Preliminary Assessment of the Weight of the Aircraft Fuselage as a Result of the Transition to Composite Materials

A. S. Kretov; P. A. Shataev

首页> 外文期刊>Russian Aeronautics >Preliminary Assessment of the Weight of the Aircraft Fuselage as a Result of the Transition to Composite Materials

【24h】

Preliminary Assessment of the Weight of the Aircraft Fuselage as a Result of the Transition to Composite Materials

机译：由于过渡到复合材料的导致飞机机身重量的初步评估

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

The problem of estimating the weight of the fuselage for the initial stages of design as a result of using new materials and new design solutions is considered. The approach is based on the V.A. Komarov's weight formula. A design method for estimating the CK coefficients of the load-carrying factor for real structures is proposed. The comparison of the CK for various components of loads in relation to conventional metal and composite structures is performed. A numerical analysis is performed in terms of a medium-haul aircraft.

机译：None

著录项

来源
《Russian Aeronautics》 |2020年第3期|共11页
作者
A. S. Kretov; P. A. Shataev;
展开▼
作者单位

Nanjing University of Aeronautics and Astronautics;

Tupolev Kazan National Research Technical University;

展开▼
收录信息
原文格式 PDF
正文语种 eng
中图分类航空;
关键词
fuselage; design; calculation; weight formula; load-carrying factor; weight assessment;

机译：机身;设计;计算;重量配方;承载因子;体重评估;

相似文献

外文文献
中文文献
专利

1. Light weight HTPB-clay nanocomposites(HCN)with enhanced ablation performance as inhibition materials for composite propellant [J] . Kavita Ghosh, L.V. Gaikwad, R.K. Kalal, 兵工学报（英文版） . 2021,第002期
2. Integrity of composite aircraft fuselage materials under crash fire conditions [J] . G. La Delfa, J. W. Luinge, A. G. Gibson Plastics, Rubber and Composites . 2009,第2a3a4期

机译：飞机着火时复合材料机身的完整性
3. A parametric aircraft fuselage model for preliminary sizing and crashworthiness applications [J] . D. B. Schwinn, D. Kohlgrueber, J. Scherer, CEAS Aeronautical Journal . 2016,第3期

机译：用于初步定型和防撞性应用的参数化飞机机身模型
4. Vertical Drop Test of Composite Fuselage Section of a Regional Aircraft [J] . Di Palma L., Di Caprio F., Chiariello A., AIAA Journal . 2020,第1期

机译：支线飞机组合机身截面的垂直跌落试验
5. A preliminary prediction method for the efect of new fuselage materials on transport aircraft weight [C] . R. Slingerland, F. van AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference . 2007

机译：新型机身材料对运输机重量影响的初步预测方法
6. Finite Element Analysis of Composite Aircraft Fuselage Frame. [D] . Dandekar, Aditya Milind. 2017

机译：复合材料飞机机身框架的有限元分析。
7. Application of Dual Focused Ultrasonic Phased Array Transducer in Two Orthogonal Cross-Sections for Inspection of Multi-Layered Composite Components of the Aircraft Fuselage [O] . Renaldas Raišutis, Olgirdas Tumšys 2020

机译：双聚焦超声相控阵传感器在两个正交截面中用于飞机机身多层复合部件检查的应用
8. Influence of Fuselage Bulkhead Stiffness on Composite Wing Weight of a Civil Aircraft [O] . Lohith N, Kumari Asha, Varughese Byji 2012

机译：机身舱壁刚度对民用飞机复合机翼重量的影响
9. Weight Assessment for Fuselage Shieldingon Aircraft With Open-Rotor Engines and Composite Blade Loss. [R] . Carney, K., Pereira, M., Kohlman, L., 2013

机译：具有开式转子发动机和复合叶片损失的机身屏蔽飞机重量评估。

Preliminary Assessment of the Weight of the Aircraft Fuselage as a Result of the Transition to Composite Materials

摘要

著录项

相似文献

相关主题

期刊订阅