Abstract: A support system for use with an aircraft or vehicle capable of hovering. The support system includes a detecting portion provided outside an airframe and configured to detect a target object that may become an obstacle; an imaging portion configured to take an image of surroundings of the aircraft; a data processing portion; a display portion and the like. The data processing portion acquires data from the detecting portion and an avionics system. The data processing portion uses the acquired data to generate target object schematic image data indicating approach of the target object or possibility of the approach of the target object and outputs the target object schematic image data to the display portion. The display portion displays an obstacle state display image based on the target object schematic image data, the obstacle state display image schematically showing a state of the obstacle around the aircraft.

Abstract: A mount board has a plurality of terminals electrically connected to a plurality of pins of a semiconductor device, and a conductor pattern. An electrostatic withstand voltage test device includes a metal plate on which the mount board is installed, a power supply for applying a voltage to the metal plate, an insulator disposed between the metal plate and the mount board, a switch circuit connected between the terminals and ground wiring, and a controller for controlling the switch circuit. The switch circuit includes a plurality of first switches provided corresponding to the terminals and each connecting a corresponding terminal to the ground wiring. The controller turns on at least one first switch selected from the first switches when an electric charge stored in the conductor pattern is discharged to the ground wiring through the semiconductor device.

Abstract: A support system for use with an aircraft or vehicle capable of hovering. The support system includes a detecting portion provided outside an airframe and configured to detect a target object that may become an obstacle; an imaging portion configured to take an image of surroundings of the aircraft; a data processing portion; a display portion and the like. The data processing portion acquires data from the detecting portion and an avionics system. The data processing portion uses the acquired data to generate target object schematic image data indicating approach of the target object or possibility of the approach of the target object and outputs the target object schematic image data to the display portion. The display portion displays an obstacle state display image based on the target object schematic image data, the obstacle state display image schematically showing a state of the obstacle around the aircraft.

Abstract: A support system for use with an aircraft or vehicle capable of hovering. The support system includes a detecting portion provided outside an airframe and configured to detect a target object that may become an obstacle; an imaging portion configured to take an image of surroundings of the aircraft; a data processing portion; a display portion and the like. The data processing portion acquires data from the detecting portion and an avionics system. The data processing portion uses the acquired data to generate target object schematic image data indicating approach of the target object or possibility of the approach of the target object and outputs the target object schematic image data to the display portion. The display portion displays an obstacle state display image based on the target object schematic image data, the obstacle state display image schematically showing a state of the obstacle around the aircraft.

Abstract: A support system for use with an aircraft or vehicle capable of hovering. The support system includes a detecting portion provided outside an airframe and configured to detect a target object that may become an obstacle; an imaging portion configured to take an image of surroundings of the aircraft; a data processing portion; a display portion and the like. The data processing portion acquires data from the detecting portion and an avionics system. The data processing portion uses the acquired data to generate target object schematic image data indicating approach of the target object or possibility of the approach of the target object and outputs the target object schematic image data to the display portion. The display portion displays an obstacle state display image based on the target object schematic image data, the obstacle state display image schematically showing a state of the obstacle around the aircraft.

Abstract: A tubular cover is obtained by causing a fabric woven from a warp and weft to be imparted with a curl by a heat treatment, wherein the tubular cover is characterized in that the warp and/or the weft are folded yarns created by twisting together multiple strands of yarn that have already been twisted in either an S- or Z-winding-direction, the winding direction of the twisting when the folded yarn is created being the opposite of the yarn-winding direction.

Abstract: A tubular cover is obtained by causing a fabric woven from a warp and weft to be imparted with a curl by a heat treatment, wherein the tubular cover is characterized in that the warp and/or the weft are folded yarns created by twisting together multiple strands of yarn that have already been twisted in either an S- or Z-winding-direction, the winding direction of the twisting when the folded yarn is created being the opposite of the yarn-winding direction.

Abstract: A molded case houses switching parts and includes a case main body and a cover placed on an upper portion of the case main body. The case main body includes a bottom portion case that forms a bottom portion of a circuit breaker and an intermediate case, placed on an upper portion of the bottom portion case, having a dividing wall that blocks off a space between the intermediate case and the bottom portion case. A power source side terminal block and second movable contact are fitted inside the bottom portion case, and a first movable contact, the load side terminal block, the contact portion, and the arc extinguishing chamber are fitted inside the intermediate case.

Abstract: A molded case housing each part is configured of a case main body (54) and a cover (55) placed on an upper portion of the case main body, the case main body (54) is configured of a bottom portion case (56) that forms a bottom portion of a circuit breaker and an intermediate case (57), placed on an upper portion of the bottom portion case, having a dividing wall that blocks off a space between the intermediate case and the bottom portion case. A power source side terminal block (3) and second movable contact (4) are fitted inside the bottom portion case, and a first movable contact (5), the load side terminal block (9), the contact portion (52), and the arc extinguishing chamber (6) are fitted inside the intermediate case.