发明名称 ASSEMBLY OF GAS TURBINE ENGINE DISC AND SUPPORTING JOURNAL OF SUPPORTING BEARING; COOLING CIRCUIT OF TURBINE DISC OF SUCH ASSEMBLY
摘要 FIELD: machine building.SUBSTANCE: turbine disc includes an annular fastening flange rigidly attached to a radial annular part of a journal by means of bolts. Bolts subsequently pass through fastening holes made in a radial annular fastening flange of the turbine disc and in the radial annular part of the journal. Radial annular part of the journal includes through holes for air circulation between the journal inlet and outlet. Holes are made between fastening holes of the journal. Another object of this invention is a cooling circuit of the turbine disc in a gas turbine engine, which includes a removal channel at the turbine disc outlet, which passes through the above described holes.EFFECT: invention allows passage of ventilation air between the journal inlet and outlet.10 cl, 6 dwg
申请公布号 RU2504661(C2) 申请公布日期 2014.01.20
申请号 RU20100154117 申请日期 2009.05.29
申请人 SNEKMA 发明人 BONNO DAM'EN;GAREHN FABRIS;ZHJUDE MORIS GI;LANZHEVEN TOMA
分类号 F01D5/08 主分类号 F01D5/08
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