Investigation on the Crashworthiness of a Composite Fuselage Barrel with Double–Double Designed Frames

被引:0
|
作者
Riccio A. [1 ]
Garofano A. [1 ]
Di Caprio F. [2 ]
机构
[1] Department of Engineering, University of Campania “Luigi Vanvitelli”, Via Roma 29, Caserta, Aversa
[2] C.I.R.A. (Italian Aerospace Research Centre), Via Maiorise, Capua
关键词
composite fuselage; composite laminate optimization; crashworthiness; double–double laminates; finite element method;
D O I
10.1002/masy.202300183
中图分类号
学科分类号
摘要
Double–double (DD) laminates approach enables the design of mass-minimized composite structures with number and orientation of plies tailored on the acting loads. Thus, the investigation of the crashworthiness capabilities is crucial in assessing the airworthiness of DD designed structures. In this work, two composite fuselage barrel configurations with conventional and DD designed frames have been compared to study their crashworthiness performance during an impact event. Numerical results highlight that configurations with DD optimized frames exhibit performance in terms of crashworthiness and passive safety for passengers comparable to the one with conventional designed frames while reducing the structure's total mass by up to 13%. © 2024 Wiley-VCH GmbH.
引用
收藏
相关论文
共 50 条
  • [1] Investigation of the Crashworthiness Performances and the Effect on Passengers of a Double-Double Designed Skin in a Composite Fuselage Barrel
    Garofano, Antonio
    Riccio, Aniello
    DYNAMIC RESPONSE AND FAILURE OF COMPOSITE MATERIALS, DRAF 2024, 2025, : 188 - 197
  • [2] On the effectiveness of double-double design on crashworthiness of fuselage barrel
    Garofano, Antonio
    Sellitto, Andrea
    Acanfora, Valerio
    Di Caprio, Francesco
    Riccio, Aniello
    AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 140
  • [3] On the use of double-double design philosophy in the redesign of composite fuselage barrel frame components
    Garofano, Antonio
    Sellitto, Andrea
    Di Caprio, Francesco
    Riccio, Aniello
    POLYMER COMPOSITES, 2024, 45 (05) : 4250 - 4265
  • [4] A Numerical Assessment on the Influences of Material Toughness on the Crashworthiness of a Composite Fuselage Barrel
    Riccio, A.
    Saputo, S.
    Sellitto, A.
    Di Caprio, E.
    APPLIED SCIENCES-BASEL, 2020, 10 (06):
  • [5] Research on effects of composite skin on crashworthiness of composite fuselage section
    Feng, Zhenyu
    Mou, Haolei
    Zou, Tianchun
    Ren, Jian
    INTERNATIONAL JOURNAL OF CRASHWORTHINESS, 2013, 18 (05) : 459 - 464
  • [6] Experimental and numerical investigation on the crashworthiness of a composite fuselage sub-floor support system
    Riccio, A.
    Raimondo, A.
    Di Caprio, F.
    Fusco, M.
    Sanita, P.
    COMPOSITES PART B-ENGINEERING, 2018, 150 : 93 - 103
  • [7] Optimal selection of composite layup considering the fuselage crashworthiness
    Wang, Dong
    Chen, Lin
    Ji, Shaohua
    Cao, Hua
    Xiong, Meirong
    Wang, Changchun
    Qiu, Ju
    COMPOSITES PART C: OPEN ACCESS, 2025, 16
  • [8] Crashworthiness Simulation Research of Fuselage Section with Composite Skin
    Mou Haolei
    Zou Tianchun
    Feng Zhenyu
    Ren Jian
    3RD INTERNATIONAL SYMPOSIUM ON AIRCRAFT AIRWORTHINESS (ISAA 2013), 2014, 80 : 59 - 65
  • [9] Development of a scale model composite fuselage concept for improved crashworthiness
    Jackson, KE
    Fasanella, EL
    Kellas, S
    JOURNAL OF AIRCRAFT, 2001, 38 (01): : 95 - 103
  • [10] Research on Effects of Oblique Struts on Crashworthiness of Composite Fuselage Sections
    Zou, Tianchun
    Mou, Haolei
    Feng, Zhenyu
    JOURNAL OF AIRCRAFT, 2012, 49 (06): : 2059 - 2063