发明名称 ЗАДНЕЕ КРЕПЛЕНИЕ АВИАЦИОННОГО ДВИГАТЕЛЯ С ТЯГАМИ И РЫЧАГОМ В ФОРМЕ БУМЕРАНГА
摘要 The system has a cross-bar (15) fixed to a fitting, in its central part, by a connecting unit with a pivotal axis. The unit has two connections on the central part cooperating with a mounting lug (130) on the fitting. Each of two thrust acceleration connecting rods is connected to a back of the cross-bar by another connecting unit. The cross-bar comprises of connecting units (155-135, 157-137) with a mast. The latter connecting unit is constituted of a lateral mounting lug (155) of the cross-bar and a clevis mounting (200). The connecting units (155-135, 157-137) are constituted of lateral mounting lugs (155, 157) of the cross-bar and clevis mountings (135, 137), respectively.
申请公布号 RU2004119904(A) 申请公布日期 2005.12.10
申请号 RU20040119904 申请日期 2004.06.29
申请人 СНЕКМА МОТЕР (FR) 发明人 ЛЕВЕНШТЕЙН Филипп (FR);ДАРСИ Фредерик Жан-Марк (FR);ТЕНЬЕР Марк (FR)
分类号 B64D27/16;B64C1/16;B64D27/26 主分类号 B64D27/16
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