Development and research of metrological characteristics of express-analysis of heat-resistant nickel alloys

Karachevtsev F.N., Zagvozdkina T.N., Orlov G.V.
UDC
620.1.08:669.018.44:669.245
DOI
10.18577/2307-6046-2015-0-11-9-9
Article PDF (Russian) (528.89 KB)
How to cite
Karachevtsev F.N., Zagvozdkina T.N., Orlov G.V. Development and research of metrological characteristics of express-analysis of heat-resistant nickel alloys // Proceedings of VIAM. 2015. No. 11. DOI: 10.18577/2307-6046-2015-0-11-9-9. URL: https://test.viam.ru/en/journal/2015/11/9
Keywords
measurement technique, nickel alloys, the metrological characteristics, optical emission method.
Abstract

Heat-resistant nickel alloys (HRNA) are one of the promising materials, which are used in aviation engineering for manufacture of a wide range of parts and structures for various purposes. Improvement in heat resistance of HRNA depends on the conditions of their production and chemical composition. In this regard control of the composition of HRNA in the process of their production by method of express-analysis is an extremely important problem. The developed method of optical emission analysis provides relative error at determination of the content of alloying elements not more than 5% at values of the mass fraction of more than 1%.

Reference list
  1. Kablov E.N. Fiziko-himicheskie i tehnologicheskie osobennosti sozdaniya zharoprochnyh splavov, soderzhashhih renij [Physical and chemical and technological features of creation of the heat resisting alloys containing rhenium] //Vestnik Moskovskogo universiteta. Ser. 2. Himiya. 2005. T. 46. №3. S. 155–167.
  2. Kablov E.N., Lomberg B.S., Ospennikova O.G. Sozdanie sovremennyh zharoprochnyh materialov i tehnologij ih proizvodstva dlya aviacionnogo dvigatelestroeniya [Creation of modern heat resisting materials and technologies of their production for aviation engine-building] //Krylya Rodiny. 2012. №3–4. S. 34–38.
  3. Kablov E.N., Ospennikova O.G., Petrushin N.V., Visik E.M. Monokristallicheskij zharoprochnyj nikelevyj splav novogo pokoleniya s nizkoj plotnostyu [Single-crystal nickel-based superalloy of a new generation with low-dencsity] //Aviacionnye materialy i tehnologii. 2015. №2 (35). S. 14–25.
  4. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Nikelevye litejnye zharoprochnye splavy novogo pokoleniya [Nickel foundry heat resisting alloys of new generation] //Aviacionnye materialy i tehnologii. 2012. №S. S. 36–52.
  5. Lomberg B.S., Ovsepjan S.V., Bakradze M.M., Mazalov I.S. Vysokotemperaturnye zharoprochnye nikelevye splavy dlya detalej gazoturbinnyh dvigatelej [High-temperature heat resisting nickel alloys for details of gas-turbine engines] //Aviacionnye materialy i tehnologii. 2012. №S. S. 52–57.
  6. Kablov E.N., Petrushin N.V., Svetlov I.L., Demonis I.M. Litejnye zharoprochnye nikelevye splavy dlya perspektivnyh aviacionnyh GTD [Foundry heat resisting nickel alloys for perspective aviation GTE] //Tehnologiya legkih splavov. 2007. №2. S. 6–16.
  7. Shmotin Ju.N., Starkov R.Ju., Danilov D.V., Ospennikova O.G., Lomberg B.S. Novye materialy dlya perspektivnogo dvigatelya OAO «NPO „Saturn”» [New materials for the perspective engine of JSC «NPO „Saturn”»] //Aviacionnye materialy i tehnologii. 2012. №2. S. 6–8.
  8. Kablov E.N., Ospennikova O.G., Petrushin N.V. Novyj monokristallicheskij intermetallidnyj (na osnove γʹ-fazy) zharoprochnyj splav dlya lopatok GTD [New single crystal heat-resistant intermetallic γʹ-based alloy for GTE blades] //Aviacionnye materialy i tehnologii. 2015. №1 (34). S. 34–40.
  9. Sidorov V.V., Rigin V.E., Filonova E.V., Timofeeva O.B. Structurnye isslidovaniya i svoistva monokristallov splavov VZhM4-VI i VZhM5-VI [The structure investigations and properties of VGM4-VI and VGM5-VI single crystal alloys with increased phosphorus quantity] // Trudy VIAM. 2014. №3. St. 02. (viam-works.ru).
  10. Lomberg B.S., Bakradze M.M., Chabina E.B., Filonova E.V. Vzaimosvjaz struktury i svojstv vysokozharoprochnyh nikelevyh splavov dlya diskov gazoturbinnyh dvigatelej [Interrelation of structure and properties of high-heat resisting nickel alloys for disks of gas-turbine engines] //Aviacionnye materialy i tehnologii. 2011. №2. S. 25–30.
  11. Chabina E.B., Filonova E.V., Lomberg B.S., Bakradze M.M. Struktura sovremennyh deformiruemyh nikelevyh splavov [Structure of modern deformable nickel alloys] //Vse materialy. Jenciklopedicheskij spravochnik. 2012. T. 6. S. 22–27.
  12. Petrushin N.V., Eljutin E.S., Chabina E.B., Timofeeva O.B. O fazovyh i strukturnyh prevrashhenijah v zharoprochnyh renijsoderzhashhih splavah monokristallicheskogo stroeniya [About phase and structural transformations in heat resisting the reniysoderzhashchikh alloys of a single-crystal structure] //Litejnoe proizvodstvo. 2008. №7. S. 1–7.
  13. Letov A.F., Karachevcev F.N., Gundobin N.V., Titov V.I. Razrabotka standartnyh obrazcov sostava splavov aviacionnogo naznacheniya [Development of standard samples of structure of alloys of aviation appointment] //Aviacionnye materialy i tehnologii. 2012. №S. C. 393–398.
  14. Letov A.F., Karachevcev F.N. Opyt razrabotki standartnyh obrazcov aviacionnyh splavov [Experience of development of standard samples of aviation alloys] //Mir izmerenij. 2012. №8. S. 31–35.
  15. Karachevcev F.N., Letov A.F., Procenko O.M., Jakimova M.S. Razrabotka standartnyh obrazcov sostava aviacionnyh splavov [Development of standard samples of structure of aviation alloys] //Standartnye obrazcy. 2013. №4. S. 30–34.