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The turbomachinery module is composed of propeller and stator blades, which are supported by fixed devices and corresponding turbomachinery

机译:涡轮机械模块由螺旋桨和定子刀片组成,该刀片由固定装置和相应的涡轮机器支撑

摘要

Title: turbine module, consisting of propeller and stator blades, supported by fixtures and corresponding turbinesThe invention relates to an X-axis longitudinal axis turbomachinery module, comprising:An unprocessed propeller (2) for rotation about the longitudinal axis X,At least one rectifier (3) comprising a plurality of stator blades (23) extending substantially along the radial Z axis, each stator blade (23) comprising a blade (24) rising radially from the blade (25), andThe stator blades (23) surround a pitch system (34) passing through the timing shaft a at the bottom (25) of each stator blade (23),According to the invention, at least two adjacent stator blades (23) are connected to each other through at least one fixing piece (37) coupled to the blade (24) of the stator blade (23) through at least one pivot (42), and are installed radially away from the foot (25) of the stator blade (23),The pivot (42) extends along the pivot B coaxial with the timing shaft a, which aims to pivot the stator blade (23) around the pivot B, and includes an anti vibration device (55) of the pivot (42).Summary figure: Figure 2
机译:标题:由螺旋桨和定子叶片组成的涡轮模块,由固定装置和相应的涡轮部门支撑涉及X轴纵向轴线涡轮机械模块,包括:绕纵向轴线X,至少一个整流器绕旋转的未处理的螺旋桨(2) (3)包括多个定子叶片(23)基本上沿径向Z轴延伸,每个定子叶片(23)包括从叶片(25)径向上升的叶片(24),并且定子叶片(23)围绕间距根据本发明的通过至少两个固定件( 37)连接到定子叶片(23)的叶片(24)通过至少一个枢轴(42),并且枢轴(42)径向远离定子叶片(23)的脚(25)安装,枢轴(42)延伸沿着枢轴B与定时轴A同轴,这旨在PIV围绕枢轴B围绕定子叶片(23),包括枢轴(42)的抗振动装置(55)。样品图:图2

著录项

  • 公开/公告号FR3112809A1

    专利类型

  • 公开/公告日2022-01-28

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号FR2007783

  • 发明设计人 GILLES ALAIN MARIE CHARIER;

    申请日2020-07-23

  • 分类号F01D9/02;F01D5/26;F02K3/02;

  • 国家 FR

  • 入库时间 2022-08-24 23:34:31

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