2015
DOI: 10.3103/s1067821215030190
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Application of high-current pulsed electron beams for the restoration of operational properties of the blades of gas-turbine engines

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Cited by 8 publications
(6 citation statements)
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“…This is indicated by the presence of the following crater types: multi-ring, adjacent and nick-like. It is known (Shulov et al, 2015) that craters of such types are the most dangerous with respect to corrosion resistance (Figure 6).…”
Section: Resultsmentioning
confidence: 99%
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“…This is indicated by the presence of the following crater types: multi-ring, adjacent and nick-like. It is known (Shulov et al, 2015) that craters of such types are the most dangerous with respect to corrosion resistance (Figure 6).…”
Section: Resultsmentioning
confidence: 99%
“…analysis of the performed investigations shows (Kablov, 2001;Shulov et al, 2010;Shulov et al, 2013;Shulov et al, 2015;Kosmin and Budinovsky, 2016) that both character and intensity of turbine blade damages at high temperature corrosion are determined by the following factors: (i) anti-corrosion properties of protective coatings, (ii) level of active static and vibration loads, (iii) operating temperature of turbine blades, as well as (iv) concentration of corrosion-active substances in fuel combustion products. In some cases, high-temperature corrosion acts as an independent disturbing factor (Budinovskii and Muboyadzhan, 2003;Shejko et al, 2017;Ivanov et al, 2018;Braceras et al, 2018).…”
Section: Anmentioning
confidence: 98%
“…However, for every 1% reduction in efficiency, the fuel consumption of the aero-engine will increase by 2%. Therefore, it is necessary to monitor the blade tip clearance in real-time to obtain the blade operation status in advance and provide a strong guarantee for the safe operation of the aero-engine [4] .…”
Section: Introductionmentioning
confidence: 99%
“…However, for every 1% reduction in efficiency, the fuel consumption of the aero-engine will increase by 2%. Therefore, it is necessary to monitor the blade tip clearance in real-time to obtain the blade operation status in advance and provide a strong guarantee for the safe operation of the aero-engine [4] .The common measurement methods of tip clearance include probe measurement, capacitance measurement, eddy current measurement, microwave measurement, ultrasonic measurement, reflection intensity measurement, interference intensity measurement, and laser measurement [5] . The optical fiber measurement method has a fast response, strong anti-electromagnetic interference ability, and high reliability, and is suitable for working in harsh, high-temperature, and high-pressure environments.…”
mentioning
confidence: 99%
“…At present, special attention is paid to the development of high-intensity methods of surface engineering of engineering parts of a fairly wide range, as well as their extremely rapid implementation of technological processes created on their basis in the industry. One of the demanded tools for surface engineering can be using high-current pulsed electron beams (HCPEB) of microsecond duration to modify the surface and near-surface layers of parts (Novikov et al, 2010;Uglov et al, 2011;Shulov et al, 2012;Gromov et al, 2013;Shulov et al, 2014;Shulov et al, 2015). The study of the effect of HCPEB irradiation on the surface of the layers of the heatresistant multicomponent ion-plasma coating Ni-Cr-Al-Y under various conditions, as well as the analysis of structural-phase changes occurring upon modification, were the objectives of this work.…”
Section: Introductionmentioning
confidence: 99%