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[1]谷小军,徐珉轲,张薇,等.重型运载火箭发动机机架与舱段传力结构一体化拓扑优化设计[J].火箭推进,2022,48(02):27-35.
 GU Xiaojun,XU Minke,ZHANG Wei,et al.Integrated topology optimization design of heavy rocket engine frame and segment force transmission structure[J].Journal of Rocket Propulsion,2022,48(02):27-35.
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重型运载火箭发动机机架与舱段传力结构一体化拓扑优化设计

参考文献/References:

[1] 何巍, 刘伟, 龙乐豪. 重型运载火箭及其应用探讨[J]. 导弹与航天运载技术, 2011(1):1-5.
[2] 张智, 容易, 秦曈, 等. 重型运载火箭总体技术研究[J]. 载人航天, 2017, 23(1):1-7.
[3] 李平. 中国载人航天推进技术发展设想[J]. 火箭推进, 2011, 37(2):1-7.
LI P. Development of propulsion technology for Chinese manned launch vehicles[J]. Journal of Rocket Propulsion, 2011, 37(2):1-7.
[4] 王国辉, 曾杜娟, 刘观日, 等. 中国下一代运载火箭结构技术发展方向与关键技术分析[J]. 宇航总体技术, 2021, 5(5):1-11.
[5] 顾名坤, 何巍, 唐科, 等. 中国液体运载火箭结构系统发展规划研究[J]. 宇航总体技术, 2021, 5(2):55-67.
[6] ZHU J H, ZHANG W H, XIA L. Topology optimization in aircraft and aerospace structures design[J]. Archives of Computational Methods in Engineering, 2016, 23(4):595-622.
[7] CAO Y F, GU X J, ZHU J H, et al. Precise output loads control of load-diffusion components with topology optimization[J]. Chinese Journal of Aeronautics, 2020, 33(3): 933-946.
[8] ORME M, MADERA I, GSCHWEITL M, et al. Topology optimization for additive manufacturing as an enabler for light weight flight hardware[J]. Designs, 2018, 2(4):51.
[9] 石波, 盛刚, 黄雪刚, 等. 吸气式发动机可调喷管调节片结构优化设计[J]. 火箭推进, 2021, 47(3):52-59.
SHI B, SHENG G, HUANG X G, et al. Structural optimization design for variable nozzle flap of airbreathing engines[J]. Journal of Rocket Propulsion, 2021, 47(3):52-59.
[10] 严博燕, 吕江彦, 刘元敏. 固体火箭发动机喷管扩张段壳体结构优化设计[J]. 火箭推进, 2019, 45(3):54-58.
YAN B Y, LYU J Y, LIU Y M. Optimal design on solid rocket motor nozzle divergent cone[J]. Journal of Rocket Propulsion, 2019, 45(3):54-58.
[11] BALDZHIEV R S, ALEKSEYEV A A, AZAROV A V. Topology optimization of the lattice payload adapter for carrier rocket[J]. IOP Conference Series:Materials Science and Engineering, 2019, 683(1):012061.
[12] WANG J, ZHU J H, HOU J, et al. Lightweight design of a bolt-flange sealing structure based on topology optimization[J]. Structural and Multidisciplinary Optimization, 2020, 62(6):3413-3428.
[13] 范瑞祥, 姚瑞娟, 朱振涛, 等. 一种新型7台火箭发动机并联推力传递结构方案[J]. 载人航天, 2020, 26(5):630-634.
[14] ZHU J H, ZHAO Y B, ZHANG W H, et al. Bio-inspired feature-driven topology optimization for rudder structure design[J], Engineered Science. 2019, 5: 46–55.
[15] ZHOU Y, ZHANG W H, ZHU J H, et al. Feature-driven topology optimization method with signed distance function[J]. Computer Methods in Applied Mechanics and Engineering, 2016, 310: 1-32.
[16] ZHOU Y, ZHANG W H, ZHU J H. Concurrent shape and topology optimization involving design-dependent pressure loads using implicit B-spline curves[J]. International Journal for Numerical Methods in Engineering, 2019, 118(9): 495-518.
[17] ZHOU Y, ZHU J H, ZHAN H F, et al. A bio-inspired B-spline offset feature for structural topology optimization[J]. Computer Methods in Applied Mechanics and Engineering, 2021, 386: 114081.
[18] 胡海峰. 液体火箭发动机推力室一体化设计分析关键技术分析[D]. 西安:西北工业大学, 2012.
[19] AINSWORTH M. Essential boundary conditions and multi-point constraints in finite element analysis[J]. Computer Methods in Applied Mechanics and Engineering, 2001, 190(48):6323-6339.
[20] YOON K H, HEO S P, SONG K N, et al. Dynamic impact analysis of the grid structure using multi-point constraint(MPC)equation under the lateral impact load[J]. Computers & Structures, 2004, 82(23/24/25/26):2221-2228.

备注/Memo

收稿日期:2022-01-20 修回日期:2022-03-06
基金项目:国家自然科学基金(51790171, 51761145111, 51735005, 11722219)
作者简介:谷小军(1986—),男,博士,副教授,研究领域为智能材料与结构设计。
通信作者:朱继宏(1981—),男,博士,教授,研究领域为航空航天高性能结构设计。

更新日期/Last Update: 1900-01-01