Requirements for the order and the procedure of estimating structural strength characteristics of metal alloys for the main and critical parts of aviation gas turbine engines


Cite item

Full Text

Abstract

Requirements of the technical regulations for the order and procedure of estimating structural strength of metal alloys used in critical and main parts of aviation engines in their certification are outlined in the paper. The scope of work to be carried out by the engine designer, the developer of the material/semi-finished product and the engine manufacturer to confirm the compliance with the mentioned requirements is described. The tasks to be solved at different stages of general and special qualification of the material are discussed. The spectrum of the main mechanical characteristics of alloys, including mono-crystal alloys, to be determined during the qualification tests is presented. The standards in accordance to which the tests are to be performed are mentioned. Relationships for the determination of the material characteristics to be used in estimating the strength and service life of engine parts are given. The requirements for the statistical processing of the results of investigating the structural strength of alloys are discussed, as well as the requirements for setting the values of the mechanical properties guaranteed in the delivery of materials/semi-finished products. The necessity to have data on possible presence of different defects in the main (critical for safe operation) engine parts is mentioned. The reference list includes principal technical regulations the requirements of which are to be met during special qualification of alloys used for the manufacture of the main and critical aviation engine parts.

About the authors

Yu. A. Nozhnitsky

Central Institute of Aviation Motors named after P.I. Baranov, Moscow

Author for correspondence.
Email: nozhnitsky@ciam.ru

Doctor of Science (Engineering), Professor

Deputy General Director 

Russian Federation

E. B. Kachanov

Certification Center «MATERIAL», Moscow

Email: av-ccmaterial@yandex.ru

Doctor of Science (Engineering), Professor

Director 

Russian Federation

E. R. Golubovskiy

Central Institute of Aviation Motors named after P.I. Baranov, Moscow

Email: golubovskiy@ciam.ru

Doctor of Science (Engineering), Professor

Head of the Department of Structural Strength Alloys

Russian Federation

V. K. Kouevda

Interstate Aviation Committee (IAC), Moscow

Email: expert@mak.ru

Candidate of Science (Engineering)

Deputy Head of Aviation Register Presidium 

Russian Federation

References

  1. Aviation Rules. Part 21. «Certification Procedures for aviation technics». Moscow: Interstate Aviation Committee Publ., 1994. 40 p. (In Russ.)
  2. Aviation rules. Part 33. «Norms of air-worthiness of aircraft engines», with Amendments 33-1 and 33-2, inclusive. Mos-cow: Interstate Aviation Committee Publ., 2012. 46 р. (In Russ.)
  3. Guide 33-VD-M «The order of evalua-tion of conformity of the materials used in the construction of aircraft engine, the re-quirements of Aviation regulations». Mos-cow: Aviaizdat Publ., 2013. (In Russ.)
  4. Advisory Circular No. RC-AP-33.15-1 «Guidelines for determining design values of the characteristics of structural strength me-tallic materials». Moscow: Aviaizdat Publ., 2013. (In Russ.)
  5. Manual R-CCM-01 «Certification of production materials / prefabricates for avia-tion technics». Iss. 3. Moscow: Aviaizdat Publ., 2012. (In Russ.)
  6. Manual R-CCM -02 Estimation of the production technology of materials (semi-finished) for the certification of production. Issue 4. Moscow: Aviaizdat Publ., 2012. (In Russ.)
  7. Manual R-CCM -03 Certification of la-boratories conducting tests and inspection of materials. Issue 5. Moscow: Aviaizdat Publ., 2012. (In Russ.)
  8. Manual R-CCM-04 «Quality Assess-ment of materials / semi-finished products at certification their production». Issue 5. Mos-cow: Aviaizdat Publ., 2012. (In Russ.)
  9. Kachanov E.B. Efficiency of Applica-tion of the Quality Management System in Enterprises Producing Semi-products for Civil Aircraft. Tekhnologiya legkikh splavov. 2013. No. 4. P. 26-31. (In Russ.)
  10. Rules of accreditation of testing labor-atories /centers (PAL 94). Moscow: Aviation Register of International Aviation Committee Publ., 1994. (In Russ.)
  11. Guidelines for the accreditation of testing laboratories / canters (MR 2010). Moscow: Aviation Register of International Aviation Committee Publ., 2011. (In Russ.)
  12. OST 1 90294-80. Steel and heat re-sistant alloys. A method of determining the sensitivity to notch when tested for long-term strength. (In Russ.)
  13. GOST 9.308-85. Unified system of corrosion and ageing protection. Metal and non-metal inorganic coatings. Methods for accelerated corrosion tests. (In Russ.)
  14. GOST 6032-2003. Corrosion-resistant steels and alloys. Test methods of intercrys-talline corrosion resistance. (In Russ.)
  15. GOST1497-84. Metals. Methods of tension test. (In Russ.)
  16. GOST 9651-84. Metals. Methods of tension tests at elevated temperatures. (In Russ.)
  17. ASTM E-8M «Standard Test Methods for Tension Testing of Metallic Materials».
  18. ASTM E-21 «Standard Test Methods for Elevated Temperature Tension Testing of Metallic Materials».
  19. GOST 10145-81. Metals. Stress-rupture test method. (In Russ.)
  20. GOST 3248-81. Metals. Creep test method. (In Russ.)
  21. ASTM E-139 «Standard Test Methods for Conducting Creep, Creep-Rupture, and Stress-Rupture Tests of Metallic Materials».
  22. GOST 25.502-79. Strength analysis and testing in machine building. Methods of metals mechanical testing. Methods of fa-tigue testing. (In Russ.)
  23. ASTM Е-606 «Standard Practice for Strain-Controlled Fatigue Testing».
  24. ASTM E-466 «Standard Practice for Conducting Force Controlled Constant Am-plitude Axial Fatigue Tests of Metallic Mate-rials».
  25. ASTM E-468 «Standard Practice for Presentation of Constant Amplitude Fatigue Tests Results for Metallic Materials».
  26. OST 1 021927-90. Metals. Method of determining the rate of growth of fatigue cracks in the test with constant amplitude load. (In Russ.)
  27. ASTM Е-647 «Standard Test Method for Measurement of Fatigue Crack Growth Rates».
  28. Lvovskiy B.N. Statisticheskie metody postroenia empiricheskich formul [Statistical methods for constructing empirical formulas]. Moscow: Vysshaya shkola Publ., 1982. 224 p.
  29. Kablov E.N., Golubovskiy E.R. Zharoprochnost nikelevysh splavov [Heat- resistant nickel alloys]. Moscow: Mashi-nostroenie Publ., 1998. 464 p.
  30. Structural strength of gas turbine en-gine materials and parts / еd. by I.A. Birger, B.F. Balashov. Moscow: Mashinostroenie Publ., 1981. 222 p.
  31. Kuevda V.K., Nozhnitsky Y.A. New approach for management of life of aviation engines and their main parts. Conversion in mashinbuilding of Russia. 2005. No 4-5. P. 79-82. (In Russ.)
  32. Nozhnitsky Y.A. Confirmation of life of aviation gas turbine engines and their crit-ical parts. Proc. of the third school-seminar «Modern problems of life of materials and structures». Moscow: Moscow State University of Mechanical Engineering (MAMI) Publ., 2000. P. 74-89. (In Russ.)

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies