THE PRINCIPLES OF FATIGUE APPROVAL FOR TRANSPORT AIRCRAFT AFTER ITS PRINCIPAL STRUCTURE ELEMENTS MODIFICATION

机译：修改主结构元素后运输飞机的疲劳认可原则

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

During modification aircraft structure ispossible as new critical areas in redesignedstructure parts, so too new spectrum aircraftapplying, as a consequence - new load spectrumfor initial structure parts. For compliance withairworthiness requirements, from the fatiguepoint of view, proposing to use bunch of finalelement analyses (linear static) together withengineer-analytical analyses. Effective stressconcentration to have estimate through design,analyses, fatigue test of “design-like” sampleswith typical for this aircraft joints (bolts, rivets).The estimation of maintenance conditionsaircrafts with redesigned structure concerningvariable loads can perform by applying “LoadMonitoring System” (LMS), based on FDR(Flight Data Recorder) information or specialsystem.

机译：改装过程中飞机的结构是重新设计中可能成为新的关键区域结构零件，也是如此新的频谱飞机结果是应用了新的负载谱用于初始结构零件。为了符合来自疲劳的适航要求观点，建议使用一堆最终的元素分析（线性静态）以及工程师分析分析。有效压力通过设计进行估算的浓度，分析，“样样”样品的疲劳测试与该飞机的典型接头（螺栓，铆钉）。维修条件的估算重新设计结构的飞机可变载荷可以通过应用“载荷基于FDR的“监控系统”（LMS）（飞行数据记录器）信息或特殊系统。

著录项

来源
《Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences》|2014年|1-5|共5页
会议地点
作者
V. I. Kleptsov;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类
关键词
aircraft; modification; fatique; analyses; test;

机译：飞机;改装;疲劳;分析;测试;

相似文献

外文文献
中文文献
专利

1. Advanced damage tolerance and risk analysis methodologies and tools for aircraft structures containing multiple-site and multiple-element fatigue damages [J] . M Liao, Y Bombardier, G Renaud, Proceedings of the Institution of Mechanical Engineers . 2012,第G11期

机译：包含多点和多元素疲劳损伤的飞机结构的高级损伤承受能力和风险分析方法和工具
2. Application of Finite Element Method for Determining Loads for the New Method of Acoustic Fatigue Testing of Aircraft Structures [J] . Andrzej Szot, Antoni Niepokólczycki Fatigue of Aircraft Structures . 2010,第1期

机译：有限元法在飞机结构声疲劳试验新方法中确定载荷的应用
3. An elastic-plastic finite element alternating method for analyzing wide-spread fatigue damage in aircraft structures [J] . C. R. Pyo, H. Okada, S. N. Atluri Computational Mechanics . 1995,第1期

机译：飞机结构广泛疲劳损伤的弹塑性有限元交替法
4. THE PRINCIPLES OF FATIGUE APPROVAL FOR TRANSPORT AIRCRAFT AFTER ITS PRINCIPAL STRUCTURE ELEMENTS MODIFICATION [C] . V. I. Kleptsov Congress of the International Council of the Aeronautical Sciences . 2014

机译：经线结构元素修改后运输机疲劳批准原则
5. Delamination Arrest by Fasteners in Aircraft Structures Under Static and Fatigue Loading. [D] . Richard, Luke. 2017

机译：在静态和疲劳载荷下飞机结构中紧固件的分层脱扣。
6. Effects of Doped Elements (Si Cr W and Nb) on the Stability Mechanical Properties and Electronic Structures of MoAlB Phase by the First-Principles Calculation [O] . Yongxin Jian, Zhifu Huang, Yu Wang, 2020

机译：掺杂元素（SiCrW和Nb）对第一原理计算的MoALB相位稳定性力学性能和电子结构的影响
7. Application of Finite Element Method for Determining Loads for the New Method of Acoustic Fatigue Testing of Aircraft Structures [O] . Antoni Niepokólczycki, Andrzej Szot 2009

机译：有限元法测定用于飞机结构的声学疲劳试验新方法的负载

THE PRINCIPLES OF FATIGUE APPROVAL FOR TRANSPORT AIRCRAFT AFTER ITS PRINCIPAL STRUCTURE ELEMENTS MODIFICATION

摘要

著录项

相似文献

相关主题

期刊订阅