Application and Research of Composite Parts Manufacturing and Assembly on Aircraft Engine Nacelle Torque Box

被引:0
|
作者
Li, Shengxiong [1 ]
Zhou, Jian [1 ]
Li, Zeyan [2 ]
Li, Deliang [3 ]
机构
[1] Avic Xian Aircraft Ind Grp Co Ltd, Xian 710089, Peoples R China
[2] Hebei Univ Engn, Coll Mat Sci & Engn, Handan 056038, Peoples R China
[3] Shaanxi Yanchang Petr Northwest Rubber Co Ltd, Xianyang 712000, Peoples R China
关键词
Composite material; Composite manufacturing; Aircraft parts; Aircraft manufacturing;
D O I
10.1007/978-981-97-3998-1_4
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The quality of aircraft components is directly related to the quality, safety, performance and flight life of aircraft, The only way is to strictly control the quality of aircraft materials and parts processing, and strictly control the design, production and assembly of aircraft, Can control the quality and performance of the whole aircraft assembly, to ensure safety and prolong the life of the aircraft. The use of composite materials not only improves the strength and safety of aircraft, but also reduces the weight of aircraft and increases the effective load of aircraft, which is a major breakthrough in the aircraft manufacturing industry. "High performance, low cost and multi-function" is the development direction of composite materials in the future, while low-cost manufacturing technology is the development focus of composite materials in the future. Low-cost raw materials, rapid prototyping process technology, large-scale, integrated and integrated products are the core of the development of composite materials in the future. The aircraft engine nacelle torque box project is developed, produced, inspected and delivered in accordance with the numerical models and drawings provided as well as delivery specifications. The torque box of engine nacelle is an important component of aircraft, and the amount of composite material accounts is more than 60%. Advanced composite materials have the advantages of light weight, high specific strength, high specific stiffness, strong designability, good fatigue fracture resistance, corrosion resistance, good dimensional stability and easy to form a large area, at the same time, the use of integral manufacturing technology can greatly reduce the number of parts and fasteners, reduce structural weight, reduce production costs. In view of this, the research and development of aircraft torque box products to reduce the weight of aircraft, increase the payload, simplify the aircraft process equipment, reduce the assembly workload, to shorten the development cycle and reduce the cost of aircraft development is of great significance. Briefly introduces the structure of the torque box of aircraft engine, and systematically analyzes the application process of digital composite parts manufacturing and assembly on the torque box of aircraft. The manufacturing and assembling process of composite parts are studied, and some processing technologies of composite parts are analyzed.
引用
收藏
页码:39 / 51
页数:13
相关论文
共 50 条
  • [21] Application and Analysis of Composite Materials in Actuation System for Commercial Aircraft Engine
    Feng Shaoheng
    2021 13TH INTERNATIONAL CONFERENCE ON MEASURING TECHNOLOGY AND MECHATRONICS AUTOMATION (ICMTMA 2021), 2021, : 5 - 8
  • [22] Research of an aircraft engine cylinder assembly integrity assessment - Thermomechanical FEM analysis
    Vucetic, Nikola
    Jovicic, Gordana
    Krstic, Branimir
    Zivkovic, Miroslav
    Milovanovic, Vladimir
    Kacmarcik, Josip
    Antunovic, Ranko
    ENGINEERING FAILURE ANALYSIS, 2020, 111
  • [23] Research and application of superplastic forming titanium alloys for commercial aircraft parts
    Gershon, B
    Eldror, I
    PRICM 5: THE FIFTH PACIFIC RIM INTERNATIONAL CONFERENCE ON ADVANCED MATERIALS AND PROCESSING, PTS 1-5, 2005, 475-479 : 3047 - 3050
  • [24] Numerical Optimization of Vacuum Assisted Manufacturing of Aircraft Composite Parts Using the Predictive Assessment of Objectives
    Shevtsov, Sergey
    Zhilyaev, Igor
    Huang, Jyun-Ping
    Snezhina, Natalia
    2021 12TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE), 2021, : 125 - 132
  • [25] Research on Application of Engine Assembly Process Design Based on Assembly Simulation Technology
    Liu, Chao
    Liu, Zhen-dong
    Zhao, Hong-feng
    Sun, Qiao
    2018 3RD INTERNATIONAL CONFERENCE ON COMPUTATIONAL MODELING, SIMULATION AND APPLIED MATHEMATICS (CMSAM 2018), 2018, 310 : 19 - 27
  • [26] Review of the application of flexible, measurement-assisted assembly technology in aircraft manufacturing
    Mei, Zhongyi
    Maropoulos, Paul G.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART B-JOURNAL OF ENGINEERING MANUFACTURE, 2014, 228 (10) : 1185 - 1197
  • [27] Advance in the technology of manufacturing gas turbine engine parts by the method of granular metallurgy as the basis for successful development of aircraft engine production (continuation)
    Garibov, G.S.
    Chepkin, V.M.
    Kuznechno-Shtampovochnoe Proizvodstvo (Obrabotka Metallov Davleniem), 2002, (07): : 18 - 22
  • [28] Experimental and numerical evaluation of fracture characteristics of composite material used in the aircraft engine cover manufacturing
    Grbovic, Aleksandar
    Kastratovic, Gordana
    Bozic, Zeljko
    Bozic, Ivan
    Obradovic, Aleksandar
    Sedmak, Aleksandar
    Sedmak, Simon
    ENGINEERING FAILURE ANALYSIS, 2022, 137
  • [29] Research progress of ceramic matrix composite parts based on additive manufacturing technology
    Lu, Zhongliang
    Cao, Jiwei
    Song, Zhaoqiang
    Li, Dichen
    Lu, Bingheng
    VIRTUAL AND PHYSICAL PROTOTYPING, 2019, 14 (04) : 333 - 348
  • [30] Research on key technology of intelligent production line of aircraft structural parts based on intelligent manufacturing
    Liu, Xinyu
    Qiao, Miaomiao
    Meng, Biao
    2019 5TH INTERNATIONAL CONFERENCE ON ENVIRONMENTAL SCIENCE AND MATERIAL APPLICATION, 2020, 440