发明名称 dispositivo de suspensão de um turborreator
摘要 A turbojet is suspended by attachments including hinged links. An attachment includes a support including three branches with passages through which a pin passes, the pin being oriented generally parallel to a direction that is tangential to a casing and being hinged to a central branch of the support by a ball joint.
申请公布号 BR112013015196(A2) 申请公布日期 2016.09.13
申请号 BR20131115196 申请日期 2011.12.20
申请人 SNECMA 发明人 THOMAS ALAIN CHRISTIAN VINCENT;WOUTER BALK
分类号 B64D27/18;B64D27/26 主分类号 B64D27/18
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