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Helicopter rotor blade adjustment installation - for remote controlled helicopter models and having cylinder shaped pressure spring with adjustable length

机译:直升机旋翼桨叶调节装置-用于遥控直升机模型,并具有长度可调的圆柱状压力弹簧

摘要

The blade adjustment installation for helicopter rotors, preferably remote controlled models has the rotor blades turnable in relation to the rotor seesaw. The latter are fitted with rotor attachments in which the rotor connectors are axially supported and inserted both turnable and fixable. The walling of the pipe shaped rotor attachments (2) have two slots (3, 3') lying opposite each other which are offset against each other in screw shape with a guide bolt running through them attached to the rotor connector (5). A cylinder shaped pressure spring (6) is supported between the guide bolt (4) and the pipe shaped attachment (2) with its length adjustable during axial movement of the rotor blade.
机译:用于直升机旋翼的叶片调节装置,最好是遥控模型,其旋翼叶片可相对于旋翼跷跷板旋转。后者装有转子附件,转子连接器在其中轴向支撑并可旋转和固定地插入其中。管形转子附件(2)的壁具有彼此相对的两个狭槽(3、3'),该狭槽以螺钉形状彼此偏置,并且穿过它们的导向螺栓附接到转子连接器(5)。圆柱形压力弹簧(6)支撑在导向螺栓(4)和管状附件(2)之间,其长度在转子叶片轴向运动期间可调节。

著录项

  • 公开/公告号DE2433801A1

    专利类型

  • 公开/公告日1976-05-26

    原文格式PDF

  • 申请/专利权人 PELZL ERNST 8207 HEMHOF;

    申请/专利号DE19742433801

  • 发明设计人 PELZL ERNST 8207 HEMHOF;

    申请日1974-07-13

  • 分类号B64C27/54;A63H27/12;

  • 国家 DE

  • 入库时间 2022-08-23 02:05:38

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