"485818" . . . "V sou\u010Dasn\u00FDch leteck\u00FDch motorech jsou turb\u00EDnov\u00E9 lopatky jedny z nejv\u00EDce nam\u00E1han\u00FDch vysokoteplotn\u00EDch sou\u010D\u00E1st\u00ED. Pracuj\u00ED za vysok\u00FDch teplot, okolo 800C, za st\u0159\u00EDdav\u00FDch nap\u011B\u0165ov\u00FDch podm\u00EDnek a ve velmi agresivn\u00ED atmosf\u00E9\u0159e. Proto mus\u00ED b\u00FDt vyrobeny z materi\u00E1lu, kter\u00FD t\u011Bmto vliv\u016Fm odol\u00E1v\u00E1, konkr\u00E9tn\u011B z niklov\u00FDch precipita\u010Dn\u011B zpevn\u011Bn\u00FDch superslitin . Aby byly lopatky co nejv\u00EDce chr\u00E1n\u011Bny proti vysokoteplotn\u00ED korozi a oxidaci jsou chr\u00E1n\u011Bny dif\u00FAzn\u00ED alitosilitovanou vrstvou."@cs . . . . "SK - Slovensk\u00E1 republika" . "35-38" . . . "S" . "turbine blades, ZHS6K, layer"@en . "1335-0803" . "The microstructural analysis of turbine blades made from alloy \u017DS6K"@en . "Mikrostrukturn\u00ED anal\u00FDza turb\u00EDnov\u00FDch lopatek ze superslitiny \u017DS6K"@cs . . "4"^^ . "The turbine blades of present aero jet planes are one of the most stressed parts of jet engine. Because of high working temperature (mostly up to 800C), centrifugal power and hot corrosion, the turbine blades must be made of material, which is able to work uder this conditions. Ni - base superalloys, thanks to its unique mechanical properties combination, are commonly used for production of these turbine blades. However, even Ni - base superalloys should be protected befor hot corrosion negative influence. To protect a turbine blade surface against hot corrosion influence diffusion alitize protective layer is used very often."@en . . "Belan, Juraj" . "2"^^ . "Posp\u00ED\u0161ilov\u00E1, Simona" . "1"^^ . "26210" . "Mikrostrukturn\u00ED anal\u00FDza turb\u00EDnov\u00FDch lopatek ze superslitiny \u017DS6K"@cs . "Mikrostrukturn\u00ED anal\u00FDza turb\u00EDnov\u00FDch lopatek ze superslitiny \u017DS6K" . "RIV/00216305:26210/06:PU59297!RIV07-MSM-26210___" . . "Materi\u00E1lov\u00E9 in\u017Einierstvo" . . "Mikrostrukturn\u00ED anal\u00FDza turb\u00EDnov\u00FDch lopatek ze superslitiny \u017DS6K" . "13" . . . "RIV/00216305:26210/06:PU59297" . "V sou\u010Dasn\u00FDch leteck\u00FDch motorech jsou turb\u00EDnov\u00E9 lopatky jedny z nejv\u00EDce nam\u00E1han\u00FDch vysokoteplotn\u00EDch sou\u010D\u00E1st\u00ED. Pracuj\u00ED za vysok\u00FDch teplot, okolo 800C, za st\u0159\u00EDdav\u00FDch nap\u011B\u0165ov\u00FDch podm\u00EDnek a ve velmi agresivn\u00ED atmosf\u00E9\u0159e. Proto mus\u00ED b\u00FDt vyrobeny z materi\u00E1lu, kter\u00FD t\u011Bmto vliv\u016Fm odol\u00E1v\u00E1, konkr\u00E9tn\u011B z niklov\u00FDch precipita\u010Dn\u011B zpevn\u011Bn\u00FDch superslitin . Aby byly lopatky co nejv\u00EDce chr\u00E1n\u011Bny proti vysokoteplotn\u00ED korozi a oxidaci jsou chr\u00E1n\u011Bny dif\u00FAzn\u00ED alitosilitovanou vrstvou." . "The microstructural analysis of turbine blades made from alloy \u017DS6K"@en . "[8C9CF5462BB8]" . . "2" .