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Mechanism for driving members for adjusting the orientation of blades

机译:用于驱动构件以调节叶片方向的机构

摘要

A drive mechanism (10) for driving a first adjustment member (12) for adjusting the orientation of the blades (14) of a first turbomachine rectifier stage (16) and a second adjustment member (18) for adjusting the orientation of the blades (20) of a second turbomachine rectifier stage (22), which comprises a mechanism for simultaneously moving the two adjustment members (12, 18) in the turbomachine, characterised in that it comprises a single drive wheel (24) that simultaneously drives the first adjustment member (12) and the second adjustment member (18) and comprises two gear stages (26, 28) that are arranged between the drive wheel (24) and one or the other of the first adjustment member (12) and the second adjustment member (18) and that have different transmission ratios.
机译:用于驱动第一调节构件( 12 )的驱动机构( 10 ),该第一调节构件用于调节第一涡轮机的叶片( 14 )的方向整流器级( 16 )和第二调节构件( 18 ),用于调节第二涡轮机整流器级的叶片( 20 )的方向( 22 ),其包括用于同时移动涡轮机中的两个调节构件( 12、18 )的机构,其特征在于,它包括单个驱动轮( 24 )同时驱动第一调节部件( 12 )和第二调节部件( 18 )并包括两个齿轮级( 26, 28 )布置在驱动轮( 24 )与第一调节构件( 12 )和第二调节构件(< B> 18 )并且具有不同的传动比。

著录项

  • 公开/公告号US10502088B2

    专利类型

  • 公开/公告日2019-12-10

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号US201515508751

  • 发明设计人 PIERRE-ALAIN FRANCIS CLAUDE SEBRECHT;

    申请日2015-09-03

  • 分类号F01D17/16;F04D29/56;

  • 国家 US

  • 入库时间 2022-08-21 11:24:14

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