发明名称 УСТРОЙСТВО ОХЛАЖДЕНИЯ ДИСКОВ ТУРБИН
摘要 The device has an upstream (32) and downstream annular plate (34) extending radially from upstream and downstream flanges (36, 38) of a lower platform, respectively. An airtight device (42) extends longitudinally between the plates to seal an annular cavity. Bolded links (83) maintain the upstream and downstream plates against the respective flanges. Holes (70) inject cooling air towards a turbine disc.
申请公布号 RU2004104120(A) 申请公布日期 2005.07.27
申请号 RU20040104120 申请日期 2004.02.13
申请人 СНЕКМА МОТОРС (FR) 发明人 ИМБУР Себастьен (FR);СУПИЗОН Жан-Люк (FR);ПАБЬОН Филипп (FR)
分类号 F02C1/00;F01D5/08;F01D11/02;F02C7/18;F16J15/447 主分类号 F02C1/00
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