Abstract

The density of a substance is one of its main physical characteristics. This is especially true for materials used in aviation, where the mass of each structural element should be minimized as much as possible. When developing new structural materials, for example, heat-resistant nickel alloys, which are widely used in the manufacture of gas turbine engine parts, it is extremely important to have a reliable and accurate method for assessing the density of the material being developed. Until now, no unified method has been proposed for calculating the density of heat-resistant nickel alloys. The paper reviews the available approaches to assessing the density of alloys and proposes a new formula that allows one to calculate the density of an alloy with a high accuracy based on the information on its composition. The proposed approach takes into account the spatial fcc structure of heat-resistant nickel alloys as well as the molar mass and molar volume of the elements that form the alloy. To check the accuracy of the calculations, a database of 69 heat-resistant nickel alloys was collected, containing information on the composition of the alloys and their known density. According to the proposed formula, as well as using some other known approaches, the density for the alloys from the database was calculated. The calculation results showed that the proposed method provided the best accuracy among all considered ones: the standard deviation of the calculated values from the real ones for the entire sample was 0.1 %, the mean values and medians practically coincide. In addition, the calculation errors are normally distributed and have an average value of −0.0001. The existing methods give a minimum error of 1.2 %, thus, the proposed approach improved the accuracy of calculating the density of heat-resistant nickel alloys by about an order of magnitude, which is a significant result both from the point of view of the general scientific approach and from the point of view of engineering practice. Taking into account the results obtained, the proposed formula can be widely used in the development of new and modification of existing heat-resistant nickel alloys.

Highlights

  • Точная эмпирическая формула определения плотности жаропрочных никелевых сплавов Тарасов Д

  • When developing new structural materials, for example, heat-resistant nickel alloys, which are widely used in the manufacture of gas turbine engine parts, it is extremely important to have a reliable and accurate method for assessing the density of the material being developed

  • No unified method has been proposed for calculating the density of heat-resistant nickel alloys

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Summary

Введение

Разработка жаропрочных никелевых сплавов (ЖНС) со специальными свойствами для применения в газотурбинных двигателях является сложной научной и инженерной задачей, требующей высокой концентрации усилий специалистов, особенно в свете тенденций на снижение плотности сплавов с сохранением и улучшением их характеристик и применение высокототехнологичного монокристаллического литья [1,2,3,4]. Современные принципы экономного легирования в первую очередь ставят своей целью снижение стоимости сплава, но параллельно с этим рассматриваются и вопросы снижения плотности, в частности за счет снижения содержания дорогостоящего и чрезвычайно плотного рения [5 – 7]. В свете вышесказанного было бы полезно при разработке ЖНС количественно учитывать фактор плотности, а для этого необходимо иметь метод точной ее оценки, а именно — аналитическую зависимость плотности сплава от содержания в нем легирующих элементов. Необходимо также разделять вопросы оценки плотности сплавов в твердом и жидком состоянии. Предметом нашего исследования является плотность ЖНС при нормальных условиях, для определения которой мы связали физические принципы вычисления плотности твердых веществ и эмпирический подход, основанный на учете особенностей структуры ЖНС

Структура и подходы к оценке плотности ЖНС
Описание подхода и экспериментальная проверка
Результаты и обсуждение
Findings
Заключение
Full Text
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