Abstract: There is provided a method for processing data sets in a processor. The processor has a pipelined data path including an input, an output, and at least one discrete stage. The pipeline is configured to enable one or more data sets, each comprising one or more data items, to enter the pipeline from the input, propagate through the pipeline, and exit the pipeline through the output. Each discrete stage represents an operation to be performed on the data item occupying the discrete stage. The method comprises defining one or more non-overlapping sections of the pipeline corresponding to portions of the pipeline occupied by the data items of at least one data set. In addition, the method comprises providing one or more logic units, each dedicated to control the progress of the data items of the at least one data set through the pipeline as the section advances through the pipeline.

Abstract: A system and method for receiving, from a data source, at least one type of information for a plurality of aircraft, calculating efficiency data based on the received information, distributing the efficiency data to users of the system and storing the calculated efficiency data, the efficiency data including an average separation between arriving aircraft, an arrival rate an airport, an elapsed time from a point of interest to an arrival of the aircraft at an airport, a comparison of an actual base leg initiation to an optimal base leg initiation for an aircraft and a comparison of an estimated time for passing fixed points on an arrival path and the actual time for passing the fixed points.

Abstract: A twist drill assembly (10) comprising a shaft (30) and a drill tip (20); the shaft having a single internal shaft conduit (34) for a fluid, extending between orifices (36, 37) formed into the shaft; the drill tip having an internal drill tip conduit (22) for the fluid, extending between orifices formed into the drill tip; the shaft and the drill tip configured such that the drill tip is connectable to an end of the shaft with the internal drill tip conduit in communication with the internal shaft conduit, allowing the fluid to be capable of flowing from the internal shaft conduit into the internal drill tip conduit; the internal shaft conduit having a spiral form aligned with a central longitudinal axis of the shaft, and configured to complement the arrangement of spiral flutes (38) formed on the shaft.

Abstract: A computer implemented method of generating a digital collage layout for a group of digital images is disclosed. A group of digital images is retrieved from a computer accessible memory. A determination is made whether to select the digital collage layout from a stored collection of digital collage layouts or to generate a new set of digital collage layouts and select the digital collage layout from the new set. Based on determination, the digital collage layout is provided from the stored collection or from the new set.

Abstract: An apparatus for endpoint detection during removal of material from an electronic component includes a mounting plate operable to provide physical and electrical attachment for a device-under-test (DUT), a spindle operable to hold a tip for removing material from the DUT, a signal generator operable to provide an input signal to a first electrode, and a microprocessor connected to use an output signal from a second electrode to terminate the removal of material when an endpoint is reached, the first electrode being one of the tip and the DUT and the second electrode being the opposite one of the tip and the DUT.

Abstract: A method for detecting an endpoint during removal of material from an electronic device includes while removing material from an electronic device-under-test (DUT) using a tip driven by a spindle, applying an input signal to the DUT via the tip and using an output signal received from one of the DUT and a mounting plate to which the DUT is attached to determine an endpoint for removal of material.

Abstract: A cutter element (100) for a rotary machine tool having an axis of rotation, the cutter element comprising a plurality of cutting edges (110) defined by at least one cutter structure (120) comprising superhard material, consecutive cutting edges being spaced apart by at most 10 mm and configured operable to cut a body when moved in a direction that is substantially non-aligned with the axis of rotation.

Abstract: A lightweight concrete masonry unit for veneering the face of a building. The veneer block includes a body with planar front, top, bottom, and side surfaces with the top, bottom, and sides perpendicular to the front surface. One or more channels are formed in the rear surface. The depth of the channels are restricted to maintain no less than one inch of remaining wall thickness between the channel bottoms and the opposite front surface. The novel shape and larger minimum wall thickness of the lightweight veneer block enables production on a commercial block machine within the standard cycle time, provides weight and raw material cost savings up to 50%, and allows block heights that are not attainable with conventional hollow core veneer blocks.

Abstract: A cargo barrier net for an aircraft includes a net mesh, defined by a plurality of net strands, a securing members coupled to one of the net strands, for securing the cargo barrier net across an internal space of an aircraft; and a tear webbing located between the securing members and the net strand. The tear webbing is configured to tear progressively when a load is applied to it, thereby increasing the effective length of net strand to which it is coupled and redistributing the load to other net strands in the cargo barrier net.

Abstract: A tip (20) for a rotary machine tool comprising a superhard structure (12) joined to a cemented carbide substrate 14 by means of at least one intermediate layer (161, 62, 163) disposed between the superhard structure (12) and the cemented carbide substrate (14), the intermediate layer or layers (161, 162, 163) comprising grains of superhard material and grains of a metal carbide material dispersed in a metal binder material.

Abstract: Disclosed is a method of monitoring operation of programmable logic for a streaming processor, the method comprising: generating a graph representing the programmable logic to be implemented in hardware, the graph comprising nodes and edges connecting nodes in the graph; inserting, on each edge, monitoring hardware to monitor flow of data along the edge. Also disclosed is a method of monitoring operation of programmable logic for a streaming processor, the method comprising: generating a graph representing the programmable logic to be implemented in hardware, the graph comprising nodes and edges connecting the nodes in the graph; inserting, on at least one edge, data-generating hardware arranged to receive data from an upstream node and generate data at known values having the same flow control pattern as the received data for onward transmission to a connected node.

Abstract: A system management human-machine interface application for use in a process control system is described herein that enables users to view/monitor information regarding system status and performance and to initiate changes to the operation of system equipment, checkpoint control stations and execute diagnostics. A system management graphical user interface includes a number of features that enhance the accessibility of system status information to users. Such enhancements include rendering selectable diagnostic information (e.g., online/offline status) on a system component navigation view. The GUI also provides access to a variety of system information including: alarms, messages, watched system management parameters, and a legend for symbols displayed in a system management navigation tree.

Abstract: A cutting insert incorporates a pre-formed discrete cutting tip which wraps around a curved cutting corner of the insert. The cutting tip includes a top layer and a bottom layer made of a relatively harder material than the top layer. In one embodiment, the bottom layer is made of polycrystalline diamond (PCD) or a polycrystalline cubic boron nitride (CBN) material and the top layer is made of cemented carbide. The cutting insert may further incorporate a chip control structure formed in the cutting tip including a plurality of facets formed on each side of a centerline for providing chip control during a cutting operation. The chip control structure can be formed in a two-step process to expose a portion of the bottom layer. The discrete cutting tip can be brazed to the cutting insert prior to forming the chip control structure.

Abstract: A system and method for receiving data on an aircraft, the data including a tail number of the aircraft, storing the data in a database, receiving a request including further data, the further data being related to the aircraft, querying the data in the database using the further data and returning the tail number of the aircraft.

Abstract: A method for receiving passive data corresponding to an aircraft in a vicinity of an airport, receiving additional information corresponding to the aircraft and predicting a time of arrival at a gate based on the passive data and the additional information. In addition, a system having a data receiving arrangement receiving passive data corresponding to an aircraft in a vicinity of an airport and additional information corresponding to the aircraft and a gate prediction module predicting a time of arrival at a gate based on the passive data and the additional information.

Abstract: A system and method for receiving, from a data source, at least one type of information for a plurality of aircraft, calculating efficiency data based on the received information, distributing the efficiency data to users of the system and storing the calculated efficiency data, the efficiency data including an average separation between arriving aircraft, an arrival rate an airport, an elapsed time from a point of interest to an arrival of the aircraft at an airport, a comparison of an actual base leg initiation to an optimal base leg initiation for an aircraft and a comparison of an estimated time for passing fixed points on an arrival path and the actual time for passing the fixed points.

Abstract: A vaso-occlusive device is disclosed. The device includes a vaso-occlusive member having a coating disposed thereon. In accordance with one embodiment, the coating comprises a polyacrylic material. In accordance with another embodiment, the coating comprises a polyvinyl alcohol-based material. In accordance with other embodiments, various other materials and coatings are applied to at least a portion of a vaso-occlusive device.

Abstract: Apparatus and a method for treating an irregularity in a wall of a vessel of a patient defined by an irregular or afflicted wall portion with adjacent normal wall portions comprises a catheter having a distal end portion for being guided through the vessel to the site of the irregularity. A balloon associated with said distal end portion of the catheter for selective inflating to contact the walls of the vessel urges a stent carried by the distal end portion of the catheter in a constricted condition for passage through the vessel into an expanded form with the stent spanning the afflicted wall portion and contacting the adjacent wall portions. The catheter is formed with lumens for inflating the balloon, for receiving a guidewire for guiding the catheter through the vessel, and for connecting a port in the catheter proximate the afflicted wall portion to enable delivery of a therapeutic agent into the vessel to contact the stent and the irregular wall portion.

Abstract: A system and method for receiving a first set of data for a plurality of aircraft landings at an airport, receiving a second set of data corresponding to the plurality of aircraft landings at the airport, the second set of data being received from a passive radar data source and comparing the first set of data to the second set of data to generate rules for analyzing additional data received from the passive radar data source. Also, a system and method for receiving passive data for an aircraft, receiving actual data for the aircraft, comparing the passive data to the actual data based on a set of rules and assigning a confidence level to the passive data based on the comparison.

Abstract: A system and method for reducing airport delays using passive radar information and analytics. The system includes (a) a data receiving arrangement receiving, from a data source, at least one type of information for a plurality of aircraft; (b) a data processing arrangement calculating efficiency data based on the received information; and (c) a data distribution arrangement organizing efficiency data into a displayable file and distribute the file to users of the system.