首页> 外国专利> Fluid conduit arrangement for carrying gas in aero engine, has two spacers partially overlapped within compensator and connected by pivot joint, where one of spacers is integrally and freely connected with compensator

Fluid conduit arrangement for carrying gas in aero engine, has two spacers partially overlapped within compensator and connected by pivot joint, where one of spacers is integrally and freely connected with compensator

机译:用于在航空发动机中输送气体的流体导管装置,具有两个垫片,该垫片在补偿器内部分重叠,并通过枢轴接头连接,其中一个垫片与补偿器一体且自由地连接

摘要

The arrangement (1) has two spacers e.g. input line (10) and output line (11), movably formed relative to each other and connected by sliding joints and a pivot joint i.e. ball-and-socket joint, which is located between the sliding joints. One of the spacers is integrally and freely connected with a compensator (2) i.e. bellows, where the compensator and the spacers are manufactured by using a generative manufacturing method. The spacers are partially overlapped within the compensator. An aperture is axially provided within the compensator in a peripheral side of the spacers. An independent claim is also included for a method for manufacturing a fluid conduit arrangement.
机译:装置(1)具有两个间隔件,例如两个。输入线(10)和输出线(11)相对于彼此可移动地形成,并且通过滑动接头和位于滑动接头之间的枢轴接头即球窝接头连接。垫片之一与补偿器(2),即波纹管一体地且自由地连接,其中,补偿器和垫片是通过使用制造方法制造的。垫片在补偿器内部分重叠。在补偿器内,在隔离件的外周侧轴向设有孔。还包括用于制造流体导管装置的方法的独立权利要求。

著录项

  • 公开/公告号DE102012209835A1

    专利类型

  • 公开/公告日2013-12-12

    原文格式PDF

  • 申请/专利权人 MTU AERO ENGINES AG;

    申请/专利号DE201210209835

  • 发明设计人 JACKSON HUGH ALUN JOHN;

    申请日2012-06-12

  • 分类号F16L51/02;F16L21;F16L27/12;

  • 国家 DE

  • 入库时间 2022-08-21 15:37:42

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