Abstract: To provide a heater chip which is excellent in energization heat generation characteristic of the ironing portion thereof, and which can efficiently and stably perform a joining process of joining a conducting thin wire to a terminal member. The heater chip comprises an ironing portion located at the lowermost position in a posture of a normal use mode and a pair of connection terminal portions and formed integrally with the ironing portion and extending symmetrically or asymmetrically upward from a left and a right ends of the ironing portion. The ironing portion has a cross-sectional area equal to or smaller than the cross-sectional areas of the connection terminal portions and on the path of a current flowing in the heater chip when energized. A concave portion is formed on one side face of the ironing portion. A thermocouple is attached to the back face of the ironing portion through a protrusion.

Abstract: Provided is a decorative sheet (100) including: a transmissive substrate (10) which is sheet-like or plate-like; a light reflective projection portion (20) formed over the light transmissive substrate (10); and a black layer (30) formed over the light reflective projection portion (20), in which an average height of the light reflective projection portions (20) is 1 to 200 pm, and the black layer (30) is formed by using a black ink satisfying conditions below.

Abstract: Provided is a decorative sheet (100) including: a transmissive substrate (10) which is sheet-like or plate-like; a light reflective projection portion (20) formed over the light transmissive substrate (10); and a black layer (30) formed over the light reflective projection portion (20), in which an average height of the light reflective projection portions (20) is 1 to 200 ?m, and the black layer (30) is formed by using a black ink satisfying conditions below. [Conditions] In a dried coated film which is formed using the black ink by a film forming method below, a gloss value of a surface of the dried coated film, which is measured at a measurement angle of 60° in accordance with JIS Z 8741 (1997) is equal to or more than 80 and a lightness L* value of the surface of the dried coated film in the CIE 1976 (L*, a*, and b*) color system, which is measured by an SCE method is equal to or less than 10.

Abstract: A flight path setting apparatus includes a display unit, a selector, a range calculator, and a display controller. The display unit displays a flight path of an aircraft. The flight path includes a plurality of points. The selector selects a first point on the basis of an operation performed by a user. The first point is any one of the points displayed by the display unit. The range calculator calculates a non-settable range on the basis of a flight performance and a surrounding environment of the aircraft. The non-settable range is a region that is around the first point and in which a second point is not settable. The second point is subsequent to the first point on the flight path. The display controller causes the display unit to display the non-settable range that relates to the first point and is calculated by the range calculator.

Abstract: A formation setting apparatus includes a display unit, a selector, a region calculator, a display controller, and a communication controller. The display unit displays a formation of formation flying that includes aircrafts. The selector selects, as a first aircraft, one of the aircrafts displayed on the display unit, on a basis of an operation performed by a user. The region calculator calculates a movable region of the first aircraft, on a basis of a distance, to the first aircraft, from one or a plurality of second aircrafts of the aircrafts excluding the first aircraft. The display controller causes the calculated movable region to be displayed on the display unit. The communication controller transmits a control signal to the first aircraft when a position within the movable region displayed on the display unit is selected by the user. The control signal causes the first aircraft to move to the selected position.

Abstract: A surface-emitting laser includes an active layer on which a spacer layer is disposed, and a reflection mirror disposed on the spacer layer, including a current constriction layer that is a selectively-oxidized layer having been selectively oxidized. The current constriction layer is disposed at a position of a node of a standing-wave of an electric field of light oscillated at the active layer and is disposed away from an interface between the spacer layer and the reflection mirror by an optical distance of one-fourth of an oscillation wavelength at the active layer. The selectively-oxidized layer is made of AlGaAs. The reflection mirror includes at least one AlGaInP layer contacting the selectively-oxidized layer.

Abstract: To provide a heater chip which is excellent in energization heat generation characteristic of the ironing portion thereof, and which can efficiently and stably perform a joining process of joining a conducting thin wire to a terminal member. The heater chip comprises an ironing portion located at the lowermost position in a posture of a normal use mode and a pair of connection terminal portions and formed integrally with the ironing portion and extending symmetrically or asymmetrically upward from a left and a right ends of the ironing portion. The ironing portion has a cross-sectional area equal to or smaller than the cross-sectional areas of the connection terminal portions and on the path of a current flowing in the heater chip when energized. A concave portion is formed on one side face of the ironing portion. A thermocouple is attached to the back face of the ironing portion through a protrusion.

Abstract: A flight path setting apparatus includes a display unit, a selector, a range calculator, and a display controller. The display unit displays a flight path of an aircraft. The flight path includes a plurality of points. The selector selects a first point on the basis of an operation performed by a user. The first point is any one of the points displayed by the display unit. The range calculator calculates a non-settable range on the basis of a flight performance and a surrounding environment of the aircraft. The non-settable range is a region that is around the first point and in which a second point is not settable. The second point is subsequent to the first point on the flight path. The display controller causes the display unit to display the non-settable range that relates to the first point and is calculated by the range calculator.

Abstract: A formation setting apparatus includes a display unit, a selector, a region calculator, a display controller, and a communication controller. The display unit displays a formation of formation flying that includes aircrafts. The selector selects, as a first aircraft, one of the aircrafts displayed on the display unit, on a basis of an operation performed by a user. The region calculator calculates a movable region of the first aircraft, on a basis of a distance, to the first aircraft, from one or a plurality of second aircrafts of the aircrafts excluding the first aircraft. The display controller causes the calculated movable region to be displayed on the display unit. The communication controller transmits a control signal to the first aircraft when a position within the movable region displayed on the display unit is selected by the user. The control signal causes the first aircraft to move to the selected position.

Abstract: A surface-emitting laser includes an active layer on which a spacer layer is disposed, and a reflection mirror disposed on the spacer layer, including a current constriction layer that is a selectively-oxidized layer having been selectively oxidized. The current constriction layer is disposed at a position of a node of a standing-wave of an electric field of light oscillated at the active layer and is disposed away from an interface between the spacer layer and the reflection mirror by an optical distance of one-fourth of an oscillation wavelength at the active layer. The selectively-oxidized layer is made of AlGaAs. The reflection mirror includes at least one AlGaInP layer contacting the selectively-oxidized layer.

Abstract: A surface-emitting laser includes a plurality of semiconductor layers; an active layer; and spacer layers, between which the active layer is held. The active layer includes a first layer including aluminum gallium indium arsenide ((AlxGa1-x)yIn1-yAs, where x and y are greater than or equal to zero but less than one), and a second layer including aluminum gallium indium arsenide ((AlmGa1-m)nIn1-nAs, where m and n are greater than or equal to zero but less than one, and at least one of m-x and n-y is not zero). The spacer layers includes aluminum gallium indium phosphide ((AlaGa1-a)bIn1-bP, where a and b are greater than or equal zero but less than one). The plurality of semiconductor layers and the active layer held between the spacer layers are laminated.

Abstract: A urea spray selective catalytic reduction (“SCR”) control system includes an SCR catalyst provided in a discharge pipe of an engine, a dosing valve for injecting urea water at an upstream side of the SCR catalyst, and NOx sensors, wherein the system controls injection of the urea water from the dosing valve. The system includes a plurality of NOx model maps corresponding to an atmospheric pressure condition, an outdoor air temperature, and an engine water temperature, and determines an amount of NOx from each NOx model map on a basis of detection values of an atmospheric pressure detector, an outdoor air temperature detector, and an engine water temperature detector, and controls an amount of injection of the urea water from the dosing valve on a basis of the amount of NOx thus determined.