首页> 外国专利> MAIN ROTOR BLADE, ADVANTAGEOUS TO PRODUCTION PROCESS, PRICE COMPETITIVENESS, QUALITY AND ENVIRONMENT, FOR HELICOPTER AND MANUFACTURING METHOD THEREOF

MAIN ROTOR BLADE, ADVANTAGEOUS TO PRODUCTION PROCESS, PRICE COMPETITIVENESS, QUALITY AND ENVIRONMENT, FOR HELICOPTER AND MANUFACTURING METHOD THEREOF

机译:主要旋翼桨叶,适用于生产过程,价格竞争力,质量和环境,适用于直升机及其制造方法

摘要

Purpose: a main rotor blades are provided for the helicopter and a manufacturing method of the main rotor blades for helicopter, it can obtain effect, such as the shortening of production process, pass through improvement, quality improvement and the environmental protection of the price competitiveness of sizable difference compared with existing material and manufacturing method. Construction: manufacturing method includes that a piece of sword of a manufacturing process (4) passes through in one forging rate of the first solid-state extrusion; Cutting edge stretches sword and distorts sword to a desired angle, after the both ends of clamping reduction sword are to a stenter stationary jaw (5) and a stenter moving jaw (6) to the process of certain length; The mobile process of stretching, extension twisted blade is rebounded according to the forming process of sword; Torsion angle expected from a manufacturing process main rotor blades by heat treatment checks main rotor blades and finally checks heat treated main rotor blades, after the expected torsion angle for checking the main rotor blades manufactured by stretching process. It can include that a piece of sword of manufacturing process (4) passes through in the first solid-state extrusion forging rate by manufacturing method that formula, which distorts the manufacture of aluminium main rotor blades,; Cutting edge stretches sword and distorts sword to desired angle, after the both ends of clamping reduction sword are to stretcher leveler stationary jaw (5) and stretcher leveler moving jaw (6) to the process of certain length; The mobile process of stretching, extension twisted blade is rebounded according to the forming process of sword; Pass through the manufacturing process main rotor blades torsion angle inspection of heat treatment and manipulates main rotor blades and finally check heat treated main rotor blades after the torsion angle for checking main rotor blades manufacture by stretching process and manipulate torsion angle inspection main rotor blades.
机译:目的:为直升机提供主旋翼及其制造方法,可以达到缩短生产工艺,经过改进,质量提高和价格竞争的环境保护等作用。与现有材料和制造方法相比有很大的差异。构造:制造方法包括:以第一固态挤压的一个锻造速率通过制造工序(4)的剑;切刀将剑的两端伸至展幅机固定钳口(5)和展幅机移动钳口(6)至一定长度的过程后,将剑伸开并扭曲成所需角度。伸缩,伸展扭曲刀片的移动过程根据剑的形成过程而反弹;在通过制造工序对主转子叶片进行热处理时所期望的扭转角在检查用于对通过拉伸加工而制造的主转子叶片的期望扭转角之后,检查主转子叶片,并最终对热处理后的主转子叶片进行检查。可以包括通过以下公式的制造方法以第一固态挤压锻造速率通过制造工艺(4)的一剑,该公式扭曲了铝主动叶片的制造;刃口将剑伸开并扭曲至所需角度,夹紧复位剑的两端分别向担架校平器固定爪(5)和担架校直器移动爪(6)至一定长度的过程;伸缩,伸展扭曲刀片的移动过程根据剑的形成过程而反弹;通过制造过程中主转子叶片的扭转角热处理检查,并操纵主转子叶片,最后在扭转角之后检查热处理过的主转子叶片,以通过拉伸过程检查主转子叶片的制造,并操纵扭转角检查主转子叶片。

著录项

  • 公开/公告号KR20040092616A

    专利类型

  • 公开/公告日2004-11-04

    原文格式PDF

  • 申请/专利权人 HANSUNG ILS CO. LTD.;KYUNGNAM METAL CO. LTD.;

    申请/专利号KR20030026112

  • 发明设计人 JUNG U YEONG;

    申请日2003-04-24

  • 分类号B21D53/78;

  • 国家 KR

  • 入库时间 2022-08-21 22:47:42

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