仪器仪表用户2024,Vol.31Issue(7) :22-24.DOI:10.3969/j.issn.1671-1041.2024.07.008

探讨飞机发动机减震器模具设计

Exploring the Mold Design of Aircraft Engine Shock Absorbers

李文清 田绍熙
仪器仪表用户2024,Vol.31Issue(7) :22-24.DOI:10.3969/j.issn.1671-1041.2024.07.008

探讨飞机发动机减震器模具设计

Exploring the Mold Design of Aircraft Engine Shock Absorbers

李文清 1田绍熙2
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作者信息

  • 1. 贵州航天精工制造有限公司,贵州遵义 563006
  • 2. 贵州航天精工制造有限公司,贵州 遵义563006
  • 折叠

摘要

飞机发动机减震器是维系飞机飞行安全,保证乘客乘机舒适度的关键部件.为了保证飞机发动机减震器生产高效、高质,模具设计成为行业关注的焦点.本文基于此,简要概述飞机发动机减震器结构特点、工作原理以及对模具设计的特殊要求,重点提出一套系统性的模具设计方案,旨在为飞机发动机减震器设计与生产提供借鉴.

Abstract

The shock absorber of an aircraft engine is a critical component that maintains the safety of aircraft flight and ensures passenger comfort.To ensure efficient and high-quality production of aircraft engine shock absorbers,mold design has become a focus of attention in the industry.Based on this,this article briefly summarizes the structural characteristics,working principles,and special requirements for mold design of aircraft engine shock absorbers.It focuses on proposing a systematic mold design scheme,aiming to provide a reference for the design and production of aircraft engine shock absorbers.

关键词

飞机发动机/减震器/模具设计

Key words

aircraft engine/shock absorber/mold design

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出版年

2024
仪器仪表用户
天津仪表集团有限公司,中国仪器仪表学会节能技术应用分会

仪器仪表用户

影响因子:0.255
ISSN:1671-1041
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