发明名称 Turbomachine casing comprising a cavity-free shroud and yokes reinforced by stiffeners
摘要 The invention relates to a turbomachine casing (1) comprising: a hub (2), an outer shroud (3), and yokes (11) projecting from the outer shroud (3), for attaching the housing (1), characterised in that it comprises at least one stiffener (10) extending between pairs of yokes (11) facing each other, and comprising a central part (18) and side arms (19) projecting from the central part (18).
申请公布号 GB201614257(D0) 申请公布日期 2016.11.09
申请号 GB20160014257 申请日期 2015.01.20
申请人 Safran Aircraft Engines 发明人
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