首页> 外国专利> Hydraulic accumulator for hydraulic circuit of aircraft, has outer envelope welded on base, and bayonet system assuring mechanical connections for maintaining envelope and base, where system has pin surrounding upper end of base

Hydraulic accumulator for hydraulic circuit of aircraft, has outer envelope welded on base, and bayonet system assuring mechanical connections for maintaining envelope and base, where system has pin surrounding upper end of base

机译:用于飞机液压回路的液压蓄能器,其外部外壳焊接在基座上,卡口系统可确保机械连接以维持外壳和基座,其中系统的销钉围绕基座的上端

摘要

The accumulator (1) has an outer envelope (3) welded on a base (2), and a bayonet system assuring mechanical connections for maintaining the envelope and the base. The envelope has an end (7) including a part (10) provided with an inner wall. The system has a pin (13) surrounding an upper end (6) of the base, and a pin (14) located on the inner wall. A mechanical locking system locks position of the former pin with respect to the latter pin.
机译:蓄能器(1)具有一个焊接在基座(2)上的外壳(3),以及一个卡口系统,可确保用于保持外壳和基座的机械连接。外壳的一端(7)包括具有内壁的部分(10)。该系统具有围绕基座的上端(6)的销(13)和位于内壁上的销(14)。机械锁定系统将前一个销相对于后一个销的位置锁定。

著录项

  • 公开/公告号FR2909733A1

    专利类型

  • 公开/公告日2008-06-13

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE SOCIETE ANONYME;

    申请/专利号FR20060055355

  • 发明设计人 GEORGET GREGORY;

    申请日2006-12-07

  • 分类号F15B1/04;B64D47/00;

  • 国家 FR

  • 入库时间 2022-08-21 19:47:07

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