Abstract: In a fastener structure for a vehicle, a height adjustment spacer is interposed between first and second vehicle body frames fixed with a bolt and a nut. The nut has a first insertion hole through which a bolt is screwed, and is fixed to a surface of the first vehicle body frame. The height adjustment spacer has a second insertion hole through which the bolt is inserted, and is disposed in contact with another surface of the first vehicle body frame. The bolt is inserted through an attachment hole of the second vehicle body frame, the second insertion hole, an attachment hole of the first vehicle body frame, and the first insertion hole. On a contact surface between the height adjustment spacer and the first vehicle body frame, a protrusion and a recess are provided to surround an entirety of the second insertion hole, the second insertion hole respectively.

Abstract: A skid rail for aircrafts comprising (i) a base member comprising a long board fixed to a bottom surface of an aircraft fuselage, and bosses integrally projecting from an outer surface of the long board with longitudinal intervals, (ii) cores bonded to the long board between the bosses to form a rail-shaped, integral structure, and (iii) a skin covering the bosses and the cores, the base member and the skin being formed by a first fiber-reinforced plastic having fabrics of glass fibers and/or carbon fibers, and the cores being formed by a second fiber-reinforced plastic having fabrics of fibers having higher wear resistance than that of fibers in the first fiber-reinforced plastic.

Abstract: Plural regions are defined within a main wing by a plurality of spars and ribs. Of these regions, predetermined regions extending from a main wing connecting portion of the pylon to an internal space of a leading edge skin are used as wiring/piping accommodating chambers for collectively accommodating wiring and piping which provide communication between an engine and a fuselage, a predetermined region adjacent to parts of the wiring/piping accommodating chambers is used as a landing device accommodating chamber for accommodating a landing device and predetermined regions adjacent to other parts of the wiring/piping accommodating chambers are used as fuel tanks. Thus, the maintainability is improved as compared with the case where the wiring and the piping are distributed within the main wing. In addition, because the wiring/piping accommodating chambers are isolated from the landing device accommodating chamber and the fuel tanks, the operational reliability can be improved.

Abstract: A skid rail for aircrafts comprising (i) a base member comprising a long board fixed to a bottom surface of an aircraft fuselage, and bosses integrally projecting from an outer surface of the long board with longitudinal intervals, (ii) cores bonded to the long board between the bosses to form a rail-shaped, integral structure, and (iii) a skin covering the bosses and the cores, the base member and the skin being formed by a first fiber-reinforced plastic having fabrics of glass fibers and/or carbon fibers, and the cores being formed by a second fiber-reinforced plastic having fabrics of fibers having higher wear resistance than that of fibers in the first fiber-reinforced plastic.

Abstract: In a wing structure for an aircraft, a rib extends in a chord direction for connecting spars to each other with upper and lower stringer through holes through which stringers of skins pass being formed in upper and lower edges of the rib. A bead is formed on the rib so as to extend between the upper and lower stringer through holes. Upper and lower ends of the bead are formed into arcuate shapes so as to surround the upper and lower stringer through holes, respectively. Thus, it is possible to enhance the buckling strength of the rib against a shear load acting on the wing of the aircraft.

Abstract: Plural regions are defined within a main wing by a plurality of spars and ribs. Of these regions, predetermined regions extending from a main wing connecting portion of the pylon to an internal space of a leading edge skin are used as wiring/piping accommodating chambers for collectively accommodating wiring and piping which provide communication between an engine and a fuselage, a predetermined region adjacent to parts of the wiring/piping accommodating chambers is used as a landing device accommodating chamber for accommodating a landing device and predetermined regions adjacent to other parts of the wiring/piping accommodating chambers are used as fuel tanks. Thus, the maintainability is improved as compared with the case where the wiring and the piping are distributed within the main wing. In addition, because the wiring/piping accommodating chambers are isolated from the landing device accommodating chamber and the fuel tanks, the operational reliability can be improved.

Abstract: In a wing structure for an aircraft, a rib extends in a chord direction for connecting spars to each other with upper and lower stringer through holes through which stringers of skins pass being formed in upper and lower edges of the rib. A bead is formed on the rib so as to extend between the upper and lower stringer through holes. Upper and lower ends of the bead are formed into arcuate shapes so as to surround the upper and lower stringer through holes, respectively. Thus, it is possible to enhance the buckling strength of the rib against a shear load acting on the wing of the aircraft.

Abstract: In a wing of an airplane, a front spar having a C-shape in section includes a web, flanges, and a reinforcing partition wall. An intermediate spar having an I-shape in section includes a web, flanges, and a reinforcing partition wall. Ribs can be positioned in a span direction by coupling front and rear portions of the ribs to the reinforcing partition wall of the front spar and the reinforcing partition wall of the intermediate spar, without the provision of an assembling jig having a positioning function and without the use of a special positioning member. In addition, the ribs can be positioned in a cord direction by bringing rear ends of the ribs into abutment against a front surface of the web of the intermediate spar. Thus, it is possible to assemble the wing of the airplane using an inexpensive assembling jig having no rib-positioning function.

Abstract: In a wing of an airplane, a front spar having a C-shape in section includes a web, flanges, and a reinforcing partition wall. An intermediate spar having an I-shape in section includes a web, flanges, and a reinforcing partition wall. Ribs can be positioned in a span direction by coupling front and rear portions of the ribs to the reinforcing partition wall of the front spar and the reinforcing partition wall of the intermediate spar, without the provision of an assembling jig having a positioning function and without the use of a special positioning member. In addition, the ribs can be positioned in a cord direction by bringing rear ends of the ribs into abutment against a front surface of the web of the intermediate spar. Thus, it is possible to assemble the wing of the airplane using an inexpensive assembling jig having no rib-positioning function.

Abstract: A plasticizing apparatus used for a pre-plasticization-type injection molding machine is equipped with a screw drive section which comprises a rotational drive section supported in an axially moveable manner and adapted to rotate the screw; and an advancement/retraction drive section including a servomotor and a ball-screw mechanism for converting rotational motion of the servomotor to linear motion in order to axially move the rotational drive section. By virtue of the above-described structure, the screw disposed within the barrel is rotated by the rotational drive section of the screw drive section, so that the molding material within the barrel is plasticized (melted) and is then supplied to the injection apparatus. Further, the rotational drive section (screw) is advanced and retracted by the advancement/retraction section of the screw drive section, so that the resin passage of the barrel is opened and closed in accordance with the position of the screw.

Abstract: Disk removing device uses its disk pickup arm to remove or take out, from an injection mold unit, a disk having been molded by the mold unit. The disk removing device includes a rotary motor for rotating the disk pickup arm, and an arm support shaft which has the disk pickup arm at its distal end portion and which is rotated, together with the arm, by the rotary motor. The arm support shaft is coupled at its other end to a linear shaft of a linear motor so that the rotary and linear motors are coupled with each other in series via the arm support shaft. The disk removing device also includes a bearing member rotatable by the rotary motor, and the arm support shaft is supported by the bearing member for rotation and axial sliding movement relative to the bearing member. Such arrangements can effectively reduce the necessary number of component parts and overall size of the disk removing device, and thus the disk removing device can be installed snugly in a small space.

Abstract: A plasticizing apparatus used for a pre-plasticization-type injection molding machine is equipped with a screw drive section which comprises a rotational drive section supported in an axially moveable manner and adapted to rotate the screw; and an advancement/retraction drive section including a servomotor and a ball-screw mechanism for converting rotational motion of the servomotor to linear motion in order to axially move the rotational drive section. By virtue of the above-described structure, the screw disposed within the barrel is rotated by the rotational drive section of the screw drive section, so that the molding material within the barrel is plasticized (melted) and is then supplied to the injection apparatus. Further, the rotational drive section (screw) is advanced and retracted by the advancement/retraction section of the screw drive section, so that the resin passage of the barrel is opened and closed in accordance with the position of the screw.

Abstract: Disk removing device uses its disk pickup arm to remove or take out, from an injection mold unit, a disk having been molded by the mold unit. The disk removing device includes a rotary motor for rotating the disk pickup arm, and an arm support shaft which has the disk pickup arm at its distal end portion and which is rotated, together with the arm, by the rotary motor. The arm support shaft is coupled at its other end to a linear shaft of a linear motor so that the rotary and linear motors are coupled with each other in series via the arm support shaft. The disk removing device also includes a bearing member rotatable by the rotary motor, and the arm support shaft is supported by the bearing member for rotation and axial sliding movement relative to the bearing member. Such arrangements can effectively reduce the necessary number of component parts and overall size of the disk removing device, and thus the disk removing device can be installed snugly in a small space.