Abstract: An agricultural fertilizer system and method for applying a granular fertilizer to a field. A hopper defines a cavity adapted to hold the granular fertilizer and a metering device is coupled to the hopper, and is adapted to deliver a metered amount of fertilizer through a fertilizer hose coupled to a fertilizer spreader. A sensor device is disposed along the fertilizer hose between the fertilizer hose input and the fertilizer house output to identify a blockage resulting from a build-up of fertilizer. A blower delivers an airflow through an airflow hose operatively connected to the fertilizer hose, wherein the airflow hose is connected to the blower hose between the metering device and the sensor device. The airflow provided by the blower reduces or eliminates a buildup of fertilizer within the fertilizer hose to maintain a proper flow of fertilizer from the metering device and the fertilizer spreader.

Abstract: A catheter, including a catheter tube defining: a proximal end; a distal end; a longitudinal axis; a lumen therethrough; and one or more zones having each having a cut pattern segment therein, wherein cut pattern segment defines a plurality of cuts spaced around a circumference of the tube. The distal end may include a tip segment having a plurality of helical segments extending around the longitudinal axis, wherein each helical segment includes two substantially parallel filars connected at distal ends thereof.

Abstract: A catheter, including a catheter tube defining: a proximal end; a distal end; a longitudinal axis; a lumen therethrough; and one or more zones having each having a cut pattern segment therein, wherein cut pattern segment defines a plurality of cuts spaced around a circumference of the tube. The distal end may include a tip segment having a plurality of helical segments extending around the longitudinal axis, wherein each helical segment includes two substantially parallel filars connected at distal ends thereof.

Abstract: A device displays a clock face in response to receiving a request to display a clock face. In accordance with a determination that a respective graphical element is to be displayed at a respective location on the clock face, the clock face includes a plurality of analog-dial graphical elements corresponding to respective units of time, where the plurality of analog-dial graphical elements includes a first analog-dial graphical element that occupies a first position and has a first size. In accordance with a determination that the respective graphical element is not to be displayed at a respective location on the clock face, the clock face includes the plurality of analog-dial graphical elements corresponding to the respective units of time, and the first analog-dial graphical element of the plurality of analog-dial graphical elements occupies a second position and/or has a second size. In some embodiments, clock faces are reordered.

Abstract: A fuel additive for hydrocarbon fuel that is fueled in fired burners and open flames for enhancing fuel storage, for enhancing fuel combustion by increasing fuel efficiency, and/or for reducing undesirable emissions, such as pollutants, includes an inorganic metal oxide, a metal carboxylate, an acid, and an organic dispersion fluid.

Abstract: The invention relates to an unmanned air vehicle control system and method, designed such that, in one mission mode, the vehicle follows the mission route. The system comprises means (400, 450) for storing data indicating at least one auxiliary route (4000, 4001, 4002, 4003), such that each of a plurality of the mission route segments (10, 20), is assigned at least part (30, 31, 32, 33) of at least one auxiliary route. Furthermore, the system comprises route change means (53) designed for, as a response to a mission abandonment event (52), determining which part of which auxiliary route is assigned to the mission route segment where the vehicle is located, such that the vehicle can change the mission route to the corresponding auxiliary route.

Abstract: According to the method of the invention, control parameters V indicating speed, R indicating turn characteristics and ? indicating a path angle are determined such that these parameters are maintained between limits, and such that one of them deviates as little as possible from a corresponding control input parameter Ri. In order to maintain (as much as possible) the value of R unchanged, V can be varied. The method may include the calculation of the maximum and minimum thrust available.

Abstract: The invention relates to an unmanned air vehicle control system and method, designed such that, in one mission mode, the vehicle follows the mission route. The system comprises means (400, 450) for storing data indicating at least one auxiliary route (4000, 4001, 4002, 4003), such that each of a plurality of the mission route segments (10, 20), is assigned at least part (30, 31, 32, 33) of at least one auxiliary route. Furthermore, the system comprises route change means (53) designed for, as a response to a mission abandonment event (52), determining which part of which auxiliary route is assigned to the mission route segment where the vehicle is located, such that the vehicle can change the mission route to the corresponding auxiliary route.

Abstract: According to the method of the invention, control parameters V indicating speed, R indicating turn characteristics and ? indicating a path angle are determined such that these parameters are maintained between limits, and such that one of them deviates as little as possible from a corresponding control input parameter Ri. In order to maintain (as much as possible) the value of R unchanged, V can be varied. The method may include the calculation of the maximum and minimum thrust available.

Abstract: A water bottle swing is provided including a stand with a swing assembly rotatably coupled thereto. In use, a water bottle is situated within the swing assembly so the water may be easily dispensed therefrom. Further provided is a rigid retainer including a loop wire having a linear portion with a first end coupled to the swing assembly. The loop wire further has a second end with a circular loop portion formed thereon.