includes multiple concentric layers with alternating spokes. A bonded multilayer cover may be employed which is received within a recess in an outer surface of the tire body element from the tire tread. A mounting plate is engaged to the cover and attached to the wheel.

Abstract: A non-pneumatic tire and wheel assembly incorporates a tire tread and a conventional vehicle wheel with an elastomer tire body element and integral wall elements extending radially inward from the tire body element for sealing engagement with the wheel. The tire body element includes multiple concentric layers with alternating spokes. A bonded multilayer cover may be employed which is received within a recess in an outer surface of the tire body element from the tire tread. An attachment plate is engaged to the cover and attached to the wheel.

Abstract: Apparatus, systems and methods for electronic device protection are provided. A particular apparatus includes a non-conductive substrate and a plurality of cells including conductive members coupled to the non-conductive substrate. The conductive members are arranged to form a first discontinuous mesh, where each conductive member of a cell is separated from conductive members of adjacent cells by a gap and a cavity is defined in the non-conductive substrate at a location of each gap.

Abstract: A system for supporting a load across non-intersecting beams each having a web depending from an upper chord with an upper surface generally parallel with a chordal plane includes at least one crossing member intersecting the beams at intersection loci. At each intersection locus the beam presents a channel receiving a crossing member in a nesting orientation in an installed orientation. The crossing member includes a support expanse configured for an abutting relation with the upper chord to present the upper surface and a top surface of the crossing member as coplanar in the installed orientation. The beam and the crossing member have aperture-pairs in register in the installed orientation. The apertures accommodate tension resisting members or compression resisting members coupled with the upper chord and traversing the crossing member for resisting tension or compression forces on the upper chord in the installed orientation.

Abstract: An apparatus comprises a sensor system, a flexible line, and a sensor. The sensor system is capable of detecting skew in at least some of a plurality of control surfaces for a vehicle. The flexible line extends across a number of interfaces for a portion of the plurality of control surfaces. The sensor is connected to the flexible line and is capable of detecting the skew in the portion of the plurality of control surfaces in response to a selected amount of movement of the flexible line.

Abstract: A data collection system for a vehicle is provided. The data collection system includes a first data collection node configured to obtain data from a vehicle subsystem, and a processor communicatively coupled to the data collection node via a wiring system, wherein the wiring system includes a plurality of conductors and an overbraid surrounding said plurality of conductors, said overbraid comprising at least one fiber optic cable integrally woven therein and configured for the transmission of data related to an operational status of the vehicle subsystem.

Abstract: The disclosure provides for a friction stir welding tool cleaning method and apparatus for fixed and retractable pin tools. The method and apparatus use a heating component, a temperature indicator component, a controller component, and a rotatable tool cleaner component for cleaning fixed pin tools. An additional bore cleaner component is used for cleaning retractable pin tools. Heat is applied to a friction stir welding tool having a surface with weld process residue material until the process residue material is sufficiently plasticized, and then the tool cleaner component is applied to the heated tool to remove the plasticized residue on the pin and shoulder surfaces of the tool, and for retractable pin tools, the bore cleaner component is applied to the heated tool to remove the plasticized residue in the tool bore.