Patent classifications
B21D47/00
HONEYCOMB, IN PARTICULAR DEFORMABLE HONEYCOMB, FOR LIGHTWEIGHT COMPONENTS, CORRESPONDING PRODUCTION METHOD, AND SANDWICH COMPONENT
A honeycomb for curved surface lightweight components includes a plurality of elongate ribbons and connecting regions. The connecting regions are provided, respectively, between opposing ribbons to connect the ribbons together in a portion-wise manner in a firmly bonded relationship in a transverse direction. The connecting regions are arranged at regular spacings along the longitudinal direction of a ribbon. Honeycomb-like cells form cavities between the ribbons. With respect to three successive ribbons, a displacement of the connecting regions between first and second ribbons relative to the connecting regions between second and third ribbons toward a first side of the longitudinal direction is lesser than toward a second side of the longitudinal direction. Consequently, at least a part of the cells in cross-section in the longitudinal direction/transverse direction plane have at least one longer limb corresponding to the greater displacement and at least one shorter limb corresponding to the lesser displacement.
HONEYCOMB, IN PARTICULAR DEFORMABLE HONEYCOMB, FOR LIGHTWEIGHT COMPONENTS, CORRESPONDING PRODUCTION METHOD, AND SANDWICH COMPONENT
A honeycomb for curved surface lightweight components includes a plurality of elongate ribbons and connecting regions. The connecting regions are provided, respectively, between opposing ribbons to connect the ribbons together in a portion-wise manner in a firmly bonded relationship in a transverse direction. The connecting regions are arranged at regular spacings along the longitudinal direction of a ribbon. Honeycomb-like cells form cavities between the ribbons. With respect to three successive ribbons, a displacement of the connecting regions between first and second ribbons relative to the connecting regions between second and third ribbons toward a first side of the longitudinal direction is lesser than toward a second side of the longitudinal direction. Consequently, at least a part of the cells in cross-section in the longitudinal direction/transverse direction plane have at least one longer limb corresponding to the greater displacement and at least one shorter limb corresponding to the lesser displacement.
Stabilizer
A stabilizer formed by using a metal bar having a solid structure and configured to reduce a displacement between right and left wheels, including a torsion part extending in a vehicle width direction, being capable of a torsional deformation, and having a diameter of 10 to 32 mm, is provided. The stabilizer has a chemical composition containing at least C: 0.15% by mass or more to 0.39% by mass or less, Mn, B, and Fe, and also has a metal structure 90% or more of which is a martensite structure.
Stabilizer
A stabilizer formed by using a metal bar having a solid structure and configured to reduce a displacement between right and left wheels, including a torsion part extending in a vehicle width direction, being capable of a torsional deformation, and having a diameter of 10 to 32 mm, is provided. The stabilizer has a chemical composition containing at least C: 0.15% by mass or more to 0.39% by mass or less, Mn, B, and Fe, and also has a metal structure 90% or more of which is a martensite structure.
Method and die set for forming a surface in a metal panel
A die set for forming a panel having a surface includes a stationary die, a moveable die, and a clamp attached to the stationary die to secure a panel blank. The moveable die includes a moveable brazing formation surface and the stationary die includes a stationary brazing formation surface for forming the surface. One of the moveable and stationary dies includes a male bead forming portion, and the other includes a female bead forming portion for forming a bead. The male and female bead forming portions extend in a continuous and uninterrupted, generally parallel relationship with the moveable and stationary brazing formation surfaces. The male and female bead forming portions are operable to engage the panel blank during movement of the moveable die to induce tensile forces in both a first direction parallel to a path of the surface and a second direction transverse to the path.
Method and die set for forming a surface in a metal panel
A die set for forming a panel having a surface includes a stationary die, a moveable die, and a clamp attached to the stationary die to secure a panel blank. The moveable die includes a moveable brazing formation surface and the stationary die includes a stationary brazing formation surface for forming the surface. One of the moveable and stationary dies includes a male bead forming portion, and the other includes a female bead forming portion for forming a bead. The male and female bead forming portions extend in a continuous and uninterrupted, generally parallel relationship with the moveable and stationary brazing formation surfaces. The male and female bead forming portions are operable to engage the panel blank during movement of the moveable die to induce tensile forces in both a first direction parallel to a path of the surface and a second direction transverse to the path.
HIGH-STRENGTH METAL PLATE FOR VEHICLES
A high-strength metal plate for vehicles is provided. The plate includes oval embossments that protrude from the plate. The embossments include first embossments that have a longer axis oriented in a first direction and second embossments that have a longer axis in a second direction. Bridges are provided on portions of the flat plate between the embossments and flat portions are provided on the flat plate to be surrounded by the first and second embossments while the bridges separate the flat portions from each other.
ISOGRID PATTERNS FOR STRUCTURAL AIRCRAFT PANELS
One embodiment includes a structural panel for an aerospace vehicle, including a single sheet of material, the material having a first raised pattern on a first side, and a second raised pattern on a reverse side, wherein a repeating portion of the first raised pattern is substantially identical in size and shape to a repeating portion of the second raised pattern, and is rotated at an angle θ to the first raised pattern.
ISOGRID PATTERNS FOR STRUCTURAL AIRCRAFT PANELS
One embodiment includes a structural panel for an aerospace vehicle, including a single sheet of material, the material having a first raised pattern on a first side, and a second raised pattern on a reverse side, wherein a repeating portion of the first raised pattern is substantially identical in size and shape to a repeating portion of the second raised pattern, and is rotated at an angle θ to the first raised pattern.
PROCESSING DEVICE, AND METHOD FOR CONTROLLING PROCESSING DEVICE
A processing device processes a frame-shaped workpiece which extends in a prescribed extension direction, and includes, integrally, a plate-shaped web surface portion, a plate-shaped first flange portion that bends and extends from one end of the web surface portion, and a plate-shaped second flange portion which bends from the other end of the web surface portion and extends in the opposite direction to the first flange portion. The processing device includes a shaping device which conveys the workpiece in the extension direction, and an exit side pinch roll device provided further downstream, in the workpiece conveying flow direction, than the shaping device. The exit side pinch roll device includes a first roll which presses a central region of an upper surface side of the web surface portion, and a second roll which presses a central region of a lower surface side of the web surface portion.