Журнал Российского общества по неразрушающему контролю и технической диагностике
The journal of the Russian society for non-destructive testing and technical diagnostic
 
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23 | 11 | 2024
2016, 07 July

DOI: 10.14489/td.2016.07.pp.061-067

 

Lozhkova D.S., Krasnov I.S., Dalin М.А.
ESTIMATION OF DEFECT OF BBLANKS GTE WHEELS OF TITANIUM ALLOYS
(pp. 61-67)

Abstract. The questions of gas turbine engine titanium alloy bars and disks exceedence evaluation are observed in this paper. The “exceedence” concept is defined. It characterizes the probable defects of known or greater than known size content at known quantity of material after non-destructive evaluation. This work is devoted to titanium bars hard alpha inclusions because they are the most dangerous. Some approaches allowing to evaluate gas turbine engine titanium alloy bars and disks exceedence are observed. They differ from each other and depend on the defect detection statistic data availability. For each approaches the plotting algorithm of probability of exceedence versus anomaly area continuous curves at known quantity of material is described. Computing experiments confirming their working capacity are made. As result of saving experience and making experiments general methodology of gas turbine critical parts metallurgy defects content quantity evaluation is developed.

Keywords: exceedence, ultrasonic testing, gas turbine engine, titanium alloy, engine critical parts.

 

 D. S. Lozhkova, I. S. Krasnov, M. A. Dalin (All-Russian Scientific Research Institute of Aviation Materials, Moscow, Russia) E-mail: Данный адрес e-mail защищен от спам-ботов, Вам необходимо включить Javascript для его просмотра.

 

 

1. Nochovnaia N. A. (2007). Prospects and problems of titanium alloys usage. Aviatsionnye materialy i tekhnologii. Vypusk Perspektivy razvitiia i primeneniia titanovykh splavov dlia samoletov, raket, dvigatelei i sudov, (1), pp. 4-8. Moscow: VIAM. [in Russian language]
2. Kashapov O. S., Novak A. V., Nochovnaia N. A., Pavlova T. V. (2013). State, problems and prospects of development of heat-resistant titanium alloys for GTE parts. Trudy VIAM, (3), article No. 02. Available at: viam-works.ru (Accessed: 22.01.2016). [in Russian language]
3. Kablov E. N., Ospennikova O. G., Bazyleva O. A. (2011). Materials for high thermal loaded parts of GTE. Vestnik MGTU im. N. E. Baumana. Seriia Mashinostroenie, (2), pp. 13-19. [in Russian language]
4. Kablov E. N. (2012). Strategic directions of development of materials and technologies of their processing for the period until 2030. Aviatsionnye materialy i tekhnologii, (S), pp. 7-17. [in Russian language]
5. Kablov E. N. (2012). Modern materials - the basis of innovative modernization of Russia. Metally Evrazii, (3), pp. 10 – 15. [in Russian language]
6. Khorev A. I. (2013). Fundamental and applied works on structural titanium alloys and promising directions of their development. Trudy VIAM, (2), article No. 04. [in Russian language] Available at: viam-works.ru (Accessed: 22.01.2016)
7. Inozemtsev A. A., Bashkatov I. G., Koriakovtsev A. S. (2007). Application of alloys based on titanium in products developed by JSC «Aviadvigatel». Aviatsionnye materialy i tekhnologii. Vypusk Perspektivy razvitiia i primeneniia titanovykh splavov dlia samoletov, raket, dvigatelei i sudov, (1), pp. 13-16. [in Russian language]
8. Norms of airworthiness of aircraft engines. (2012). Aviation rules. Part 33. Interstate aviation Committee. (pp. 7-11). Moscow: Aviaizdat. [in Russian language]
9. Kablov E. N. (2015). Innovation developments of FSUE «All-Russian Scientific Institute of Aviation Materials» of the State Research Center of the Russian Federation on implementation «Strategic directions of development of materials and processing technologies for the period up to 2030». Aviatsionnye materialy i tekhnologii, (1), pp. 3 – 33. [in Russian language]
10. An executive update on the turbine rotor material design (TRMD) program. (2003). 6th Annual FAA/Air Force/NASA/Navy Workshop on the Application of Probabilistic Methods to Gas Turbine Engines 18-20 March 2003.
11. FAA Advisory Circular: AC 33.14-1, titled «Damage Tolerance for High Energy Turbine Engine Rotors». (2001). Washington, U.S. Dpt of Transportation, Federal Aviation Administration.
12. Lozhkova D. S., Krasnov I. S. (2015). Experimental studies on the evaluation of the defectiveness of weld joints of the main parts of GTEs. Defektoskopiia, (2), pp. 10-16. [in Russian language]
13. Antipov V. V. (2012). The development strategy of titanium, magnesium, beryllium and aluminum alloys. Aviatsionnye materialy i tekhnologii, (5), pp. 157-167. [in Russian language]
14. Lozhkova D. S., Dalin M. A., Tsykunov N. V. (2014). Reliability evaluation of titanium alloys automated ultrasonic inspection using mathematical modeling. V mire nerazrushaiushchego kontrolia, (6), pp. 24-28. [in Russian language]
15. Dalin M. A., Generalov A. S., Boichuk A. S., Lozhkova D. S. (2013). Main trends in the development of acoustic methods of non-destructive testing. Aviatsionnye materialy i tekhnologii, (1), pp. 64-68. [in Russian language]
16. Ivchenko G. I., Medvedev Iu. I. (1984). Mathematical statistics. Moscow: Vysshaia shkola. [in Russian language

 

 

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