发明名称 GAS TURBINE ENGINE COOLED BLADE
摘要 FIELD: engines and pumps.SUBSTANCE: claimed blade comprises the cooling medium feed cavities, non-metallic porous material powder and metallic material. Claimed blade is made by the ply-by-ply laser sintering of powder materials in 3D format. Every ply of said materials includes non-metallic porous permeable material reinforced by metallic material that makes an array shape to preset profile of the blade. The blade surface outer ply in contact with high-temperature incident flow of combustion products is made of non-metallic porous permeable material in depth not smaller than the side of cubic array structure. Zirconium dioxide is used as said non-metallic porous permeable material.EFFECT: longer thermal-fatigue life crack resistance, normal operating performances at flow temperature of up to 2000°.3 cl, 12 dwg
申请公布号 RU2568600(C1) 申请公布日期 2015.11.20
申请号 RU20140138766 申请日期 2014.09.24
申请人 AKTSIONERNOE OBSHCHESTVO "INZHINIRINGOVAJA KOMPANIJA "AEHM-TEKHNOLOGII" (AO "AEHM-TEKHNOLOGII") 发明人 TUMAKOV ALEKSEJ GRIGOR'EVICH;BAJGALIEV BORIS ERGAZOVICH
分类号 F01D5/18 主分类号 F01D5/18
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