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.
Химический состав
UDIMET® alloy R41 is primarily composed of nickel with significant additions of cobalt, chromium, tungsten, and molybdenum to enhance its mechanical and thermal properties:
Элемент | Состав (%) |
---|---|
Никель (Ni) | 50.0 – 60.0 |
Кобальт (Со) | 14.0 – 17.0 |
Хром (Cr) | 15.0 – 18.0 |
Вольфрам (Ж) | 3,0 – 5,0 |
Молибден (Мо) | 2.5 – 4.0 |
Железо (Fe) | 3,0 – 5,0 |
Титан (Ti) | 1.5 – 2.5 |
Алюминий (Al) | 0.1 – 0,5 |
Бор (Б) | 0.005 – 0.05 |
Углерод (С) | 00,05 макс. |
Механические свойства
UDIMET® alloy R41 exhibits excellent mechanical properties suitable for high-temperature applications:
Свойство | Ценить |
---|---|
Предел прочности, тыс.фунтов на квадратный дюйм (МПа) | 150 – 180 (1034 – 1241) |
Предел текучести (смещение 0,2%), тыс.фунтов на квадратный дюйм (МПа) | 110 – 140 (758 – 965) |
Удлинение (% на 2 дюйма) | 20 – 25 |
Твердость, Роквелл C (HRC) | 35 – 40 |
Характеристики производительности
UDIMET® alloy R41 offers several performance advantages:
- Высокотемпературная прочность: Maintains excellent mechanical properties at temperatures up to 1000°C (1832°F), suitable for use in gas turbines and other high-temperature applications.
- Устойчивость к окислению: 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.
Промышленные приложения
UDIMET® alloy R41 is utilized in various demanding industries where high performance under extreme conditions is required:
Промышленный сектор | Приложения |
---|---|
Аэрокосмическая промышленность | Gas turbine components including blades, discs, and seals. |
Выработка энергии | Turbine blades, combustion chambers, and heat exchangers. |
Химическая обработка | Reactor vessels, pipelines, and valves for handling corrosive chemicals at high temperatures. |
Формы и размеры
UDIMET® alloy R41 is available in various forms and sizes to meet specific application needs:
- Формы: Листы, пластины, прутки, поковки и проволока.
- Размеры: Толщина листов от 0,5 мм до 100 мм и диаметр круглых прутков от 1 мм до 300 мм.
Производственные стандарты
UDIMET® alloy R41 conforms to international production standards ensuring quality and reliability:
Форма продукта | Доступные формы | Доступные размеры | Производственные стандарты |
---|---|---|---|
Плиты/листы | Листы, плиты | Толщина: 0,5 мм – 100 мм | ASTM B637, AMS 5764 |
Бары/стержни | Круглые стержни, Квадратные стержни | Диаметр: 1 мм – 300 мм | ASTM B637, AMS 5764 |
Поковки | Блоки, Диски, Кольца | Размер: Индивидуальный | ASTM B637, AMS 5764 |
Сварка и обработка
UDIMET® alloy R41 offers good weldability and processing characteristics:
- Сварка: Можно сваривать такими методами, как TIG, MIG и контактная сварка. Для сохранения свойств могут потребоваться предварительный нагрев и термообработка после сварки.
- Обрабатываемость: Обычно обрабатывается в отожженном состоянии с использованием твердосплавных инструментов и соответствующих смазочно-охлаждающих жидкостей.
Преимущества и недостатки
Аспект | Подробности |
---|---|
Преимущества | Exceptional high-temperature strength and oxidation resistance, good creep resistance, and wide availability in various forms and sizes. |
Недостатки | Higher cost compared to standard nickel alloys, requires specialized processing and handling due to its high strength and alloying elements. |
Сравнение с аналогичными сплавами
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:
Тип/свойство сплава | УДИМЕТ® сплав R41 | UDIMET® alloy 718 | УДИМЕТ® сплав 720 |
---|---|---|---|
Химический состав | High 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. |
Механические свойства | Higher 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. |
Приложения | Gas 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.