Abstract: An aircraft including a wing with a fixed wing portion and a wing tip device rotatably hingedly attached at a fixed wing portion outboard end. The wing includes a wing fold mechanism configured to actuate the wing tip device to rotate relative to the fixed wing portion to at least three commanded and predetermined wing fold angles and to restrain rotational movement of the wing tip device at each commanded position. A first position corresponds to high-speed flying, a second position to ground-based operations and a third position to low-speed flying. The flying positions rotate the wing tip to a position where upper and lower wing tip surfaces are continuations of the upper and lower surfaces of the fixed wing, with a low-speed incidence angle being less than a high-speed incidence angle. The ground-based position reduces the wing span to the greatest degree of the three positions.

Abstract: A water containment system has: a peripheral dam formed of one or more arcuate longitudinal wall sections that are configured to be secured in an assembled position in use around a water tank as the water tank rests on a ground surface, the peripheral dam defining an open water-tank-receiving base; and a drain port defined in the peripheral dam. In a method of retrofitting a water containment system around a water tank, the method includes: assembling a peripheral dam, formed of one or more arcuate longitudinal wall sections around the water tank as the water tanks rests on a ground surface; securing the peripheral dam to the ground surface; and connecting a drain line from a drain port in the peripheral dam to a drain.

Abstract: A method for creating and deploying plugins for use with one or more web-hosted large language model applications includes: displaying a user interface comprising a code template for creation of a plugin, wherein the code template comprises a context template, a native function template, and a semantic prompt template; receiving modifications to the code template via the user interface to form a modified code template, the modified code template comprising: custom context based on the context template; custom native code comprising one or more computer executable functions based on the native function template; and a custom prompt configured to prompt a large language model based on the semantic prompt template; generating a plugin based on the modified code template; and storing the plugin within a database of a plugin registry.

Abstract: An air handling transport includes a base frame, and an air housing mounted to the base frame. The air housing includes a combustion air plenum on a longitudinal side of the air handling transport, the combustion air plenum outputting filtered combustion air. The transport further includes an exhaust stack mounted to the base frame for releasing combustion exhaust air. The exhaust stack is rotatable between the longitudinal side in an operation mode and an end side in a transportation mode. The exhaust stack includes a stack base having an exhaust plenum and a stack extension. The stack extension is housed within the stack base in the transportation mode and extends vertically by a predetermined vertical distance in the operation mode.

Abstract: The present invention relates to a novel anti-cancer radiopharmaceutical treatment that is particularly suitable for targeting PARP enzyme expressing cancers. The novel treatment involves PARP-targeted Auger-emitting radiopharmaceutical compounds of formula (I), or a pharmaceutically acceptable salt or solvate thereof: wherein: A1, A2 and A3 are each as defined herein. The present invention also relates to processes for the preparation of these compounds, to pharmaceutical compositions comprising them, and to their use in the treatment cancer.

Abstract: An embodiment includes a platform shape memory polymer system. Such an embodiment exhibits a blend of tunable, high performance mechanical attributes in combination with advanced processing capabilities and good biocompatibility. A post-polymerization crosslinking synthetic approach is employed that combines polyurethane and thiol-ene synthetic processes. Other embodiments are described herein.

Abstract: The present application discloses a method, system, and computer system for building a model associated with a dataset. The method includes receiving a data set, the dataset comprising a plurality of keys and a plurality of key-value relationships, determining a plurality of models to build based at least in part on the dataset, wherein determining the plurality of models to build comprises using the dataset format information to identify the plurality of models, building the plurality of models, and optimizing at least one of the plurality of models.

Abstract: A package having a product locking feature can include a product display panel to which a product is secured with a product locking assembly. The product locking assembly can include a locking element and a receiving element, the locking element being one-way insertable into the receiving element in two stages, the first stage being for securing the product display panel to the product and the second stage being further insertion of the locking element into the receiving element after the product is removed from the product display panel.

Abstract: An embodiment includes a platform shape memory polymer system. Such an embodiment exhibits a blend of tunable, high performance mechanical attributes in combination with advanced processing capabilities and good biocompatibility. A post-polymerization crosslinking synthetic approach is employed that combines polyurethane and thiol-ene synthetic processes. Other embodiments are described herein.

Abstract: An aircraft wing is disclosed having a fixed wing with a tip, and a wing tip device rotatably mounted on a hinge at the tip of the fixed wing, such that the wing tip device is rotatable about the hinge, and an actuation system for rotating the wing tip device about the hinge. The actuation system includes a motor, at least one geared rotary actuator, a reduction gearbox, a clutch for selectively decoupling rotation of the motor from rotation of the geared rotary actuator, the geared rotary actuator is driveable by the motor and arranged to convert rotary motion into a different rotary motion and is arranged to rotate the wing tip device relative to the tip of the fixed wing. The clutch is coupled to the geared rotary actuator by a shaft and the shaft is fixed in rotation to a mass disposed radially outwardly from the shaft.

Abstract: An aircraft wing is disclosed having a fixed wing with a tip, and a wing tip device rotatably mounted on a hinge at the tip of the fixed wing, such that the wing tip device is rotatable about the hinge, and an actuation system for rotating the wing tip device about the hinge. The actuation system includes a motor, at least one geared rotary actuator, a reduction gearbox, a clutch for selectively decoupling rotation of the motor from rotation of the geared rotary actuator, the geared rotary actuator is driveable by the motor and arranged to convert rotary motion into a different rotary motion and is arranged to rotate the wing tip device relative to the tip of the fixed wing. The reduction gearbox is positioned between the clutch and the geared rotary actuator along a drive train between the motor and the geared rotary actuator.

Abstract: An aircraft wing is provided having a fixed wing with a gulled wing tip rotatably mounted at the tip thereof, the gulled wing tip extending below a wing plane defined by the end of the fixed wing such that the centre of gravity of the gulled wing tip is located below the wing plane. Lowering the centre of gravity of the gulled wing tip has been found to reduce the onset of flutter. The gulled wing tip may be gulled about a hinge axis where it meets the fixed wing, or may be otherwise folded or curved to lower the centre of gravity of the gulled wing tip.

Abstract: The present application discloses a method, system, and computer system for building a model associated with a dataset. The method includes receiving a data set, the dataset comprising a plurality of keys and a plurality of key-value relationships, determining a plurality of models to build based at least in part on the dataset, wherein determining the plurality of models to build comprises using the dataset format information to identify the plurality of models, building the plurality of models, and optimizing at least one of the plurality of models.

Abstract: An antenna may include rigid antenna ribs, a flexible antenna reflector layer, and a flexible support member extending behind the flexible antenna reflector layer between adjacent antenna ribs and having first and second sets of openings therein. A drawstring may extend through the first set of openings between adjacent ribs and a rear support cord is behind the flexible support member between adjacent ribs. Tie cords may extend between the flexible antenna reflector layer and the rear support cord and pass through respective ones of the second set of openings. A biasing member may maintain tension in the drawstring as adjacent antenna ribs move between first and second positions so that the flexible support member defines a pleated support body for the flexible antenna reflector layer.

Abstract: An antenna may include rigid antenna ribs, a flexible antenna reflector layer, and a flexible support member extending behind the flexible antenna reflector layer between adjacent antenna ribs and having first and second sets of openings therein. A drawstring may extend through the first set of openings between adjacent ribs and a rear support cord is behind the flexible support member between adjacent ribs. Tie cords may extend between the flexible antenna reflector layer and the rear support cord and pass through respective ones of the second set of openings. A biasing member may maintain tension in the drawstring as adjacent antenna ribs move between first and second positions so that the flexible support member defines a pleated support body for the flexible antenna reflector layer.

Abstract: An aircraft wing has a fixed wing and a moveable wing tip device. The wing is operable in a fixed flight configuration, in which the wing tip device is fixed relative to the fixed wing and the wing tip device is forward swept, and a moving flight configuration in which the wing tip device is free to move relative to the fixed wing. The forward moveable swept wing tip device may provide particular synergy with a forward swept fixed wing.

Abstract: An aircraft wing is disclosed having a main fixed wing portion and a wing tip device at a tip thereof. The wing tip device is configurable between a flight configuration and a ground configuration, in which ground configuration the wing tip device is moved away from the flight configuration such that the span of the aircraft wing is reduced. A hinge arrangement connects the main fixed wing portion and the wing tip device and enables the wing tip device to rotate between the ground configuration and the flight configuration. The hinge arrangement protrudes beyond an outer surface of the main fixed wing portion and wing tip device. A fairing covers at least part of the hinge arrangement on at least a suction side of the wing.

Abstract: The present disclosure relates to a fiber optic connector including a ferrule assembly in which an optical fiber is secured by bonding material. The fiber optic connector includes a molded tube for facilitating injecting the bonding material into the ferrule assembly during manufacture of the fiber optic connector.

Abstract: An embodiment includes a platform shape memory polymer system. Such an embodiment exhibits a blend of tunable, high performance mechanical attributes in combination with advanced processing capabilities and good biocompatibility. A post-polymerization crosslinking synthetic approach is employed that combines polyurethane and thiol-ene synthetic processes. Other embodiments are described herein.

Abstract: The present application discloses a method, system, and computer system for querying a model associated with a dataset. The method includes providing an input interface via which a first entity inputs a dataset, receiving the dataset, and providing a selection interface that exposes to a second entity the plurality of models determined for the dataset and/or the plurality of results corresponding to the plurality of models using the index entries. The dataset comprises a plurality of keys and a plurality of key-value relationships, and the dataset is formatted according to a predefined format, wherein index entries are generated for a plurality of models and a plurality of results corresponding to the plurality of models.