Standard

Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines. / Kuznetsov, V. p.; Lesnikov, V. p.; Muboyadzhyan, S. a. et al.
In: Metal Science and Heat Treatment, Vol. 49, No. 5-6, 01.05.2007, p. 253-259.

Research output: Contribution to journal › Article › peer-review

Harvard

Kuznetsov, VP, Lesnikov, VP, Muboyadzhyan, SA & Repina, OV 2007, 'Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines', Metal Science and Heat Treatment, vol. 49, no. 5-6, pp. 253-259. https://doi.org/10.1007/s11041-007-0045-2

APA

Kuznetsov, V. P., Lesnikov, V. P., Muboyadzhyan, S. A., & Repina, O. V. (2007). Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines. Metal Science and Heat Treatment, 49(5-6), 253-259. https://doi.org/10.1007/s11041-007-0045-2

Vancouver

Kuznetsov VP, Lesnikov VP, Muboyadzhyan SA, Repina OV. Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines. Metal Science and Heat Treatment. 2007 May 1;49(5-6):253-259. doi: 10.1007/s11041-007-0045-2

Author

Kuznetsov, V. p. ; Lesnikov, V. p. ; Muboyadzhyan, S. a. et al. / Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines. In: Metal Science and Heat Treatment. 2007 ; Vol. 49, No. 5-6. pp. 253-259.

BibTeX

@article{f4e226442aec4b3c841a72088040e4d6,
title = "Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines",
abstract = "Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a ZrO 2: Y 2O 3 ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100-1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. ",
author = "Kuznetsov, {V. p.} and Lesnikov, {V. p.} and Muboyadzhyan, {S. a.} and Repina, {O. v.}",
year = "2007",
month = may,
day = "1",
doi = "10.1007/s11041-007-0045-2",
language = "English",
volume = "49",
pages = "253--259",
journal = "Metal Science and Heat Treatment",
issn = "0026-0673",
publisher = "Springer",
number = "5-6",

}

RIS

TY - JOUR

T1 - Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines

AU - Kuznetsov, V. p.

AU - Lesnikov, V. p.

AU - Muboyadzhyan, S. a.

AU - Repina, O. v.

PY - 2007/5/1

Y1 - 2007/5/1

N2 - Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a ZrO 2: Y 2O 3 ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100-1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described.

AB - Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a ZrO 2: Y 2O 3 ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100-1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described.

UR - https://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcAuth=tsmetrics&SrcApp=tsm_test&DestApp=WOS_CPL&DestLinkType=FullRecord&KeyUT=000251500300008

UR - http://www.scopus.com/inward/record.url?partnerID=8YFLogxK&scp=36849086435

U2 - 10.1007/s11041-007-0045-2

DO - 10.1007/s11041-007-0045-2

M3 - Article

VL - 49

SP - 253

EP - 259

JO - Metal Science and Heat Treatment

JF - Metal Science and Heat Treatment

SN - 0026-0673

IS - 5-6

ER -

ID: 41254814