Lega UDIMET® R41

UDIMET-Lega-r41

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:

ElementoComposizione (%)
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
Boron (B)0.005 – 0.05
Carbonio (C)00,05 massimo

Proprietà meccaniche

UDIMET® alloy R41 exhibits excellent mechanical properties suitable for high-temperature applications:

ProprietàValore
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:

  • High-Temperature Strength: Maintains excellent mechanical properties at temperatures up to 1000°C (1832°F), suitable for use in gas turbines and other high-temperature applications.
  • Oxidation Resistance: Provides superior resistance to oxidation and corrosion in high-temperature and aggressive environments.
  • Creep Resistance: 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 industrialeApplicazioni
AerospazialeGas turbine components including blades, discs, and seals.
Produzione di energiaTurbine blades, combustion chambers, and heat exchangers.
Elaborazione chimicaReactor 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 prodottoForme disponibiliTaglie disponibiliStandard di produzione
Lastre/FogliFogli, PiattiSpessore: 0,5 mm – 100 mmASTM B637, AMS 5764
Barre/AsteBarre tonde, Barre quadrateDiametro: 1 mm – 300 mmASTM B637, AMS 5764
ForgiatiBlocchi, Dischi, AnelliDimensioni: personalizzatoASTM B637, AMS 5764

Saldatura e lavorazione

UDIMET® alloy R41 offers good weldability and processing characteristics:

  • Saldatura: Can be welded using methods such as TIG, MIG, and resistance welding. Preheating and post-weld heat treatment may be required to maintain properties.
  • Lavorabilità: Generally machined in the solution-annealed condition using carbide tools and appropriate cutting fluids.

Vantaggi e svantaggi

AspettoDettagli
VantaggiExceptional high-temperature strength and oxidation resistance, good creep resistance, and wide availability in various forms and sizes.
SvantaggiHigher cost compared to standard nickel alloys, requires specialized processing and handling due to its high strength and alloying elements.

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 legaLega UDIMET® R41UDIMET® alloy 718UDIMET® lega 720
Composizione chimicaHigh nickel, cobalt, chromium, tungsten, molybdenum for high-temperature strength.High nickel, chromium, and niobium with smaller additions of aluminum and titanium.High nickel, cobalt, chromium, tungsten, molybdenum for high-temperature strength.
Proprietà meccanicheHigher tensile and yield strength, superior creep resistance at high temperatures.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.
ApplicazioniGas turbines, aerospace components requiring high-temperature strength and oxidation resistance.Aerospace components, high-temperature bolts, and fasteners.Gas turbines, aerospace components requiring high-temperature strength and oxidation resistance.

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.