Abstract: A support unit for moving an object may include an elongated member, at least one suction device coupled to the elongated member for attaching to an object, a lifting mechanism for raising and lowering the elongated member and an attached object, and a rotating member for moving the support unit and the attached object from a departure location to a destination location.

Abstract: A multiple nested interferometric fiber optic gyroscope system having varying functions may include a first fiber optic coil, a second fiber optic coil which is smaller than the first fiber optical coil and nested within and transversely to the first fiber optic coil, and a third fiber optic coil which is smaller than the second fiber optical coil and nested within and transversely to the second fiber optic coil.

Abstract: Methods, systems, and apparatus, including computer program products, for determining a probability that a traffic conversion of a content item associated with a content source (e.g., website) will occur based on past traffic patterns for that content source. A traffic conversion defines, for example, minimum traffic interactions of one or more associated user sessions with a content source. The minimum traffic interactions can be based on, for example, the duration of the one or more user sessions on the content source, or a quantity of pages associated with the content source navigated in the one or more associated user sessions.

Abstract: An adapter for connecting a ring guide and rod with a holder for a radiation sensing device is provided herein. The adapter includes but is not limited to a first engagement member for engaging a complementary engagement member formed on the rod and a second engagement member for engaging a holder for a radiation sensing device. The adapter also includes but is not limited to a handle connecting the first engagement member to the second engagement member.

Abstract: Apparatus for cutting plural aligned ply strips includes plural knife blades disposed in a spaced manner such that each knife blade is aligned with and in closely spaced relation to an associated ply strip. The knife blades are pivotally mounted in a common housing and are coupled to a single rotational drive for allowing each knife blade to assume the same predetermined cutting angle relative to its associated ply strip, where the cutting angle may be varied between ±45°. The plural knife blades are coupled to a rotational drive by means of plural circular drive gears and are connected to a linear drive for displacing the knife blades into contact with the ply strips for cutting the strips at the predetermined angle. The severed edges of the aligned ply strips are formed in mutual linear alignment and do not include projecting triangular patterns, or crenelations.

Abstract: A method of determining environmental data along a trajectory of an aircraft may assist in the evaluation of flight conditions along the trajectory. Environmental data may be at least one of collected, derived, and fused from a plurality of weather sources using at least one processor. The environmental data may be filtered, extrapolated, and fused, using the at least one processor, within at least one selected volume of airspace over a trajectory of the aircraft based on selected weather-applicability time intervals, and on at least one of user-selected parameters and weighted environmental data criteria. The trajectory may comprise at least one of a planned trajectory, a current trajectory, and an intent trajectory of the aircraft. An effect of the filtered, extrapolated, and fused environmental data on the trajectory may be determined using the at least one processor.

Abstract: A removable, modular, cargo deck trailer system may include different types of modular, interchangeable, removable deck units which are configured to be removably and interchangeably attached to a trailer. The different types of modular, interchangeable, removable deck units may collectively include a plurality of moving apparatus for moving cargo in a lengthwise direction relative to the deck units, for moving cargo in a vertical direction relative to the deck units, and for moving cargo in at least one of a widthwise direction relative to the deck units, and in a rotating direction relative to the deck units.

Abstract: The present invention relates to voice-activated vehicle control, and to the control of UAVs (unmanned air vehicles) using speech in particular. A method of controlling a vehicle is provided that includes receiving one or more instructions issued as speech and analyzing the speech using speech recognition software to provide a sequence of words and a word confidence measure for each word so recognized. The sequence of words is analyzed to identify a semantic concept corresponding to an instruction based on the analysis, and a semantic confidence level for the semantic concept identified derived at least in part with reference to the word confidence measures of the words associated with the semantic concept. A spoken confirmation of the semantic concept so identified based on the semantic confidence level is provided, and the semantic concept is used to provide a control input for the vehicle.

Abstract: An apparatus for single-side, thermal shock testing of a specimen may comprise a base and thermal insulation. The base may comprise an internal cavity disposed within the base. The internal cavity may extend through a first outer surface of the base. A specimen-supporting surface may be recessed within the first outer surface for supporting a specimen within the base to substantially close the internal cavity. The thermal insulation may not substantially cover the first outer surface, but may substantially cover other outer surfaces of the base.

Abstract: A ballistic resistant through insert with floating capability for stopping a ballistic projectile, comprising at least one of a bullet, a ballistic fragment, and a particle fragment, may comprise a stud, a floating nut, and a cap. The stud may have a flat base portion and a cylindrical stud portion mounted thereon. The cylindrical stud portion may comprise a stud cylinder aperture. The floating nut may be located inside the stud cylinder aperture such that the floating nut floats within the stud cylinder aperture. The cap may have a flat cap portion and a cylindrical cap portion mounted thereon. The cylindrical cap portion may mate with the cylindrical stud portion. The stud may be made of a material for stopping a ballistic projectile. The flat base portion of the stud may have a minimum thickness for stopping a ballistic projectile.

Abstract: A system for automatically detecting corona effects in operating dynamic electromechanical equipment may include: at least one sensor connected to operating dynamic electromechanical equipment, a controller connected to the at least one sensor and to the operating dynamic electromechanical equipment; and a corona phenomena detection device. The at least one sensor may be adapted to measure behavior of emitted signals of the operating dynamic electromechanical equipment. The controller may be adapted to adjust emitted signals of the operating dynamic electromechanical equipment to correct for errors detected by the sensor in the emitted signals The corona phenomena detection device may be adapted to automatically detect corona effects of the dynamic electromechanical equipment.

Abstract: In one embodiment of a method to reduce vertical position errors of an aircraft, a disturbance input acting on the aircraft may be determined. The magnitude of the disturbance may be converted into a delta lift command if the magnitude of the disturbance is outside a criteria. The delta lift command may be post processed. The delta lift command may be converted into symmetric lateral surface position commands for control surfaces. The symmetric lateral surface position commands may be communicated to lateral control surface actuators to move the control surfaces according to the symmetric lateral surface position commands.

Abstract: A trench opener/closer is provided for an agricultural seeding machine movable in a planting direction. The trench opener/closer includes a disc opener assembly, a gauge wheel assembly, a closing assembly, a boot member, and a seed delivery member. The disc opener assembly has a first axis of rotation. The gauge wheel assembly has a second axis of rotation disposed rearward of the first axis of rotation in the planting direction. The closing assembly has a third axis of rotation disposed rearward of the second axis of rotation in the planting direction. The boot member extends between the disc opener assembly and the closing assembly. The seed delivery member is disposed rearward of the disc opener assembly in the planting direction. The seed delivery member is disposed adjacent to both a trailing edge of the boot member and the closing assembly.

Abstract: An apparatus for curing a composite assembly may include a base tool, a growth control apparatus, and at least one engagement fitting. The base tool may have a different thermal expansion growth rate than a composite assembly to be cured using the apparatus. The growth control apparatus may have a different thermal expansion growth rate than the base tool. The engagement fitting may be moveably disposed relative to the base tool and connected to the growth control apparatus. The engagement fitting may hold a composite assembly being cured against the engagement fitting. The growth control apparatus may grow a pre-determined amount during curing of a composite assembly to produce a cured composite assembly having a pre-determined design dimension.

Abstract: A system for single wire secondary distribution comprising a spacecraft platform; a central bus interface unit coupled to the spacecraft platform; a payload unit coupled to the central bus interface unit; and a centralized power supply for powering the central bus interface unit and the payload unit; wherein the spacecraft platform provides a command to the central bus interface unit; wherein the central bus interface unit interrupts the power to the payload unit in a manner corresponding to the commands received by the central bus interface unit; wherein the payload unit decodes the interruption to the power and executes the command from the spacecraft platform.

Abstract: The invention relates to a method of bonding two members together utilizing a stack of solid film adhesive and a layer of solid film adhesive, both disposed between the members. A pressure-applying device may be utilized to apply low pressure to force the members together. The pressure may force the stack to compress and expand in varying directions in order to substantially remove air-bubbles between the layer and one of the members. A heating device may be utilized to change the layer and the stack into liquid states in order to bond the members together with a void-free bond-line.

Abstract: The invention relates to a combined thermal protection and surface temperature control apparatus. In one embodiment, a combined thermal protection and surface temperature control apparatus comprises a porous member having an entrance side, and a separate exit side. One or more coolant entrance channels extend through the entrance side, extend part-way through the porous member, and end within the porous member before reaching the exit side. Conversely, one or more coolant exit channels begin within the porous member, extend through a portion of the porous member, and extend through the exit side. The coolant entrance and exit channels may be parallel and may alternate. The channels may only extend across a portion of the thickness of the porous member.

Abstract: In one embodiment, a method is used to provide dynamic electrical power management which may minimize the potential for overload conditions and may ensure that system performance limits are maintained. The method may dynamically limit the primary load system power draw in response to the net power draw of all other electrical power users on the aircraft which may ensure that the total power levels remain below critical limits. The method may also provide predictive controls to handle rapid load transients. Additionally, if vital functions are not being met, the method may shed other selected aircraft electrical loads which may ensure that adequate power is provided to the primary load system.

Abstract: The disclosure provides bearing sleeves or bushings made of memory shape material, and processes for installing such bearing sleeves or bushings. In one process, inner and outer surfaces of a bearing sleeve, made of a memory shape material, may be compressed at least one first temperature. A bearing may be inserted in a cavity of the bearing sleeve, and the bearing sleeve may be disposed adjacent to a surface of a structure, while the bearing sleeve is at the at least one first temperature. The inner and outer surfaces of the bearing sleeve may be expanded, at least one second temperature, to abut against the bearing and the surface of the structure.