journal article·2023-07-26Open access

Progress in Lightweight Design Methods for Large-Size Panel Structures in Manned Pressurized Capsules

Zhiyong Zhou, Chenfan Yu, Xiuzhu Han, Kaiwei Zheng, Chao Jiang, Kuo Tian

Applied Sciences· Volume 13· Issue 15

Abstract

The pressurized capsule structure provides the pressure environment for astronauts or payloads in space, which is thus considered as the most crucial structural component for manned spacecraft. The manned deep space exploration mission (MDSEM) brings new challenges to the pressurized capsule structure: extremely low structural weight, long service life, reusability and adaptability to the harsh deep space environment. The conventional welded panel pressurized capsule structure (WPPCS) is not able to meet these new requirements. To address the above challenges, this paper comprehensively expounds why the current WPPCS cannot meet the requirements of MDSEMs based on the analysis of the vibration environment and structural characteristics of the pressurized capsule structure. Furthermore, a new type of integrated panel pressurized capsule structure (IPPCS) is proposed, showing the lightweight advantage compared with WPPCS. Finally, the technical details and research results of the strength criterion, design method, material upgrading and structural integrity manufacturing process of the IPPCS are fully introduced. The conclusions drawn in this paper will provide useful and meaningful references for the future development of large-size, lightweight pressurized capsule structures.
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Research context

OpenAlex topics: Structural Analysis and Optimization · Mechanical Engineering and Vibrations Research · Spacecraft and Cryogenic Technologies

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

School of Mechanical, Electronic and Control Engineering, Beijing Jiaotong University, Beijing 100044, China

Beijing Institute of Spacecraft System Engineering, Beijing 100094, China

China National International Science and Technology Cooperation Base, Beijing Jiaotong University, Beijing 100044, China

State Key Laboratory of Structural Analysis, Optimization and CAE Software for Industrial Equipment, Dalian University of Technology, Dalian 116024, China

Funding

National Key Research and Development Program project of China

References (47)

Show source-provided references
1. Design of low mass dimensionally stable composite base structure for a spacecraft10.1016/j.compositesb.2010.11.003 ↗
2. Integrated design optimization of stiffened plate structures10.1108/02644409910304185 ↗
3. Technology progress of integral panel structure for large space station
4. Manufacturing Technology for large cabin structures of china manned spacecraft
5. Welding the structure of the Buran orbital aircraft10.1080/09507119709454434 ↗
6. Analysis and optimization of lunar exploration architecture based on reusable human spacecraft10.2514/1.A34265 ↗
7. Overview of reusable space systems with a look to technology aspects10.1016/j.actaastro.2021.07.039 ↗
8. Cheng, Z.L. (2017). Research on Modeling and Optimization of Manned Exploration of the Moon System Using Reusable Trans-Lunar Injection Spacecraft, National University of Defense Technology.
9. Study on damage tolerance behavior of integrally stiffened panel and conventional stiffened panel
10. Brief introduction and recent development on the manufacture of aluminum alloy integral panels in aerospace applications10.1504/IJMSI.2021.125814 ↗
11. Swiech, L. (2019). Experimental and numerical studies of low-profile, triangular grid-stiffened plates subjected to shear load in the post-critical states of deformation. Materials, 12.10.3390/ma12223699 ↗
12. Benfratello, S., Giambanco, F., and Palizzolo, L. (2009, January 14–17). Optimal design of structures under dynamic loading. Proceedings of the XIX Congresso Nazionale AIMETA, Ancona, Italy.
13. Structural design of frames able to prevent element buckling
14. Bernard, L., and Joel, W. (1996, January 24–26). Critical fracture of international space station modules following orbital debris penetration. Proceedings of the Space Programs and Technologies Conference, Huntsville, AL, USA.
15. Monitoring the orbital decay of the Chinese space station Tiangong-1 from the loss of control until the re-entry into the Earth’s atmosphere10.1016/j.jsse.2019.10.004 ↗
16. The challenges of designing a lightweight spacecraft structure for landing on the lunar surface10.1016/j.actaastro.2011.08.003 ↗
17. On the elasto-plastic buckling of Integrally Stiffened Panels (ISP) joined by Friction Stir Welding (FSW): Numerical simulation and optimization algorithms10.1016/j.ijmecsci.2013.09.002 ↗
18. A data-driven modelling and optimization framework for variable-thickness integrally stiffened shells10.1016/j.ast.2022.107839 ↗
19. Optimum design of shell structures with stiffening beams10.2514/1.9041 ↗
20. Design of an innovative laser-assisted four-point bending forming process for high-stiffened structure of aluminum alloy10.1016/j.optlastec.2021.107313 ↗
21. Structural optimization strategies for simple and integrally stiffened plates and shells10.1108/02644400510598769 ↗
22. Design, optimization, and evaluation of integrally stiffened Al-7050 panel with curved stiffeners10.2514/1.C031118 ↗
23. Direct evaluation of the limit states of engineering structures exhibiting limited, nonlinear kinematical hardening—ScienceDirect10.1016/j.ijplas.2012.10.008 ↗
24. Shakedown analysis for structural design applied to a manned airtight module10.1016/j.ijpvp.2018.02.006 ↗
25. Shakedown analysis of bounded kinematic hardening engineering structures under complex cyclic loads: Theoretical aspects and a direct approach10.1016/j.engstruct.2022.114034 ↗
26. A residual stress decomposition based method for the shakedown analysis of structures10.1016/j.cma.2014.03.019 ↗
27. A simplified technique for shakedown limit load determination10.1016/j.nucengdes.2006.09.033 ↗
28. A numerical approach for predicting shakedown limit in ratcheting behavior of materials10.1016/j.matdes.2012.12.049 ↗
29. On shakedown theory for elastic–plastic materials and extensions10.1016/j.jmps.2007.11.005 ↗
30. Integrity assessment of defective pressurized pipelines by direct simplified methods10.1016/S0308-0161(97)00084-7 ↗
31. Shakedown analysis of defective pressure vessels by a kinematic approach10.1007/s004190050254 ↗
32. A comparative study of shape imperfection and internal pressure effects on plastic, shakedown and elastic limit loads using large and small strain formulation of 90° pipe bends10.1016/j.ijpvp.2021.104347 ↗
33. Application of lower bound direct method to engineering structures10.1007/s10898-006-9069-1 ↗
34. Shakedown solutions for ballasted track structure under multiple uniform loads
35. Shakedown analysis and its application in pavement and railway engineering10.1016/j.compgeo.2021.104281 ↗
36. Shakedown analysis of a reusable space capsule10.1016/j.ijmecsci.2022.108028 ↗
37. Design optimization of stiffened storage tank for spacecraft10.1007/s00158-007-0174-7 ↗
38. Data-driven modelling and optimization of stiffeners on undevelopable curved surfaces10.1007/s00158-020-02675-4 ↗
39. Unified approach to NURBS curve shape modification10.1016/0010-4485(95)92148-L ↗
40. Efficient multi-objective CMA-ES algorithm assisted by knowledge-extraction-based variable-fidelity surrogate model10.1016/j.cja.2022.09.020 ↗
41. Research on a algorithm of adaptive interpolation for NURBS curve10.4028/www.scientific.net/AMM.687-691.1600 ↗
42. Efficient buckling analysis and optimization method for rotationally periodic stiffened shells accelerated by Bloch wave method10.1016/j.engstruct.2022.115395 ↗
43. Gaussian process surrogate models for the CMA evolution strategy10.1162/evco_a_00244 ↗
44. Data-driven non-intrusive shape-topology optimization framework for curved shells10.1016/j.ast.2023.108405 ↗
45. Selection of main structural materials for spacecraft sealing cabins in China and abroad
46. Wesley, T., Marcia, D., John, W., Taminger, K., Hoffman, E., and Newman, S. (2021). Light Metals 2021, Springer International Publishing.
47. Study on Integrated Manufacturing Technology of Non-welded Spacecraft Structure