Standard

Ultrafine-grained Ti-6Al-4V-alloy used for production of complex-shaped articles with enhanced service properties. / Semenova, I. P.; Raab, G. I.; Polyakova, V. V.; Izmailova, N. F.; Pavlinich, S. P.; Valiev, R. Z.

в: Reviews on Advanced Materials Science, Том 31, № 2, 30.11.2012, стр. 179-184.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Semenova, IP, Raab, GI, Polyakova, VV, Izmailova, NF, Pavlinich, SP & Valiev, RZ 2012, 'Ultrafine-grained Ti-6Al-4V-alloy used for production of complex-shaped articles with enhanced service properties', Reviews on Advanced Materials Science, Том. 31, № 2, стр. 179-184.

APA

Semenova, I. P., Raab, G. I., Polyakova, V. V., Izmailova, N. F., Pavlinich, S. P., & Valiev, R. Z. (2012). Ultrafine-grained Ti-6Al-4V-alloy used for production of complex-shaped articles with enhanced service properties. Reviews on Advanced Materials Science, 31(2), 179-184.

Vancouver

Semenova IP, Raab GI, Polyakova VV, Izmailova NF, Pavlinich SP, Valiev RZ. Ultrafine-grained Ti-6Al-4V-alloy used for production of complex-shaped articles with enhanced service properties. Reviews on Advanced Materials Science. 2012 Нояб. 30;31(2):179-184.

Author

Semenova, I. P. ; Raab, G. I. ; Polyakova, V. V. ; Izmailova, N. F. ; Pavlinich, S. P. ; Valiev, R. Z. / Ultrafine-grained Ti-6Al-4V-alloy used for production of complex-shaped articles with enhanced service properties. в: Reviews on Advanced Materials Science. 2012 ; Том 31, № 2. стр. 179-184.

BibTeX

@article{c1b8ba7aaec540bd8c14555ae91e948b,
title = "Ultrafine-grained Ti-6Al-4V-alloy used for production of complex-shaped articles with enhanced service properties",
abstract = "This work presents the results of investigation of microstructure and mechanical properties of gas-turbine engine (GTE) blades made from Ti-6Al-4V alloy with an ultrafine-grained (UFG) structure fabricated by means of severe plastic deformation. A possibility of efficient shaping of a blade out of the UFG alloy by means of isothermal stamping at lowered temperatures with retention of the UFG structure in a blade-item was demonstrated. Comparative fatigue tests of blades manufactured by conventional and pilot technologies were conducted, which demonstrated increase of the fatigue endurance in blades with the UFG structure by almost 30%. The V- and T-notch impact strength of pilot blades retained the increased values (no less than 320 and 210 KJ/m2, respectively).",
author = "Semenova, {I. P.} and Raab, {G. I.} and Polyakova, {V. V.} and Izmailova, {N. F.} and Pavlinich, {S. P.} and Valiev, {R. Z.}",
year = "2012",
month = nov,
day = "30",
language = "English",
volume = "31",
pages = "179--184",
journal = "Reviews on Advanced Materials Science",
issn = "1606-5131",
publisher = "Институт проблем машиноведения РАН",
number = "2",

}

RIS

TY - JOUR

T1 - Ultrafine-grained Ti-6Al-4V-alloy used for production of complex-shaped articles with enhanced service properties

AU - Semenova, I. P.

AU - Raab, G. I.

AU - Polyakova, V. V.

AU - Izmailova, N. F.

AU - Pavlinich, S. P.

AU - Valiev, R. Z.

PY - 2012/11/30

Y1 - 2012/11/30

N2 - This work presents the results of investigation of microstructure and mechanical properties of gas-turbine engine (GTE) blades made from Ti-6Al-4V alloy with an ultrafine-grained (UFG) structure fabricated by means of severe plastic deformation. A possibility of efficient shaping of a blade out of the UFG alloy by means of isothermal stamping at lowered temperatures with retention of the UFG structure in a blade-item was demonstrated. Comparative fatigue tests of blades manufactured by conventional and pilot technologies were conducted, which demonstrated increase of the fatigue endurance in blades with the UFG structure by almost 30%. The V- and T-notch impact strength of pilot blades retained the increased values (no less than 320 and 210 KJ/m2, respectively).

AB - This work presents the results of investigation of microstructure and mechanical properties of gas-turbine engine (GTE) blades made from Ti-6Al-4V alloy with an ultrafine-grained (UFG) structure fabricated by means of severe plastic deformation. A possibility of efficient shaping of a blade out of the UFG alloy by means of isothermal stamping at lowered temperatures with retention of the UFG structure in a blade-item was demonstrated. Comparative fatigue tests of blades manufactured by conventional and pilot technologies were conducted, which demonstrated increase of the fatigue endurance in blades with the UFG structure by almost 30%. The V- and T-notch impact strength of pilot blades retained the increased values (no less than 320 and 210 KJ/m2, respectively).

UR - http://www.scopus.com/inward/record.url?scp=84870035099&partnerID=8YFLogxK

M3 - Article

AN - SCOPUS:84870035099

VL - 31

SP - 179

EP - 184

JO - Reviews on Advanced Materials Science

JF - Reviews on Advanced Materials Science

SN - 1606-5131

IS - 2

ER -

ID: 35173006