发明名称 Intermediate casing for a turbofan engine
摘要 An intermediate casing comprising an inner annular hub, an outer annular barrel and an annular part for separating flows situated between the hub and the outer barrel. A primary stream is delimited between the hub and the separation part. A secondary stream is delimited between the separation part and the outer barrel. At least one hollow arm extends radially from the hub to the outer barrel, passing through the primary and secondary streams. A transmission shaft extends radially in the hollow arm. The hollow arm comprises a hydraulic-fluid outlet situated downstream of the transmission shaft. The arm further comprises a bypass channel or pocket able to bypass the transmission shaft.
申请公布号 GB201512008(D0) 申请公布日期 2015.08.19
申请号 GB20150012008 申请日期 2015.07.09
申请人 SNECMA 发明人
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代理机构 代理人
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