发明名称 COOLING DEVICE FOR THE CASING OF AN AIRCRAFT JET ENGINE COMPRISING A SUPPORTING DEVICE
摘要 <p>The invention relates to a cooling device for the casing of a jet engine, said cooling device comprising a cooling tube and a supporting device, the supporting device comprising an attachment plate and an attachment clamp, the attachment clamp comprising a clamp body surrounding the cooling tube and an attachment element attached to the attachment plate, characterised in that the attachment plate comprises: an opening; and an attachment tab secured to said main wall of the attachment plate and arranged at one portion of the periphery of the opening, the attachment clamp passing through the opening, and the attachment element of said attachment clamp being attached to the attachment tab.</p>
申请公布号 WO2014131978(A1) 申请公布日期 2014.09.04
申请号 WO2014FR50388 申请日期 2014.02.25
申请人 SNECMA 发明人 COHIN, ARTHUR;ACHBARI, BAGHDAD;CHARRIE, AUDREY;MASSOT, AURÉLIEN, RENÉ-PIERRE
分类号 F01D11/24 主分类号 F01D11/24
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