Abstract: A method for precision touch input on a touchscreen device may detect an initial touch at a first location as a starting point and detect movement to a current location. A tension value may be computed based on distance between the starting point and current location. A visual indicator may be rendered between the locations with visual properties that vary as a function of the tension value. The method may compare the tension value to a predefined threshold and maintain a cursor at the starting point while below the threshold. When the tension value meets or exceeds the threshold, the visual indicator may indicate an engaged state and cursor movement may be enabled with an offset from the current location such that the cursor is visually separated from the touch. The system may include a touchscreen display, processor, and memory storing instructions to perform these operations.

Abstract: Disclosed herein is an electrode comprising an active layer comprising a network of high aspect ratio carbon elements defining void spaces within the network; a plurality of electrode active material particles disposed in the void spaces within the network; and a polymeric binder comprising a first polymer which is a polymer comprising an acid functional group or a salt of such acid functional group; a polyamide; or an acrylate polymer, and a second polymer.

Abstract: The battery thermal management system includes a battery pack, a circulation subsystem, and a heat exchanger. The system can optionally include a cooling system, a reservoir, a de-ionization filter, a battery charger, and a controller.

Abstract: Systems and methods for protecting and fortifying machine learning engines, artificial intelligence (AI) engines, large language models, deep learning engines, reinforcement learning engines, and AI-based agentic units. An Offline Protection Unit analyzes characteristics of a Protected Engine, and performs offline fortification of the Protected Engine against attacks; by changing operational properties or operational parameters of the Protected Engine to reduce its vulnerability to attacks. An Online Protection Unit performs analysis of at least one of: (i) inputs that are intended to be inputs of the Protected Engine, (ii) outputs that are generated by the Protected Engine; and based on the analysis, dynamically performs online fortification of the Protected Engine against attacks; by dynamically changing operational properties or operational parameters of the Protected Engine to reduce its vulnerability to attacks.

Abstract: Systems and methods for protecting machine learning engines, artificial intelligence engines, large language models, and deep learning engines. An Offline Protection Unit is configured to analyze one or more characteristics of a Protected Engine, and to perform offline fortification of the Protected Engine against attacks by changing operational properties or operational parameters of the Protected Engine to reduce its vulnerability to attacks. An Online Protection Unit is configured to perform analysis of at least one of: (i) inputs that are directed to be inputs of the Protected Engine, (ii) outputs that are generated by the Protected Engine; and based on the analysis, to dynamically perform online fortification of the Protected Engine against attacks by dynamically changing operational properties or operational parameters of the Protected Engine to reduce its vulnerability to attacks.

Abstract: The system can include an on-board thermal management subsystem. The system 100 can optionally include an off-board (extravehicular) infrastructure subsystem. The on-board thermal management subsystem can include: a battery pack, one or more fluid loops, and an air manifold. The system 100 can additionally or alternatively include any other suitable components.

Abstract: A computer-implemented method for aligning vector coordinates may include receiving vector data representing boundaries of vector-represented features. A visual representation of the vector data may be displayed on a graphical user interface. A cursor and threshold indicator may be provided on the interface. At least two potential edges for alignment may be identified within the threshold indicator area. A user selection of an alignment method and input defining an extent of alignment may be received. New alignment points may be calculated based on the selected method and defined extent. The vector data may be modified to incorporate the calculated new alignment points. The method may provide real-time visual feedback during the alignment process. Configuration options may allow customization of the threshold indicator size, alignment method, and other parameters.

Abstract: The system can include an on-board thermal management subsystem. The system 100 can optionally include an off-board (extravehicular) infrastructure subsystem. The on-board thermal management subsystem can include: a battery pack, one or more fluid loops, and an air manifold. The system 100 can additionally or alternatively include any other suitable components.

Abstract: Computer-implemented systems, methods, and products for enabling one or more nodes of a first electronic ledger platform to carry out operations with respect to one or more records of the first electronic ledger platform. The operations may include receiving an indication from a smart contract to manage a transaction associated with sale of a token by a selling entity; processing information associated with the sale of the token to initiate the transaction, the information including identity of a first entity listing the token for sale and identity of a second entity having record ownership of the token; verifying one or more events or information associated with the transaction to confirm authenticity or transferability of the token; and approving the transaction.

Abstract: The invention relates to immobilized enzyme compositions for the preparation of a hexose. Hexoses include, for example, tagatose, psicose, fructose, allose, mannose, galactose, altrose, talose, sorbose, gulose, idose, and inositol. The invention also relates to an enzymatic process for preparing a hexose from a saccharide by contacting a starch derivative with an immobilized enzyme composition of the invention.

Abstract: An aircraft propulsion unit includes an electric motor, at least one accessory unit used for operating the electric motor, an inverter module, the inverter module including a plurality of inverters for powering the electric motor and the at least one accessory unit, and a cooling system coupled to the electric motor and the inverter module, the cooling system comprising a coolant path for circulating a coolant through or adjacent to the electric motor and the at least one accessory unit.

Abstract: The system can include an on-board thermal management subsystem. The system 100 can optionally include an off-board (extravehicular) infrastructure subsystem. The on-board thermal management subsystem can include: a battery pack, one or more fluid loops, and an air manifold. The system 100 can additionally or alternatively include any other suitable components.

Abstract: Systems and methods for protecting machine learning engines, artificial intelligence engines, large language models, and deep learning engines. An Offline Protection Unit is configured to analyze one or more characteristics of a Protected Engine, and to perform offline fortification of the Protected Engine against attacks by changing operational properties or operational parameters of the Protected Engine to reduce its vulnerability to attacks. An Online Protection Unit is configured to perform analysis of at least one of: (i) inputs that are directed to be inputs of the Protected Engine, (ii) outputs that are generated by the Protected Engine; and based on the analysis, to dynamically perform online fortification of the Protected Engine against attacks by dynamically changing operational properties or operational parameters of the Protected Engine to reduce its vulnerability to attacks.

Abstract: An electric motor comprises a rotor and a stator having a yoke. The yoke includes a plurality of teeth mounted to the yoke and being aligned substantially parallel to an axis of rotation of the motor, each tooth including a first radial end adjacent to the yoke and a second radial end extending from the yoke, a plurality of field coils, each field coil being wrapped around a tooth, and a coolant circulation path including a first coolant channel defined between adjacent field coils and a second coolant channel defined between adjacent field coils and between the first radial ends of adjacent teeth. A third coolant channel may be defined between adjacent field coils and between the second radial ends of adjacent teeth.

Abstract: The system can include an on-board thermal management subsystem. The system 100 can optionally include an off-board (extravehicular) infrastructure subsystem. The on-board thermal management subsystem can include: a battery pack, one or more fluid loops, and an air manifold. The system 100 can additionally or alternatively include any other suitable components.

Abstract: An aircraft propulsion unit includes an electric motor, at least one accessory unit used for operating the electric motor, an inverter module, the inverter module including a plurality of inverters for powering the electric motor and the at least one accessory unit, and a cooling system coupled to the electric motor and the inverter module, the cooling system comprising a coolant path for circulating a coolant through or adjacent to the electric motor and the at least one accessory unit.

Abstract: An aircraft propulsion unit includes an electric motor, at least one accessory unit used for operating the electric motor, an inverter module, the inverter module including a plurality of inverters for powering the electric motor and the at least one accessory unit, and a cooling system coupled to the electric motor and the inverter module, the cooling system comprising a coolant path for circulating a coolant through or adjacent to the electric motor and the at least one accessory unit.

Abstract: An aircraft propulsion unit includes an electric motor, at least one accessory unit used for operating the electric motor, an inverter module, the inverter module including a plurality of inverters for powering the electric motor and the at least one accessory unit, and a cooling system coupled to the electric motor and the inverter module, the cooling system comprising a coolant path for circulating a coolant through or adjacent to the electric motor and the at least one accessory unit.

Abstract: An aircraft propulsion unit includes an electric motor, at least one accessory unit used for operating the electric motor, an inverter module, the inverter module including a plurality of inverters for powering the electric motor and the at least one accessory unit, and a cooling system coupled to the electric motor and the inverter module, the cooling system comprising a coolant path for circulating a coolant through or adjacent to the electric motor and the at least one accessory unit.

Abstract: The battery thermal management system includes a battery pack, a circulation subsystem, and a heat exchanger. The system can optionally include a cooling system, a reservoir, a de-ionization filter, a battery charger, and a controller.