| Light-Duty Wide-Spreading Tri-Fold Rivet | Nominal diameter: 3.2 mm Typical grip range: 1.0–3.2 mm | Thin glass-fiber or carbon-fiber laminate panels, interior covers, light guards, and non-structural trim. | Use a drilled hole only slightly larger than the rivet diameter, commonly about 3.3–3.4 mm for a 3.2 mm rivet. Confirm the laminate thickness before ordering. | Three formed legs spread the clamp load over a larger area than a standard blind rivet, reducing the risk of pull-through in thin sheet composites. | Inspect for loose heads, cracked laminate, water ingress, and corrosion staining during scheduled panel inspections. Replace any rivet with a distorted or incomplete fold. | Do not use it for primary structural joints without engineering approval. A frequent mistake is selecting the rivet by diameter alone while ignoring the actual grip range. |
| General-Purpose Medium-Grip Aluminium Tri-Fold Rivet | Nominal diameter: 4.0 mm Typical grip range: 1.5–4.8 mm | Equipment enclosures, access panels, composite fairings, and moderate-duty attachments where the rear side is inaccessible. | Common hole size is approximately 4.1–4.2 mm for a 4.0 mm rivet. Select a body length that places the material stack inside the manufacturer’s stated grip range. | Offers a practical balance of installation speed, broad load distribution, and low assembly weight. Aluminium bodies are generally easy to drill out during repairs. | Check the joint after the first service cycle because bedding-in can reduce clamp consistency. Keep the joint dry and seal exposed holes when moisture could reach the laminate core. | Do not clamp a core or laminate stack beyond the rated grip range. Over-gripping can prevent proper leg formation and leave a weak, loose joint. |
| Long-Grip Tri-Fold Rivet for Sandwich Panels | Nominal diameter: 4.8 mm Typical grip range: 3.0–6.4 mm | Honeycomb or foam-core sandwich panels with a thicker total stack, provided the local area has suitable face-sheet reinforcement. | Typical hole size is about 4.9–5.0 mm for a 4.8 mm rivet. Measure both face sheets, adhesive layers, washers, and any backing components when calculating grip. | Useful where a longer body is required and where the tri-fold legs can distribute load behind a relatively thin face sheet. | Inspect the surrounding face sheet for crushing, delamination, or moisture damage. If the panel has a soft or open core, use an approved core-filling or edge-sealing procedure before riveting. | A major mistake is treating the nominal panel thickness as the grip length without accounting for washers or reinforcement. Never allow the legs to form inside an unsupported void. |
| Large-Flange Tri-Fold Rivet for Low-Load-Bearing Composite Skins | Nominal diameter: 4.8 mm Typical grip range: 1.5–4.8 mm Flange diameter: commonly larger than standard head types | Thin or fragile laminate skins, removable covers, ducts, and assemblies where the surface needs additional bearing area. | Verify the larger flange will not interfere with adjacent hardware. The hole must be round, clean, and free from loose fibers; avoid forcing an oversized rivet into an undersized hole. | The larger head spreads surface pressure and can reduce local bearing stress on thin composite skins, especially when the joint is lightly loaded. | Look for flange lifting, surface indentation, resin cracking, and fretting around the hole. Re-seal the flange area if the joint is exposed to water, chemicals, or road debris. | Do not assume a large flange makes the joint structural. Excessive installation force can crush the laminate; use the correct nosepiece and calibrated setting tool. |
| Corrosion-Controlled Aluminium Tri-Fold Rivet for Mixed-Material Assemblies | Nominal diameter: 6.4 mm Typical grip range: 2.0–6.4 mm | Large access covers, composite housings, and low-to-medium load attachments requiring a larger fastener diameter and controlled environmental exposure. | Typical hole size is approximately 6.5–6.6 mm for a 6.4 mm rivet. Confirm galvanic compatibility between the aluminium body, mandrel, washers, and any embedded metal hardware. | Higher diameter provides more bearing area and can improve resistance to pull-through when the surrounding laminate is properly designed and reinforced. | Use a compatible sealant or isolating layer where aluminium contacts carbon-fiber material or dissimilar metals. Inspect for galvanic corrosion, white powder, pitting, and moisture traps. | Direct aluminium-to-carbon contact can create a galvanic-corrosion risk in the presence of an electrolyte. A common mistake is choosing rivet material without checking the complete material stack and service environment. |