Abstract: Provided is a method in an electricity-driven apparatus to be driven by receiving power through a plurality of battery packs in a parallel type. The method includes detecting a state of charge (SOC) of each of the plurality of battery packs, calculating a voltage difference between the plurality of battery packs based on the detected SOC, and performing battery pack balancing based on the calculated voltage difference exceeding a threshold value. The battery pack balancing is performed by a pre-charging circuit including a balancing relay.

Abstract: A power control device is provided for an aircraft. The power control device may include at least one first battery, a second battery having a lower power density and higher energy density than the at least one first battery, at least one lift motor connected, via a first electrical path, to the at least one first battery, a cruise motor connected, via a second electrical path, to the second battery, and a power control circuit configured to control the at least one first battery, the second battery, the at least one lift motor, and the cruise motor.

Abstract: The present disclosure relates to a flight system and a failure responding method therefor. A flight system includes: a plurality of fuse boxes configured to control application of a voltage to at least one propulsion device; and an interlock control apparatus configured to control interlock lines between fuse boxes connected using the interlock lines among the fuse boxes to synchronize and control opening of the fuse boxes connected using the interlock lines.

Abstract: A system for a vehicle may include a first battery pack diagnosis apparatus connected to a first battery pack, a second battery pack diagnosis apparatus connected to a second battery pack, a third battery pack diagnosis apparatus connected to a third battery pack, and a fourth battery pack diagnosis apparatus connected to a fourth battery pack. The first battery pack diagnosis apparatus may be configured to determine, based on a measured value of an integrated insulation resistance of an inverter terminal associated with the vehicle, whether a battery, of the first battery pack, the second battery pack, the third battery pack, or the fourth battery pack, is in a failure state, and based on a determination that the battery is in the failure state and based on individually measured insulation resistance of the first-fourth battery packs, determine a failure position of the battery.

Abstract: A wing frame includes a front wing beam extending in a left-right direction; a rear wing beam extending in the left-right direction and spaced rearward from the front wing beam, and a plurality of rib parts, each of which includes a middle rib coupled to a rear side of the front wing beam and a front side of the rear wing beam.

Abstract: A battery support body may include a bracket extending in a front-rear direction and a shock absorber, which may extend in the front-rear direction and may be coupled to the bracket in a direction crossing the front-rear direction. At least a portion of the shock absorber may be provided in the form of foam.

Abstract: Provided is a method in an electricity-driven apparatus to be driven by receiving power through a plurality of battery packs in a parallel type. The method includes detecting a state of charge (SOC) of each of the plurality of battery packs, calculating a voltage difference between the plurality of battery packs based on the detected SOC, and performing battery pack balancing based on the calculated voltage difference exceeding a threshold value. The battery pack balancing is performed by a pre-charging circuit including a balancing relay.

Abstract: The present disclosure relates to a flight control apparatus, a system including the same, and a method thereof. An example embodiment of the present disclosure provides a flight control apparatus, including: at least one processor, and memory storing instructions that, when executed by the at least one processor, cause the flight control apparatus to determine, based on environmental information and based on variations of a parameter for each operation mode of an aerial vehicle, a flight path among at least one candidate path associated with a destination for the aerial vehicle.

Abstract: The present disclosure relates to a battery pack diagnosis control apparatus, a battery system including the same, and a method thereof. An exemplary embodiment of the present disclosure provides a battery system including: at least one battery pack; a flight control apparatus configured to transmit at least one of a battery discharge mode command or a motor discharge command; a battery control apparatus configured to transmit a relay control command for a relay based on receiving the battery discharge mode command, and transmit a diagnosis command based on receiving the motor discharge command; and at least one battery pack control apparatus configured to control the relay based on receiving the relay control command, and diagnose a failure of the at least one battery pack by measuring a current of the at least one battery pack based on receiving the diagnosis command.

Abstract: An electronic device is disclosed. An electronic device comprises: a first memory in which an operating system and an application program executed on the operating system are stored; a second memory; a processor for loading at least some codes among codes corresponding to an application program from the first memory to the second memory, and when access information of the codes loaded in the second memory is received from a kernel of an operating system, accessing an area in which the loaded codes are stored, on the basis of the received information and executing the application program; and a snoop for monitoring access to an area in which a preset code, the access of which has been limited, from among codes loaded in the second memory is stored.

Abstract: An electronic device is disclosed. An electronic device comprises: a first memory in which an operating system and an application program executed on the operating system are stored; a second memory; a processor for loading at least some codes among codes corresponding to an application program from the first memory to the second memory, and when access information of the codes loaded in the second memory is received from a kernel of an operating system, accessing an area in which the loaded codes are stored, on the basis of the received information and executing the application program; and a snoop for monitoring access to an area in which a preset code, the access of which has been limited, from among codes loaded in the second memory is stored.

Abstract: A battery management system includes a battery pack, a resistive path, and a redundant resistive path. The battery pack includes a first output terminal and a second output terminal connected to a load. The redundant resistive path is between a first output terminal of the battery pack and the first outer terminal. The resistive path is between the second output terminal of the battery pack and a second output terminal. The controller is to detect overcurrent flowing through the battery pack using the redundant resistive path and the resistive path.

Abstract: An airbag for protecting passengers in a car or the like. An airbag apparatus includes an airbag mounted in a side of a vehicle and a non-inflatable curtain that is mounted in the side of the vehicle. The non-inflatable curtain may be activated by inflation gas provided by an inflator for the airbag. The non-inflatable curtain may be arranged above the airbag prior to deployment of the airbag. The airbag may be positioned closer to an interior of a vehicle than the non-inflatable curtain.

Abstract: A gas distribution pipe for balanced inflation and deployment of a side curtain airbag. The pipe has an end gas discharge opening and side gas discharge openings. The side discharge openings are configured to deflect the exiting gas so that at least a portion of the gas flows backwards along the outside of the pipe before entering the adjacent chamber of the airbag. An end cap for the pipe may contain both the end discharge opening and gas diverting and deflecting elements that direct gas to and through the side discharge openings.

Abstract: Systems and methods for folding airbags are disclosed. An airbag folding body includes a cavity having a rear wall and a top wall, the rear wall being opposite an entrance of an airbag cushion. The airbag folding body also includes a notch formed at an intersection of the top wall and the rear wall, the notch being adapted to capture, engage or secure a leading edge of the airbag cushion. The rear wall is adapted to direct the leading edge of the airbag toward the notch.

Abstract: There is provided a side airbag for an automobile having airbag modules 100, 200, 300, which selectively includes reinforcing pads, an inner cushion pad, a tube-type tether and a tear seam, all of which are piled in multi-layers, so that the side airbag may be developed with regulating the gas pressure duration without eccentricity, in a useful and effective manner to successfully protect a driver and passengers seated in the vehicle. The cushion pads used in the side airbag require a small amount of materials, are easily seamed and easily folded, so as to reduce costs.

Abstract: There is provided a side airbag for an automobile having airbag modules 100, 200, 300, which selectively includes reinforcing pads, an inner cushion pad, a tube-type tether and a tear seam, all of which are piled in multi-layers, so that the side airbag may be developed with regulating the gas pressure duration without eccentricity, in a useful and effective manner to successfully protect a driver and passengers seated in the vehicle. The cushion pads used in the side airbag require a small amount of materials, are easily seamed and easily folded, so as to reduce costs.