Abstract: A protection circuit for protecting an energy storage device includes a first circuit region between a first terminal of the energy storage device and a first connector node, a second circuit region between a second terminal of the energy storage device and a second connector node, a latching circuit to electrically couple the first connector node to the first terminal of the energy storage device when the latching circuit is in a closed configuration, and a contactor circuit electrically coupled to an operational switch of the latching circuit, the contactor circuit comprising a capacitor to store charge and a microcontroller to monitor an electrical property of the energy storage device to determine if a short circuit occurs and, if a short circuit does occur, cause the capacitor to discharge to the operational switch of the latching circuit to cause the latching circuit to transition to the open configuration.

Abstract: A protection circuit for protecting an energy storage device includes a first circuit region between a first terminal of the energy storage device and a first connector node, a second circuit region between a second terminal of the energy storage device and a second connector node, a latching circuit to electrically couple the first connector node to the first terminal of the energy storage device when the latching circuit is in a closed configuration, and a contactor circuit electrically coupled to an operational switch of the latching circuit, the contactor circuit comprising a capacitor to store charge and a microcontroller to monitor an electrical property of the energy storage device to determine if a short circuit occurs and, if a short circuit does occur, cause the capacitor to discharge to the operational switch of the latching circuit to cause the latching circuit to transition to the open configuration.

Abstract: A rechargeable aircraft battery assembly includes at least one lithium-ion cell having a positive cell terminal and a negative cell terminal and a battery management circuit operable to control charging and/or discharging of the lithium-ion cell. The battery management circuit is constantly off when the aircraft circuit is not engaged with the battery connector and is constantly on when the aircraft circuit is engaged with the battery connector.

Abstract: A rechargeable aircraft battery assembly includes at least one lithium-ion cell having a positive cell terminal and a negative cell terminal and a battery management circuit operable to control charging and/or discharging of the lithium-ion cell. The battery management circuit is constantly off when the aircraft circuit is not engaged with the battery connector and is constantly on when the aircraft circuit is engaged with the battery connector.

Abstract: A frame device for supporting objects such as batteries during seismic stress, comprising a pair of end frame members mounted in upstanding spaced apart relation by a plurality of vertically spaced elongated channel support members secured at opposite terminal ends to the vertical columns of the end frame members, shelves for supporting batteries spanning the channel support members and defining a plurality of compartments for the batteries, each end frame member being formed of a single sheet material shaped to define vertical columns and a web extending between the end columns, a pair of anchors, means for securing the end frames to the anchors, and means defining a plurality of openings in the web of each end frame generally aligned with the compartments formed by the shelves to provide horizontal ventilation of batteries mounted in the compartments.

Abstract: Lead-acid storage batteries of the type having a plurality of cells, each including alternating positive and negative plates, each plate including an upstanding lug, and a partition separating adjacent cells are provided with unique improved lighter weight and lower resistance plate and intercell connectors. The connector comprises at least one cell plate connector including a wall with a multiple spaced slots for receiving the lugs from either the positive or negative plates of the cells. A strap extends from the cell plate connector. The cell plate connector and the strap are formed of a metal substrate that has a lower specific gravity and higher conductivity than lead, the substrate having a lead-based outer coating that resists the corrosive effects of the battery acid. A small amount of lead is then applied covering the slotted wall and at least a portion of each lug to insure good connection.

Abstract: Lightweight, low resistance, thin plate for lead-acid electrochemical cells formed primarily of an aluminum foil substrate having a thickness of between about 0.005 inches and 0.030 inches, and a continuous outer layer of lead or lead alloy having a thickness of less than about 0.005 inches and that is corrosive resistant to the electrolytic acid of the battery.

Abstract: Lightweight, low resistance electrode plates for lead-acid batteries are formed from a highly conductive non-lead substrate with a corrosion prevention layer and a continuous layer of a corrosive resistant conductive materials, such as lead, applied from a fused salt bath.

Abstract: An improved terminal post assembly for low resistance high conductivity, lead/acid batteries in which the conventional cast lead connector which connects the battery post with the terminal has been replaced by a prefabricated connector formed of a material having a non-lead content of greater than 50% and a melting temperature of greater than 450° F.

Abstract: Light weight, low resistance electrode plates for lead-acid batteries are formed from a highly conductive non-lead substrate such as aluminum or copper, coated with a continuous layer of a corrosive resistant conductive materials, such as lead, applied from a fused salt bath.

Abstract: An improved terminal post assembly for lead/acid batteries in which the conventional cast lead connecting pad which connects the battery post with the threaded terminal has been replaced by a prefabricated connector formed of a lightweight material having high current capacity and creep resistance.

Abstract: A lead-acid aircraft battery including an electric terminal assembly for making connections to the internal electrodes of the battery, the terminal assembly being embedded in the plastic cover of the battery and effectively sealed to the cover so as to prevent corrosion by the acid electrolyte in the battery. In a first embodiment the terminal assembly includes a pair of threaded terminal posts which extend outwardly from the cover; and a receptacle; including a corresponding pair of terminal pins respectively threaded coaxially to the posts, is attached to the cover by screws. In a second embodiment an Elcon type receptacle is molded directly into the cover.

Abstract: A molded plastic receptacle for a lead-acid aircraft battery, or the like, which is adapted to be mounted on the side wall of the battery comprising threaded pin terminals which extend through the receptacle and which are molded to the receptacle. The receptacle is formed of a polycarbonate thermoplastic resin which is sufficiently strong to permit the receptacle to be mounted on the side wall of the battery by screws extending through holes in the receptacle and without any need to provide metal bushings in the holes.