Semi-hollow self-punching riveting screw with fastening thread and self-punching riveting equipment and method
A self-piercing riveting and thread tightening technology, applied in the directions of screws, rivets, mechanical equipment, etc., can solve the problems of rivet fracture failure, high cost, inapplicability, etc., to improve the material forming performance, simple structure, easy to process and manufacture Effect
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[0039] Example 1
[0040] Such as image 3 As shown, the upper sheet 4 used in this embodiment is a layer of 2mm thick 6061-T6 aluminum alloy, and the lower sheet 5 is a layer of 3mm thick Q235 low carbon steel and a layer of 4mm thick carbon fiber sheet. The total thickness of the sheet is 9mm. The yield strength of 6061-T6 aluminum alloy is 200-230Mpa, the tensile strength is 340-380Mpa, the yield strength of Q235 steel is 230-240Mpa, and the tensile strength is 370-500Mpa.
[0041] 6061-T6 aluminum alloy and Q235 low carbon steel can achieve better self-piercing riveting forming at room temperature. Q235 with better plasticity is placed in the middle as the lower plate 5, and 6061-T6 aluminum alloy is placed in the upper layer, which is realized after positioning and clamping. For riveting, the carbon fiber sheet is not suitable for riveting due to its poor plasticity. Therefore, it is used as the uppermost sheet after pre-punching. After the riveting is completed, the threaded...
Example Embodiment
[0042] Example 2
[0043] Such as image 3 As shown, the upper plate 4 and the lower plate 5 used in this embodiment are both 2mm thick 7075-T6 high-strength aluminum alloy, and a layer of 6mm thick high-strength steel plate, the total thickness of the plate is 10mm, of which 7075-T6 aluminum alloy The yield strength is 480-520Mpa, and the tensile strength is 630-670Mpa; the yield strength of high-strength steel plate is 800-900Mpa, and the tensile strength is 1200-1300Mpa.
[0044] 7075-T6 aluminum alloy cannot be riveted and formed at room temperature, so heat treatment is performed first to improve the formability of the material.
[0045] First, the double-layer 7075-T6 aluminum alloy sheet to be riveted is heated and solution treated, the solution temperature is 470-480℃, and the holding time is 25-35min. 7075 aluminum alloy has better formability at about 400℃, so solution treatment After the completion, when the 7075 aluminum alloy is cooled to 380-410°C, the self-piercing r...
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