Patent classifications
H01M6/5044
Modular battery powered handheld surgical instrument with multiple magnetic position sensors
A system comprising a surgical instrument is disclosed. The surgical instrument includes a handle, a shaft, a plurality of magnets, a plurality of sensors configured to determine a distance away from one or more of the plurality of magnets, and a processor communicatively coupled to the plurality of sensors. The processor is configured to determine a three dimensional change in position of the shaft by computing a three dimensional change in position of the one or more magnets, using the change in the distances determined by the one or more plurality of sensors.
INSULATION DETECTION DEVICE AND INSULATION DETECTION METHOD FOR COOLING PLATE OF BATTERY PACK
An insulation detection device and an insulation detection method for a cooling plate of a battery pack are provided. The device includes a detection position for placing the cooling plate of the battery pack, conductive cotton, a first conductive element, a second conductive element, and an insulation detector. The cooling plate of the battery pack is hollow, and an outer surface of the cooling plate of the battery pack is coated with an insulation coating. The conductive cotton is arranged in the detection position for wrapping the cooling plate of the battery pack. The first conductive element is connected to an inner wall of the cooling plate of the battery pack. The second conductive element is connected to the conductive cotton. A first end of the insulation detector is connected to the first conductive element, and a second end of the insulation detector is connected to the second conductive element.
Architectural materials having integrated energy storage system
The present invention is generally directed to energy storage systems comprising manufactured architectural materials having electrical battery systems embedded therein. The manufactured materials are generally provided as architectural panels, such as panels useful for interior or exterior cladding for buildings, flooring, countertops, or stairs. The panels comprise at least one battery device or battery assembly that is over-formed by and/or bonded with the architectural material. In preferred embodiments, the panels are formed by flowing a viscous architectural material precursor around the battery device or assembly and curing the precursor so as to solidify the architectural material. The panels may be electrically connected in any number of various arrangements, which can be chosen based on the specific application for the energy storage system.
BATTERY CAPACITY INDICATOR
The technology relates to a capacity indicator for use with a battery. One aspect of the technology provides an improved activation circuit for a capacity indicator that is easier to use and less prone to false alarms. A further aspect of the technology provides an improved indicator which is able to indicate battery capacity without requiring the use of expensive battery labels such as thermochromic strip. A further aspect of the technology provides a capacity determination circuit which is housed within a battery and which is able to provide a more accurate indication of battery capacity.
Jettisonable battery systems for powering electrical turbopumps for launch vehicle rocket engine systems
Disclosed herein are various technologies pertinent to jettisonable battery systems for use in rocket engine-based launch vehicles. Such systems may feature batteries that are configured to be used to power one or more electric turbopumps that may be used to supply fuel to a rocket engine or engines. One or more of the batteries may be jettisoned during flight in order to reduce weight and as they are depleted. In some implementations, a depleted battery may remain electrically connected with the turbopump(s) while a new battery is electrically connected with the turbopump(s). The depleted battery may then be electrically disconnected from the turbopump and jettisoned.
Jettisonable battery systems for powering electrical turbopumps for launch vehicle rocket engine systems
Disclosed herein are various technologies pertinent to jettisonable battery systems for use in rocket engine-based launch vehicles. Such systems may feature battery units that are configured to be used to power one or more electric turbopumps that may be used to supply fuel to a rocket engine or engines. One or more of the battery units may be jettisoned during flight in order to reduce weight and as they are depleted. In some implementations, the battery units may be connected in parallel with the turbopump(s), with a depleted battery unit being electrically disconnected from the parallel circuit and jettisoned.
BATTERY MODULES AND SYSTEMS FOR REMOTE COMMAND AND CONTROL OF SAME
Described are remote command-enabled battery modules and systems and methods incorporating them.
DATA PROCESSING APPARATUS, DATA PROCESSING METHOD AND COMPUTER READABLE MEDIUM
Provided are a data processing apparatus, a data processing method and a computer program. The data processing apparatus processes measured data of a plurality of power storage devices, comprises: a storage unit that stores determination model using an autoencoder, which is trained to reproduce measured data when measured data is input, the input measured data being of each of the plurality of energy storage devices or of each group of energy storage devices, which is grouped from the plurality of the energy storage devices; and a processor. The processor determines the measured data of an odd energy storage device out of the measured data for each of the energy storage devices or for each group of energy storage devices based on an error between reproduced measured data, which is output when the measured data is input to the determination model, and the measured data.
ELECTRICAL DEVICE POWER MANAGEMENT
An electrical device includes a memory storing a value indicative the remaining available rated capacity of one or more batteries. The stored value is changed in use to reflect reducing capacity. The initial stored value is chosen so that there is a very high (e.g. >99.9%) confidence that the one or more batteries will provide at least the capacity indicated by the initial stored value. This reduces the chance of failure during emergency procedures. The one or more batteries may be integral to the electrical device. An override facility is provided.
Modular battery powered handheld surgical instrument with self-diagnosing control switches for reusable handle assembly
Provided is a system and medical device that includes self diagnosing control switches. The control switch may be slidable within a slot in order to control activation of some function of the medical device. Due to natural wear and tear of movement of a control switch, the distances along the sliding slot that correspond to how much energy is used for the function may need to be adjusted over time in order to reflect the changing physical attributes of the actuator mechanism. The self diagnosing control switches of the present disclosures may be configured to automatically adjust for these thresholds using, for example, Hall effect sensors and magnets. In addition, in some cases, the self diagnosing control switches may be capable of indicating external influences on the controls, as well as predict a time until replacement is needed.