Abstract:
PROBLEM TO BE SOLVED: To provide a flux composition which does not cause brazing failure or discoloration even when being brazed under either a high oxygen concentration atmosphere or a high humidity atmosphere.SOLUTION: A brazing method of an aluminum alloy executes a flux coating processing which coats a flux component on a surface of an aluminum alloy member, and executes a brazing and heating processing which brazes and heats the flux component coated aluminum alloy member. The flux component is (A) a fluoro zinc alkali aluminate metal salt powder represented by a general formula (1): MZnAlF(1), and the amount of coating of (A) on the aluminum alloy member in the flux coating processing is 1-50 g/m. In the formula, M is K or Cs, w, x, y, z are positive integers, and the greatest common divisor thereof is 1.)
Abstract translation:要解决的问题:提供即使在高氧浓度气氛或高湿度气氛下进行钎焊也不会引起钎焊破坏或变色的焊剂组合物。解决方案:铝合金的钎焊方法执行焊剂涂布处理,其中 在铝合金构件的表面上涂布助焊剂组分,并且执行钎焊和加热助焊剂组分涂覆的铝合金构件的钎焊和加热处理。 助熔剂组分是(A)由通式(1)表示的氟锌碱金属铝盐粉末:MZnAlF(1),助熔剂处理中铝合金构件上的(A)涂层量为1 -50 g / m。 在公式中,M是K或Cs,w,x,y,z是正整数,其最大公约数是1)
Abstract:
PROBLEM TO BE SOLVED: To provide a shaped member which is capable of being manufactured in low cost and has excellent dimensional accuracy, excellent axial pressure crush characteristics and three-point bending characteristics, or excellent flexural rigidity and torsional stiffness, and is thus favorably applicable to an automobile constitution member.SOLUTION: A shaped member 20 includes a reinforcement member 35 joined at a welding portion provided in a ridge line section 28. A planar blank and the reinforcement member 35 are joined together at the welding portion, and are formed by bending so that the welding portion serves as the ridge line section 28.
Abstract:
A method for aligning an elongated component that is to be fitted, with at least two component segments, into two coaxial installation points (A/B; C) spaced apart from one another. In this context, the coaxiality of the component segments is checked and any existing deviation from coaxiality is measured. At least one material fusion area, limited radially and in a circumferential direction, is generated in a surface region of the component located between the component segments, at a magnitude such that as a result of the axial shrinkage ensuing upon cooling of the material fusion area, coaxiality of the component segments is produced at least within tolerable limits.
Abstract:
PROBLEM TO BE SOLVED: To provide a member welding structure that can decrease the amount of heat input and suppress deformation of the welded section.SOLUTION: A welding structure 3 is of a first member (floor member 30) including an extruded profile and a second member (support frame 50) welded to the first member, and is characterized by the first member having a contacted section 80 at which the second member contacts, and a facing section 81 formed at the end of the contacted section 80, the second member having an abutted section 90 abutted to the facing section 81, and the facing section 81 and abutted section 90 being abutted and welded. The facing section 81 preferably extends in the direction of extrusion of the extruded profile. Also, an expansion section 82 is preferably formed at the rear side of the plate section (bottom plate section 34) of the first member at the position at which the facing section 81 and the abutted section 90 are abutted and welded.
Abstract:
PROBLEM TO BE SOLVED: To enhance the strength of a joint in a side member structure in which a front side member having a U-shaped cross section opened upward and a rear side member having a cross section opened sideways are coupled through a reinforcement.SOLUTION: A reinforcement 20 has a reinforcement bottom 20a and a pair of right and left reinforcement sides 20b, 20c extending out of the side edge of the reinforcement bottom 20a. The reinforcement 20 is coupled with the front side member and the rear side member in an upward posture opened upward while being astride the front side member 3 and the rear side member 4 so as to compensate for discontinuity V on a ridge line formed in a joint J between the front side member 3 and the rear side member 4.