UDIMET® Alloy R41 (UNS N07041) Product Introduction
UDIMET® alloy R41, designated as UNS N07041, is a high-temperature nickel-based superalloy known for its exceptional strength and corrosion resistance in extreme environments. This article provides a comprehensive introduction to UDIMET® alloy R41, covering its chemical composition, mechanical properties, performance at different temperatures, industry applications, shapes and sizes, production standards, welding and processing capabilities, advantages and disadvantages, and a comparison with similar alloys.
Composizione chimica
UDIMET® alloy R41 is primarily composed of nickel with significant additions of cobalt, chromium, tungsten, and molybdenum to enhance its mechanical and thermal properties:
Elemento | Composizione (%) |
---|---|
Nichel (Ni) | 50.0 – 60.0 |
Cobalto (Co) | 14.0 – 17.0 |
Cromo (Cr) | 15.0 – 18.0 |
Tungsteno (W) | 3.0 – 5.0 |
Molibdeno (Mo) | 2.5 – 4.0 |
Ferro (Fe) | 3.0 – 5.0 |
Titanio (Ti) | 1.5 - 2,5 |
Alluminio (Al) | 0.1 – 0.5 |
Boro (b) | 0.005 – 0.05 |
Carbonio (C) | 00,05 massimo |
Proprietà meccaniche
UDIMET® alloy R41 exhibits excellent mechanical properties suitable for high-temperature applications:
Proprietà | Valore |
---|---|
Resistenza alla trazione, ksi (MPa) | 150 – 180 (1034 – 1241) |
Limite di snervamento (compensazione dello 0,2%), ksi (MPa) | 110 – 140 (758 – 965) |
Allungamento (% in 2 pollici) | 20 – 25 |
Durezza, Rockwell C (HRC) | 35 - 40 |
Caratteristiche prestazionali
UDIMET® alloy R41 offers several performance advantages:
- Resistenza ad alta temperatura: Maintains excellent mechanical properties at temperatures up to 1000°C (1832°F), suitable for use in gas turbines and other high-temperature applications.
- Resistenza all'ossidazione: Provides superior resistance to oxidation and corrosion in high-temperature and aggressive environments.
- Resistenza al creep: Exhibits high creep resistance, making it ideal for components under constant stress at elevated temperatures.
Applicazioni industriali
UDIMET® alloy R41 is utilized in various demanding industries where high performance under extreme conditions is required:
Settore industriale | Applicazioni |
---|---|
Aerospaziale | Gas turbine components including blades, discs, and seals. |
Produzione di energia | Turbine blades, combustion chambers, and heat exchangers. |
Elaborazione chimica | Reactor vessels, pipelines, and valves for handling corrosive chemicals at high temperatures. |
Forme e dimensioni
UDIMET® alloy R41 is available in various forms and sizes to meet specific application needs:
- Forme: Lamiere, lastre, barre, pezzi fucinati e fili.
- Taglie: Spessori da 0,5 mm a 100 mm per le piastre e diametri da 1 mm a 300 mm per le barre tonde.
Standard di produzione
UDIMET® alloy R41 conforms to international production standards ensuring quality and reliability:
Forma del prodotto | Forme disponibili | Taglie disponibili | Standard di produzione |
---|---|---|---|
Lastre/Fogli | Fogli, Piatti | Spessore: 0,5 mm – 100 mm | ASTM B637, AMS 5764 |
Barre/Aste | Barre tonde, Barre quadrate | Diametro: 1 mm – 300 mm | ASTM B637, AMS 5764 |
Forgiati | Blocchi, Dischi, Anelli | Dimensioni: personalizzato | ASTM B637, AMS 5764 |
Saldatura e lavorazione
UDIMET® alloy R41 offers good weldability and processing characteristics:
- Saldatura: Può essere saldato usando metodi come TIG, MIG e saldatura di resistenza. Il trattamento termico di preriscaldamento e post-salvataggio può essere necessario per mantenere le proprietà.
- Lavorabilità: Generalmente lavorata in condizioni di soluzione annealizzate usando strumenti di carburo e fluidi di taglio appropriati.
Vantaggi e svantaggi
Aspetto | Dettagli |
---|---|
Vantaggi | Exceptional high-temperature strength and oxidation resistance, good creep resistance, and wide availability in various forms and sizes. |
Svantaggi | Costi più elevati rispetto alle leghe di nichel standard richiedono elaborazione e gestione specializzate a causa dei suoi elementi elevati e legati. |
Confronto con leghe simili
UDIMET® alloy R41 (UNS N07041) is often compared with other high-temperature nickel-based superalloys such as UDIMET® alloy 718 and UDIMET® alloy 720. Here’s a brief comparison:
Tipo/proprietà della lega | Lega UDIMET® R41 | Udimet® Alley 718 | UDIMET® lega 720 |
---|---|---|---|
Composizione chimica | High nickel, cobalt, chromium, tungsten, molybdenum for high-temperature strength. | Nickel elevato, cromo e niobio con aggiunte più piccole di alluminio e titanio. | High nickel, cobalt, chromium, tungsten, molybdenum for high-temperature strength. |
Proprietà meccaniche | Maggiore resistenza alla trazione e snervamento, resistenza al creep superiore a temperature elevate. | Lower tensile and yield strength compared to UDIMET® alloy R41, good toughness and fatigue resistance. | Higher tensile and yield strength compared to UDIMET® alloy 718, excellent oxidation resistance. |
Applicazioni | Turbine a gas, componenti aerospaziali che richiedono resistenza ad alta temperatura e resistenza all'ossidazione. | Componenti aerospaziali, bulloni ad alta temperatura e dispositivi di fissaggio. | Turbine a gas, componenti aerospaziali che richiedono resistenza ad alta temperatura e resistenza all'ossidazione. |
This detailed article introduces UDIMET® alloy R41 (UNS N07041), highlighting its chemical composition, mechanical properties, performance characteristics, industry applications, available forms and sizes, production standards, welding and processing capabilities, as well as advantages, disadvantages, and a comparison with similar alloys. Engineers and professionals seeking a high-strength, high-temperature superalloy for critical applications in aerospace, power generation, and chemical processing will find UDIMET® alloy R41 well-suited for use under extreme conditions.