Abstract: A system has at least one winder configured to wind yarn to form a yarn package. At least one sampling and tying machine is configured to remove a portion of the yarn of the yarn package and tie off a free end of the yarn around the yarn package to inhibit the yarn package from unwinding. A dunnage supply area has therein at least one support structure for receiving a plurality of yarn packages thereon. A robotic arm is configured to: move the yarn package from the at least one winder to the at least one sampling and tying machine; move the yarn package from the at least one sampling and tying machine to at least one case assembly area; and stack the yarn package on a support structure in the at least one case assembly area.

Abstract: A system has at least one winder configured to wind yarn to form a yarn package. At least one sampling and tying machine is configured to remove a portion of the yarn of the yarn package and tie off a free end of the yarn around the yarn package to inhibit the yarn package from unwinding. A dunnage supply area has therein at least one support structure for receiving a plurality of yarn packages thereon. A robotic arm is configured to: move the yarn package from the at least one winder to the at least one sampling and tying machine; move the yarn package from the at least one sampling and tying machine to at least one case assembly area; and stack the yarn package on a support structure in the at least one case assembly area.

Abstract: An apparatus for servicing a twisting machine. The apparatus includes an automated guided vehicle (AGV), a robotic arm having an end effector coupled to the AGV, and a rack carried by the AGV. The rack is configured to hold a plurality of empty tubes and a plurality of yarn packages. A controller that is configured to cause the robotic arm to grip, by the end effector, a handle of a row of the twisting machine, lower a receptacle of the twisting machine to a loading position, remove an empty tube from a first receptacle of the at least one receptacle, place the empty tube on the rack, lift a yarn package from the rack, place the yarn package on the first receptacle, grip the handle of the row of the plurality of rows of the twisting machine, and raise the at least one receptacle to the operational position.

Abstract: An apparatus for servicing a twisting machine. The apparatus includes an automated guided vehicle (AGV), a robotic arm having an end effector coupled to the AGV, and a rack carried by the AGV. The rack is configured to hold a plurality of empty tubes and a plurality of yarn packages. A controller that is configured to cause the robotic arm to grip, by the end effector, a handle of a row of the twisting machine, lower a receptacle of the twisting machine to a loading position, remove an empty tube from a first receptacle of the at least one receptacle, place the empty tube on the rack, lift a yarn package from the rack, place the yarn package on the first receptacle, grip the handle of the row of the plurality of rows of the twisting machine, and raise the at least one receptacle to the operational position.

Abstract: A system has at least one winder configured to wind yarn to form a yarn package. At least one sampling and tying machine is configured to remove a portion of the yarn of the yarn package and tie off a free end of the yarn around the yarn package to inhibit the yarn package from unwinding. A dunnage supply area has therein at least one support structure for receiving a plurality of yarn packages thereon. A robotic arm is configured to: move the yarn package from the at least one winder to the at least one sampling and tying machine; move the yarn package from the at least one sampling and tying machine to at least one case assembly area; and stack the yarn package on a support structure in the at least one case assembly area.

Abstract: A system has at least one winder configured to wind yarn to form a yarn package. At least one sampling and tying machine is configured to remove a portion of the yarn of the yarn package and tie off a free end of the yarn around the yarn package to inhibit the yarn package from unwinding. A dunnage supply area has therein at least one support structure for receiving a plurality of yarn packages thereon. A robotic arm is configured to: move the yarn package from the at least one winder to the at least one sampling and tying machine; move the yarn package from the at least one sampling and tying machine to at least one case assembly area; and stack the yarn package on a support structure in the at least one case assembly area.

Abstract: An apparatus for servicing a twisting machine. The apparatus includes an automated guided vehicle (AGV), a robotic arm having an end effector coupled to the AGV, and a rack carried by the AGV. The rack is configured to hold a plurality of empty tubes and a plurality of yarn packages. A controller that is configured to cause the robotic arm to grip, by the end effector, a handle of a row of the twisting machine, lower a receptacle of the twisting machine to a loading position, remove an empty tube from a first receptacle of the at least one receptacle, place the empty tube on the rack, lift a yarn package from the rack, place the yarn package on the first receptacle, grip the handle of the row of the plurality of rows of the twisting machine, and raise the at least one receptacle to the operational position.

Abstract: A synthetic quartz composition having improved tensile strength, compression strength and bending strength comprising up to 90% quartz stone, from 5 to 90% quartz powder, from 0.1 to 20% resin, from 1 to 25% fiber, from 0.1 to 5% coupling agent, from 0.1 to 5% curing agent, up to 70% glass chip, up to 70% mirror chip, up to 5% pigment, up to 5% shell chip, and up to 5% metal flake, by weight, may be produced in panels and molded shapes such as containers.

Abstract: Hydrogen powered air vehicles that in some embodiments can fly with very long endurance (10 or more days) at altitudes over 60,000 ft carrying payloads of up to 2,000 pounds. Embodiments may include features such as large wingspan relative to fuselage and an all composite or partial composite structure for light weight and strength. The aircraft of the invention use one or more internal combustion engines adapted for hydrogen combustion, each engine driving propellers. The hydrogen fuel is stored on board in containers, located within the fuselage, as a cryogenic liquid, and is vaporized in a heat exchanger before delivery to the internal combustion engine.

Abstract: An synthetic quartz composition having improved tensile strength, compression strength and bending strength comprising up to 90% quartz stone, from 5 to 90% quartz powder, from 0.1 to 20% resin, from 1 to 25% fiber, from 0.1 to 5% coupling agent, from 0.1 to 5% curing agent, up to 70% glass chip, up to 70% mirror chip, up to 5% pigment, up to 5% shell chip, and up to 5% metal flake, by weight, may be produced in panels and molded shapes such as containers.

Abstract: Medical methods and apparatus for locating and securing intravascular devices, substantially grafts or stents-grafts, via a laparoscopic duct created by a surgical procedure to approach a blood vessel lumen. A stapler including a tubular body having at its distal end a head with a die and die lid and at is proximal end a control mechanism with a retaining handle and a control lever pivotally thereto. The lever is operatively connected via a spring-loaded pressure rod with a fastener located in the die. The movement of lever is transformed into radial forces necessary for punching through the wall of the intravascular device and the surrounding blood vessel wall with a fastener and simultaneously bending ends of the fastener apart. Securing the ends of the intravascular device to the wall of a blood vessel is performed via a set of at least two staplers, each having several simultaneously deliverable fasteners.

Abstract: Hydrogen powered air vehicles that in some embodiments can fly with very long endurance (10 or more days) at altitudes over 60,000 ft carrying payloads of up to 2,000 pounds. Embodiments may include features such as large wingspan relative to fuselage and an all composite or partial composite structure for light weight and strength. The aircraft of the invention use one or more internal combustion engines adapted for hydrogen combustion, each engine driving propellers. The hydrogen fuel is stored on board in containers, located within the fuselage, as a cryogenic liquid, and is vaporized in a heat exchanger before delivery to the internal combustion engine.

Abstract: A method and device for repairing incompetent venous valves and more specifically relates to repair method and an implantable support device—extravenous corrector (3), which is positionable about a dilated veins of the Sapheno-Femoral Junction (SFJ) (1) with the aim to apply an external compression force on the insufficient veins of SFJ and especially in the area of the venous valves. There are proposed several embodiments of a extravenous corrector for external correction of insufficient valves in venous junctions. The corrector is adapted to be placed immediately around the junction with venous valves, in abutting contact with its external area.

Abstract: The present invention rerlates to medical techniques, in particular, to methods and apparatus applied in minimally invasive vascular surgery to eliminate occlusion of blood vessel, using grafts and to prevent rupture of abdominal aorta using grafts or stent-grafts. More particularly, the present invention relates to methods and apparatus for locating and securing intravascular devices, substantially grafts, through a duct specially created by the surgeon to approach the blood vessel lumen. There is suggested a new and improved method for fixating an intravascular device to a blood vessel wall in combination with a new and improved stapler design based on this method.

Abstract: A set of logic cells is hierarchically grouped to form groups to be placed on an integrated circuit for gate array layout. A user interface allows a user to interact with a placement system. The system is supplied with input design files defining the integrated circuit, the cells to be grouped, the groups to be placed, and input/output buffers to be placed on the perimeter of the integrated circuit for connecting the groups with external circuitry. The system reads the input design files to create a database used for placing desired input/output buffers and for hierarchically grouping the cells and placing the groups. The groups are defined by their size, determined using utilization and aspect ratio values of the areas where the cells are to be placed. The user is allowed to move the buffers and groups to any valid locations within the integrated circuit.