首页> 外国专利> Jet engine for airplane, has tube with one end mounted in exhaust opening by ball joint connection free in rotation and locked in translation, and another end mounted in jambs orifice by connection free in rotation and translation

Jet engine for airplane, has tube with one end mounted in exhaust opening by ball joint connection free in rotation and locked in translation, and another end mounted in jambs orifice by connection free in rotation and translation

机译:飞机的喷气发动机,其管的一端通过球形接头自由旋转地安装在排气口并锁定在平移中,而另一端通过自由旋转的平移连接而安装在门框孔中。

摘要

The engine has a jamb connected to an external case of a diffuser grid and an external shell (14) of the engine casing. A tube is placed between an orifice (22) of the jamb and an exhaust opening (23) of the shell. An end (61) of the tube is mounted in the opening by a ball joint connection free in rotation and locked in translation. An end (63) of the tube is mounted in the orifice by the connection free in rotation and translation.
机译:发动机具有连接至扩散器格栅的外壳和发动机壳体的外壳(14)的侧柱。将管放置在侧柱的孔口(22)和壳体的排气口(23)之间。管的端部(61)通过自由旋转并平移锁定的球形接头连接安装在开口中。管的端部(63)通过自由旋转和平移的连接安装在孔中。

著录项

  • 公开/公告号FR2860041A1

    专利类型

  • 公开/公告日2005-03-25

    原文格式PDF

  • 申请/专利权人 SNECMA MOTEURS;

    申请/专利号FR20030011064

  • 发明设计人 LEPRETRE GILLES;

    申请日2003-09-22

  • 分类号F02C7/00;

  • 国家 FR

  • 入库时间 2022-08-21 21:58:21

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