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HELICOPTER MAST SPACER, HELICOPTER POWER TRANSMISSION SYSTEM EQUIPPED WITH SAME, AND HELICOPTER

机译:直升机桅杆间隔,装有相同组件的直升机动力传输系统和直升机

摘要

A mast spacer (20A) provided between a mast bearing and a mast nut in a main shaft of a helicopter, comprises a cylindrical spacer body (21). A first end of the mast spacer (20A) is a bearing contact end (22) which is fittable to an inner race of the mast bearing. For example, the bearing contact end is provided with bearing projections (23) which are fittable to recesses provided in the inner race of the mast bearing. The spacer body (21) is provided with slits, for example, a spiral slits (24) penetrating its side wall. The slits have a linear shape crossing an axial direction of the cylindrical spacer body (21).
机译:设置在直升飞机主轴上的桅杆轴承和桅杆螺母之间的桅杆间隔件(20A)包括圆柱形的间隔件主体(21)。桅杆间隔件(20A)的第一端是轴承接触端(22),该轴承接触端可装配到桅杆轴承的内圈。例如,轴承接触端设置有轴承凸起(23),该轴承凸起可装配到桅杆轴承的内圈中设置的凹槽中。隔离物主体(21)上设有缝隙,例如贯穿其侧壁的螺旋状的缝隙(24)。狭缝具有与圆筒形间隔件主体(21)的轴向交叉的直线形状。

著录项

  • 公开/公告号EP3378765B1

    专利类型

  • 公开/公告日2020-11-04

    原文格式PDF

  • 申请/专利权人 KAWASAKI JUKOGYO KABUSHIKI KAISHA;

    申请/专利号EP20160865930

  • 发明设计人 YAMAUCHI TOMOHIRO;OKADA HISASHI;

    申请日2016-11-15

  • 分类号B64C27/32;B64C27/12;F16C25/08;F16C33/58;

  • 国家 EP

  • 入库时间 2022-08-21 11:39:58

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