{"id":8385,"date":"2025-03-23T13:48:09","date_gmt":"2025-03-23T13:48:09","guid":{"rendered":"https:\/\/premiumalu.com\/?post_type=product&#038;p=8385"},"modified":"2026-07-07T08:32:47","modified_gmt":"2026-07-07T08:32:47","slug":"2117-aluminiumlegierung","status":"publish","type":"product","link":"https:\/\/premiumalu.com\/de\/produkt\/2117-aluminiumlegierung\/","title":{"rendered":"2117 Aluminium-Legierung"},"content":{"rendered":"<h2>What Is 2117 Aluminum Alloy?<\/h2>\n<p>2117 aluminum (also designated EN AW-2117 \/ UNS A92117) is a low-copper 2xxx series alloy containing approximately 2.2\u20133.0% copper with small additions of silicon, magnesium, and manganese. It is specifically developed for rivet and fastener applications where a balance of strength and ductility is essential.<\/p>\n<p>2117 is the standard alloy for solid rivets in aircraft construction \u2014 it provides adequate shear strength while maintaining enough ductility for cold heading and rivet driving without cracking. It is also used for general-purpose fasteners, cotter pins, and cold-formed hardware.<\/p>\n<p>In the T4 temper (solution heat-treated and naturally aged), 2117 achieves its best combination of shear strength and ductility. This makes it the default rivet material in most aerospace specifications.<\/p>\n<h2>Available 2117 Aluminum Products<\/h2>\n<h3>2117 Aluminum Bar &amp; Rivet Stock<\/h3>\n<p>Round bar and rivet wire are the primary forms of 2117 alloy. Available in T4 temper for optimal riveting performance.<\/p>\n<table>\n<tr>\n<th>Legierung<\/th>\n<th>Temperament<\/th>\n<th>Durchmesser (mm)<\/th>\n<th>L\u00e4nge (mm)<\/th>\n<\/tr>\n<tr>\n<td>2117<\/td>\n<td>T4, T42, T3<\/td>\n<td>3\u201350<\/td>\n<td>1,000\u20136,000<\/td>\n<\/tr>\n<\/table>\n<p>Rivet wire is available in smaller diameters (1.5\u201310 mm) for heading operations. Custom cut-to-length available on request.<\/p>\n<h3>2117 Aluminum Wire<\/h3>\n<p>Wire for rivet heading, cotter pins, and cold-formed fasteners.<\/p>\n<table>\n<tr>\n<th>Legierung<\/th>\n<th>Temperament<\/th>\n<th>Durchmesser (mm)<\/th>\n<th>Weight\/Coil (kg)<\/th>\n<th>Toleranz<\/th>\n<\/tr>\n<tr>\n<td>2117<\/td>\n<td>T4, T3<\/td>\n<td>0.8\u201312<\/td>\n<td>Min 50<\/td>\n<td>&amp;plusmn; 0.02 mm<\/td>\n<\/tr>\n<\/table>\n<h3>2117 Aluminum Sheet &amp; Plate<\/h3>\n<p>Sheet for formed brackets, doublers, and repair patches in aircraft structures.<\/p>\n<table>\n<tr>\n<th>Legierung<\/th>\n<th>Temperament<\/th>\n<th>Dicke (mm)<\/th>\n<th>Breite (mm)<\/th>\n<th>L\u00e4nge (mm)<\/th>\n<\/tr>\n<tr>\n<td>2117<\/td>\n<td>T4<\/td>\n<td>0.3\u201350<\/td>\n<td>500\u20131,500<\/td>\n<td>1,000\u20134,000<\/td>\n<\/tr>\n<\/table>\n<h3>2117 Aluminum Tube<\/h3>\n<p>Tube for structural sleeves and bushings.<\/p>\n<table>\n<tr>\n<th>Legierung<\/th>\n<th>Temperament<\/th>\n<th>OD (mm)<\/th>\n<th>Wand (mm)<\/th>\n<th>L\u00e4nge (mm)<\/th>\n<\/tr>\n<tr>\n<td>2117<\/td>\n<td>T4<\/td>\n<td>6\u201380<\/td>\n<td>1\u20138<\/td>\n<td>1,000\u20136,000<\/td>\n<\/tr>\n<\/table>\n<h2>Technische Daten und gleichwertige Bezeichnungen<\/h2>\n<table>\n<tr>\n<th>Standard<\/th>\n<th>Bezeichnung<\/th>\n<\/tr>\n<tr>\n<td>EN AW<\/td>\n<td>AW-2117<\/td>\n<\/tr>\n<tr>\n<td>UNS<\/td>\n<td>A92117<\/td>\n<\/tr>\n<tr>\n<td>ASTM (Rivet Wire)<\/td>\n<td>B316<\/td>\n<\/tr>\n<tr>\n<td>ASTM (Stange)<\/td>\n<td>B211<\/td>\n<\/tr>\n<tr>\n<td>ISO<\/td>\n<td>AlCu2.5Mg0.2<\/td>\n<\/tr>\n<tr>\n<td>Federal<\/td>\n<td>QQ-A-430 (rivet wire)<\/td>\n<\/tr>\n<\/table>\n<h2>Chemische Zusammensetzung<\/h2>\n<p>Per EN 573-3 \/ ASTM B316:<\/p>\n<table>\n<tr>\n<th>Element<\/th>\n<th>Gewicht %<\/th>\n<\/tr>\n<tr>\n<td>Si<\/td>\n<td>0.8\u20131.2<\/td>\n<\/tr>\n<tr>\n<td>Fe<\/td>\n<td>0,7 max<\/td>\n<\/tr>\n<tr>\n<td>Cu<\/td>\n<td>2.2\u20133.0<\/td>\n<\/tr>\n<tr>\n<td>Mn<\/td>\n<td>0,20 max.<\/td>\n<\/tr>\n<tr>\n<td>Mg<\/td>\n<td>0.20-0.50<\/td>\n<\/tr>\n<tr>\n<td>Cr<\/td>\n<td>0,10 max<\/td>\n<\/tr>\n<tr>\n<td>Zn<\/td>\n<td>0,25 max<\/td>\n<\/tr>\n<tr>\n<td>Ti<\/td>\n<td>0,15 max<\/td>\n<\/tr>\n<tr>\n<td>Sonstige (jeweils)<\/td>\n<td>0,05 max<\/td>\n<\/tr>\n<tr>\n<td>Sonstige (insgesamt)<\/td>\n<td>0,15 max<\/td>\n<\/tr>\n<tr>\n<td>Al<\/td>\n<td>Bilanz<\/td>\n<\/tr>\n<\/table>\n<h2>Mechanische Eigenschaften je nach Temperierung<\/h2>\n<table>\n<tr>\n<th>Temperament<\/th>\n<th>Zugfestigkeit (MPa)<\/th>\n<th>Streckgrenze (MPa)<\/th>\n<th>Dehnung A50 (%)<\/th>\n<th>Scherfestigkeit (MPa)<\/th>\n<\/tr>\n<tr>\n<td>T4<\/td>\n<td>295\u2013340<\/td>\n<td>165\u2013200<\/td>\n<td>15\u201322<\/td>\n<td>185\u2013210<\/td>\n<\/tr>\n<tr>\n<td>T42<\/td>\n<td>290\u2013330<\/td>\n<td>160\u2013190<\/td>\n<td>15\u201320<\/td>\n<td>180\u2013205<\/td>\n<\/tr>\n<tr>\n<td>T3<\/td>\n<td>260\u2013310<\/td>\n<td>140\u2013175<\/td>\n<td>18\u201325<\/td>\n<td>165\u2013195<\/td>\n<\/tr>\n<\/table>\n<p>Note: Shear strength is a critical property for rivet alloys and is included in the table above. Values are typical ranges; confirm with MTC for specific orders.<\/p>\n<h2>Leitfaden zur Auswahl der H\u00e4rtung<\/h2>\n<h3>T4 Temper \u2014 Standard Rivet Temper<\/h3>\n<p>T4 (solution heat-treated and naturally aged) is the default temper for 2117 rivet wire and bar. It provides the optimal balance of shear strength and ductility for cold-heading and rivet-driving operations. Most aerospace rivet specifications require 2117-T4.<\/p>\n<h3>T42 Temper \u2014 Controlled Properties<\/h3>\n<p>T42 is 2117 that has been solution heat-treated and naturally aged to meet specific mechanical property ranges negotiated between purchaser and supplier. Used when tighter control of shear or tensile values is required.<\/p>\n<h3>T3 Temper \u2014 Cold-Worked + Natural Aging<\/h3>\n<p>T3 provides higher ductility with slightly lower strength \u2014 suitable for applications requiring more forming before final aging.<\/p>\n<table>\n<tr>\n<th>Temperament<\/th>\n<th>Am besten f\u00fcr<\/th>\n<th>Hauptvorteil<\/th>\n<\/tr>\n<tr>\n<td>T4<\/td>\n<td>Standard rivets, structural fasteners<\/td>\n<td>Best shear\/ductility balance for rivet driving<\/td>\n<\/tr>\n<tr>\n<td>T42<\/td>\n<td>Spec-controlled rivets<\/td>\n<td>Tight property ranges per purchaser agreement<\/td>\n<\/tr>\n<tr>\n<td>T3<\/td>\n<td>Formed parts needing extra ductility<\/td>\n<td>Higher elongation before aging<\/td>\n<\/tr>\n<\/table>\n<h2>Wesentliche Merkmale<\/h2>\n<h3>Excellent Rivet Performance<\/h3>\n<p>2117-T4 is the industry-standard rivet alloy. Its shear strength (~185\u2013210 MPa) is sufficient for structural joints, while its elongation (15\u201322%) ensures reliable cold heading and driving without cracking \u2014 the two essential properties for rivet performance.<\/p>\n<h3>Good Ductility &amp; Cold Formability<\/h3>\n<p>The relatively low copper content (2.2\u20133.0%) gives 2117 better ductility than 2024 or 2014. This makes it suitable for heading, upsetting, and cold-forming operations common in fastener manufacturing.<\/p>\n<h3>M\u00e4\u00dfige St\u00e4rke<\/h3>\n<p>2117 is not a high-strength structural alloy. Its tensile strength (295\u2013340 MPa in T4) is adequate for shear-loaded joints but insufficient for primary structural members. For high-strength applications, use 2024 or 7075 instead.<\/p>\n<h3>Korrosionsbest\u00e4ndigkeit<\/h3>\n<p>2117 has moderate corrosion resistance \u2014 better than 2024 but not suitable for marine environments without protection. In aerospace construction, 2117 rivets are typically used with Alclad 2024 sheet, where the rivet and surrounding skin form a compatible dissimilar-metal joint.<\/p>\n<h2>Anwendungen<\/h2>\n<p>2117 aluminum is used wherever rivet and fastener performance is critical:<\/p>\n<ul>\n<li><strong>Aerospace rivets:<\/strong> Standard solid rivets (MS20426, AN470 series) for aircraft skin and structural joints<\/li>\n<li><strong>Automotive fasteners:<\/strong> Cotter pins, split pins, and formed hardware<\/li>\n<li><strong>General fasteners:<\/strong> Cold-headed bolts, screws, and rivets for light structural applications<\/li>\n<li><strong>CNC-Bearbeitung:<\/strong> Precision-turned bushings, sleeves, and fittings<\/li>\n<li><strong>Structural hardware:<\/strong> Clevis pins, retaining rings, and shear pins<\/li>\n<\/ul>\n<h2>Hinweise zur Bearbeitung und Oberfl\u00e4chenveredelung<\/h2>\n<ul>\n<li><strong>Cold heading:<\/strong> 2117-T4 is specifically designed for cold heading operations (rivet manufacturing). The alloy&#8217;s ductility allows it to be upset and formed without pre-heating.<\/li>\n<li><strong>Rivet driving:<\/strong> 2117 rivets can be driven by hand, pneumatic, or hydraulic methods. The alloy&#8217;s shear strength provides reliable joint performance after driving.<\/li>\n<li><strong>Zerspanung:<\/strong> Fair machinability \u2014 better than pure aluminum but not as free-cutting as 2011 or 2030. Carbide tooling recommended for production runs.<\/li>\n<li><strong>Schwei\u00dfen:<\/strong> Not recommended for structural welding. Gas tungsten arc (TIG) welding is possible for non-critical repair but is not a standard joining method for 2117 components.<\/li>\n<li><strong>W\u00e4rmebehandlung:<\/strong> Solution treatment at approximately 500\u2013510\u00b0C, followed by natural aging. Artificial aging (T6) is rarely specified for 2117.<\/li>\n<li><strong>Oberfl\u00e4cheng\u00fcte:<\/strong> Anodizing is possible; results are functional but not as cosmetically uniform as 6xxx alloys due to copper content.<\/li>\n<\/ul>\n<h2>Qualit\u00e4tsdokumente und Qualit\u00e4tspr\u00fcfung<\/h2>\n<p>Jede Bestellung von Linsy beinhaltet:<\/p>\n<ul>\n<li><strong>Werkspr\u00fcfzeugnis (MTC)<\/strong> \u2014 chemical composition and mechanical properties (including shear strength) per ASTM B316 \/ B211<\/li>\n<li><strong>Ma\u00dfpr\u00fcfbericht<\/strong> \u2014 measured against order specifications<\/li>\n<li><strong>SGS-Pr\u00fcfberichte<\/strong> auf Anfrage f\u00fcr die \u00dcberpr\u00fcfung durch Dritte erh\u00e4ltlich<\/li>\n<\/ul>\n<p>Linsy arbeitet nach den Managementsystemen ISO 9001, ISO 14001 und ISO 45001. Die Produktionsvorlaufzeiten betragen je nach Produktform und Auftragskomplexit\u00e4t 10 bis 60 Tage.<\/p>\n<h2>Why Choose Linsy for 2117 Aluminum<\/h2>\n<p>Linsy Aluminum supplies rivet and fastener alloys to aerospace and industrial buyers worldwide. For 2117 alloy:<\/p>\n<ul>\n<li>Rivet wire and bar available in T4 temper \u2014 the standard rivet specification<\/li>\n<li>Sheet, plate, and tube also available from production runs<\/li>\n<li>Custom wire diameters and coil weights on request<\/li>\n<li>MTC report included with every shipment \u2014 shear strength values provided<\/li>\n<li>Nach ISO 9001, ISO 14001, ISO 45001 zertifizierte Betriebsabl\u00e4ufe<\/li>\n<li>Produktionsvorlaufzeit 10\u201360 Tage, abh\u00e4ngig von der Spezifikation<\/li>\n<li>SGS-Pr\u00fcfung durch Dritte auf Anfrage verf\u00fcgbar<\/li>\n<\/ul>\n<h2>Weiterf\u00fchrende Ressourcen<\/h2>\n<p>Learn more about rivet alloys and aerospace fasteners:<\/p>\n<ul>\n<li><a href=\"https:\/\/premiumalu.com\/de\/2xxx-series-aluminum-alloys-guide\/\">2xxx Series Aluminum Alloys \u2014 Complete Guide<\/a><\/li>\n<li><a href=\"https:\/\/premiumalu.com\/de\/aluminum-rivet-wire-specifications-guide\/\">Aluminum Rivet Wire \u2014 Specifications &amp; Selection Guide<\/a><\/li>\n<li><a href=\"https:\/\/premiumalu.com\/de\/2017-vs-2117-aluminum-rivet-alloy-comparison\/\">2017 vs 2117 \u2014 Rivet Alloy Comparison<\/a><\/li>\n<\/ul>\n<h2>2117 Aluminum FAQ<\/h2>\n<h3>Why is 2117 used for rivets?<\/h3>\n<p>2117-T4 provides the right balance of shear strength (~185\u2013210 MPa) and ductility (15\u201322% elongation) for cold heading and rivet driving. The alloy can be upset and formed into rivet heads without cracking, and the driven rivet provides reliable shear-load performance.<\/p>\n<h3>How does 2117 compare to 2017 for rivets?<\/h3>\n<p>2017 (AD rivet alloy) has higher shear strength but lower ductility than 2117. 2117 (A rivet alloy) is more forgiving during rivet driving and is preferred for standard structural joints. 2017 is used where higher shear strength is required.<\/p>\n<h3>Can 2117 rivets be used with 2024-T3 skin?<\/h3>\n<p>Yes. 2117-T4 rivets are commonly used with 2024-T3 and Alclad 2024-T3 sheet in aircraft construction. The dissimilar-metal potential is minimal and is addressed by design standards (MIL-HDBK-5 \/ MMPDS).<\/p>\n<h3>Is 2117 weldable?<\/h3>\n<p>Not recommended for structural welding. TIG welding is possible for non-critical repair, but riveting or mechanical fastening is the standard joining method for 2117 components.<\/p>\n<h3>What is the difference between T4 and T42?<\/h3>\n<p>T42 is 2117 that has been heat-treated to meet specific mechanical property ranges negotiated between purchaser and supplier, rather than the standard T4 minimums. It provides tighter control of properties for critical applications.<\/p>\n<h2>Allgemeine Fragen zur Bestellung<\/h2>\n<h3>Wie lautet die Mindestbestellmenge?<\/h3>\n<p>MOQ depends on product form. Rivet wire typically has lower MOQ than bar or plate. Contact Linsy for specific details.<\/p>\n<h3>Can I order rivet wire in custom coil weights?<\/h3>\n<p>Yes. Standard coil weight is 50 kg minimum. Custom coil weights are available on request.<\/p>\n<h3>Welche Qualit\u00e4tsdokumente werden bereitgestellt?<\/h3>\n<p>Every shipment includes a Mill Test Certificate (MTC) with chemical composition, tensile, yield, elongation, and shear strength values. SGS third-party reports are available on request.<\/p>\n<h3>Wie ist die typische Lieferzeit?<\/h3>\n<p>Production lead time is 10\u201360 days depending on product form, dimensions, and order quantity.<\/p>\n<h3>Versenden Sie auch ins Ausland?<\/h3>\n<p>Ja. Linsy liefert Aluminiumprodukte an K\u00e4ufer weltweit. Versandbedingungen und Frachtoptionen werden bei der Bestellaufgabe best\u00e4tigt.<\/p>","protected":false},"excerpt":{"rendered":"<p>2117 aluminum is a copper-based 2xxx series alloy best known as the standard rivet alloy in aerospace construction. Its combination of moderate strength, excellent ductility, and reliable shear performance makes it the preferred choice for structural rivets and fasteners. Linsy supplies 2117 in bar, wire, sheet, and tube \u2014 all backed by mill test certificates.<\/p>\n<p><strong>Verf\u00fcgbare Formulare:<\/strong> bar \/ wire \/ sheet \/ tube \/ profile<br \/><strong>H\u00e4ufige Temperamente:<\/strong> T4 \/ T42 \/ T3<br \/><strong>Unterst\u00fctzung bei der Bearbeitung:<\/strong> riveting \/ heading \/ CNC machining \/ cold forming<br \/><strong>Qualit\u00e4tsdokumente:<\/strong> MTC-Bericht bei jeder Bestellung<\/p>","protected":false},"featured_media":8386,"template":"","meta":{"_seopress_titles_title":"2117 Aluminum Alloy Rivet Wire & Bar Supplier | Linsy Aluminum","_seopress_titles_desc":"2117 aluminum alloy \u2014 the standard aerospace rivet alloy. Bar, wire, sheet & tube in T4\/T42\/T3 temper. Shear strength data included. 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