Abstract: A secondary battery includes: a can having an accommodation space therein; an electrode assembly accommodated in the accommodation space in the can; and a cap assembly sealed with the can. The can has a beading part recessed into a side wall of the can at a region below where the cap assembly is accommodated, and the beading part has an acute angle with respect to the side wall of the can.

Abstract: A lens includes a lens unit; an intermediate layer configured to cover a surface portion of the lens unit; and a water-repellent layer, configured to cover a surface portion of the intermediate layer, including a base layer and an ultraviolet (UV) absorber disposed in the base layer.

Abstract: An oxygen supply apparatus and method for a fuel cell of an aircraft are provided. The oxygen supply apparatus includes a compressor that generates compressed air by compressing air in the atmosphere and supplies the compressed air to a fuel cell stack, an oxygen tank having a predetermined amount of oxygen stored therein. An aircraft monitoring device monitors the aircraft and determines whether oxygen supply from the oxygen tank is required, and an oxygen supply means switching device switches an oxygen supply means for the fuel cell stack from the compressor to the oxygen tank, or vice versa depending on an outcome of the monitoring.

Abstract: An embodiment flat fuel cell device includes a fuel cell comprising a cell stack in which a plurality of unit cells is stacked, a junction box electrically connected to the fuel cell, an air-processing device configured to manage inflow and outflow of air containing oxygen between an outside and the fuel cell, and a hydrogen-processing device configured to manage inflow and outflow of hydrogen to and from the fuel cell. Each of the junction box, the air-processing device, and the hydrogen-processing device is disposed so as to be contiguous with the fuel cell in a horizontal direction.

Abstract: An embodiment apparatus for complementing a braking force of a vehicle includes a driving unit configured to drive an autonomous drone, a braking complement system connected with the driving unit and configured to complement the braking force, and a controller configured to determine a braking complement condition of the vehicle and to drive the braking complement system based on the braking complement condition. An embodiment braking complement system includes a compressor, wherein the driving unit is configured to apply an electric driving force to the compressor, an air tank in which compressed air discharged from the compressor is stored, and a braking complement unit connected with a discharge end of the air tank.

Abstract: An oxygen supply apparatus and method for a fuel cell of an aircraft are provided. The oxygen supply apparatus includes a compressor that generates compressed air by compressing air in the atmosphere and supplies the compressed air to a fuel cell stack, an oxygen tank having a predetermined amount of oxygen stored therein. An aircraft monitoring device monitors the aircraft and determines whether oxygen supply from the oxygen tank is required, and an oxygen supply means switching device switches an oxygen supply means for the fuel cell stack from the compressor to the oxygen tank, or vice versa depending on an outcome of the monitoring.

Abstract: The present invention provides a busbar comprising terminals, a body connected to the terminals and includes a plurality of blades, wherein the body includes an inner body, an outer body, and connecting parts, the outer body is disposed outside the inner body, the connecting parts are arranged in a periphery of the inner body at regular intervals and connect the inner body to the outer body, the terminals are disposed in the inner body so that connection ends of the terminals are disposed between the adjacent connecting parts, the plurality of blades protrude from an upper surface of the outer body and are arranged in a circumferential direction with respect to a center of the busbar, the outer body includes a cooling hole formed to pass through from a lower surface thereof to the upper surface, and the cooling hole is disposed between adjacent blades, thereby providing an advantageous effect of reducing the number of parts to be manufactured such that manufacturing costs and manufacturing processes can be re

Abstract: The present invention provides a busbar comprising terminals, a body connected to the terminals and includes a plurality of blades, wherein the body includes an inner body, an outer body, and connecting parts, the outer body is disposed outside the inner body, the connecting parts are arranged in a periphery of the inner body at regular intervals and connect the inner body to the outer body, the terminals are disposed in the inner body so that connection ends of the terminals are disposed between the adjacent connecting parts, the plurality of blades protrude from an upper surface of the outer body and are arranged in a circumferential direction with respect to a center of the busbar, the outer body includes a cooling hole formed to pass through from a lower surface thereof to the upper surface, and the cooling hole is disposed between adjacent blades, thereby providing an advantageous effect of reducing the number of parts to be manufactured such that manufacturing costs and manufacturing processes can be re

Abstract: The present invention provides a rotor assembly comprising: a rotor including a core body, and a plurality of protrusion parts coupled to the core body so as to be detachable therefrom; and an insulator including a body encompassing the protrusion parts, and blades formed to protrude from the upper and lower surfaces of the body, thereby providing an advantageous effect of reducing the number of parts to be manufactured such that manufacturing costs and manufacturing processes can be reduced.

Abstract: The present invention provides a rotor assembly comprising: a rotor including a core body, and a plurality of protrusion parts coupled to the core body so as to be detachable therefrom; and an insulator including a body encompassing the protrusion parts, and blades formed to protrude from the upper and lower surfaces of the body, thereby providing an advantageous effect of reducing the number of parts to be manufactured such that manufacturing costs and manufacturing processes can be reduced.

Abstract: An apparatus for improving the aerodynamic characteristics of a vehicle includes a first vane configured to be rotatable on a wheel guard. An actuator is configured to provide the first vane with rotational force so as to rotate the first vane. A controller is configured to receive vehicle speed information and steering angle information of a steering wheel, and to control the operation of the actuator.

Abstract: An apparatus for improving the aerodynamic characteristics of a vehicle includes a first vane configured to be rotatable on a wheel guard. An actuator is configured to provide the first vane with rotational force so as to rotate the first vane. A controller is configured to receive vehicle speed information and steering angle information of a steering wheel, and to control the operation of the actuator.

Abstract: Embodiments relate to an image sensor and a method of manufacturing an image sensor. According to embodiments, an image sensor may include a gate over a semiconductor substrate, a first impurity region over the semiconductor substrate, a second impurity region over the semiconductor substrate, the second impurity region being shallower than the first impurity region, and a third impurity region formed in the first impurity region, and bent toward the gate at a predetermined angle. According to embodiments, the third impurity region may be an n-type impurity region. According to embodiments, an area of a photodiode may be increased and a transfer efficiency of electrons generated from a photodiode may be increased.

Abstract: A complementary metal oxide semiconductor (CMOS) image sensor (CIS) and a method for fabricating the same. A method for fabricating a CIS includes implanting first conductive type dopants in a semiconductor substrate to form a photodiode region in a surface of the semiconductor substrate, implanting second conductive type dopants in the photo diode region to form a second conductive type diffusion region, and implanting fluorine ions in the second conductive type diffusion region to form a fluorine diffusion region.

Abstract: Disclosed are a CMOS image sensor and a manufacturing method thereof.

Abstract: Disclosed are a CMOS image sensor and a manufacturing method thereof.

Abstract: Embodiments relate to an image sensor and a method of manufacturing an image sensor. According to embodiments, an image sensor may include a gate over a semiconductor substrate, a first impurity region over the semiconductor substrate, a second impurity region over the semiconductor substrate, the second impurity region being shallower than the first impurity region, and a third impurity region formed in the first impurity region, and bent toward the gate at a predetermined angle. According to embodiments, the third impurity region may be an n-type impurity region. According to embodiments, an area of a photodiode may be increased and a transfer efficiency of electrons generated from a photodiode may be increased.

Abstract: Embodiments relate to a CMOS image sensor. In embodiments, the CMOS image sensor may include a semiconductor substrate, a photodiode, a first conduction type impurity region, a first insulating layer, a conduction layer, and a second insulating layer. The semiconductor substrate may have a trench in which a device isolation layer is to be formed. The photodiode may be formed in an active region of the semiconductor substrate, and the first conduction type impurity region may be formed in sidewalls of the trench. The first insulating layer may be formed inside the trench, and a conduction layer may be formed inside the trench and doped with second conduction type impurities. A second insulating layer may be formed inside the trench.

Abstract: A method for fabricating a Complementary Metal Oxide Semiconductor (CMOS) image sensor includes implanting first conductive type dopants into a semiconductor substrate and forming a photodiode region in a surface of the semiconductor substrate, performing spike annealing to the semiconductor substrate having the photodiode region formed thereon, to thereby suppress diffusion of the first conductive type dopants and remove an interstitial between lattices, and implanting second conductive type dopants into an upper part of the photo diode region to form a second conductive type diffusion region.

Abstract: A complementary metal oxide semiconductor (CMOS) image sensor (CIS) and a method for fabricating the same. A method for fabricating a CIS includes implanting first conductive type dopants in a semiconductor substrate to form a photodiode region in a surface of the semiconductor substrate, implanting second conductive type dopants in the photo diode region to form a second conductive type diffusion region, and implanting fluorine ions in the second conductive type diffusion region to form a fluorine diffusion region.