2019
DOI: 10.1016/j.matpr.2019.07.073
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Effect of high energy ion-implantation treatment on properties of heat-resistant nickel alloys of blades of gas-compressor units

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Cited by 4 publications
(3 citation statements)
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“…The most loaded unit of aircraft engines is the blade of the first stage of the turbine, which, due to the high thermal stress and corrosion of the external environment, has a short service life of the aircraft engine as a whole [10,11,18,19].…”
Section: Steel Alloys In Aviationmentioning
confidence: 99%
“…The most loaded unit of aircraft engines is the blade of the first stage of the turbine, which, due to the high thermal stress and corrosion of the external environment, has a short service life of the aircraft engine as a whole [10,11,18,19].…”
Section: Steel Alloys In Aviationmentioning
confidence: 99%
“…Many publications appeared on the problems of aircraft construction and their materials. It is possible to list only dissertations completed in the last 2-3 years, where an bibliography is presented [6][7][8][9][10][11][12].…”
Section: Introductionmentioning
confidence: 99%
“…Owing to the use of such coatings, a higher operating efficiency of the turbine blades can be achieved, as less cooling air is needed to maintain the temperature of the blade or shroud. In addition, the service life of the parts increases, because the rate of change in the metal temperature decreases as a result of the heat-insulating effect [5].…”
Section: Introductionmentioning
confidence: 99%