【摘要】 可持续月球结构的基础在于设计能够承受月球极端环境条件的创新结构。本文提出了一种混合式月球结构设计方案，该结构由可折叠铝杆（内骨架）、凯夫拉（Kevlar）层及用于辐射屏蔽的月壤层组成，作为月球任务初期的停放设施。本文通过开展热力学与固体力学仿真分析，评估了结构的稳定性。热分析部分揭示了不同太阳高度角下，月球表面温度的分布规律及其在月昼周期内的变化，验证了结构的热稳定性。固体力学分析优化了凯夫拉层的厚度，并评估了内骨架在不同边界载荷作用下的力学响应，以保证结构的机械灵活性。设计与仿真结果表明，该结构可为居住舱、月球车等任务资产提供存储空间，有效防护辐射、极端温度及微流星体撞击，为月面作业提供稳定平台。本研究提出了一种易于实现、资源高效的初期月球结构设计方案，为未来月球定居奠定了基础。更多还原

【Abstract】 With the resurgence of lunar exploration, establishing sustainable early-stage infrastructure capable of withstanding extreme lunar conditions has become a critical prerequisite for long-term lunar settlements. This study proposes an innovative foldable pyramid-shaped hybrid lunar structure, designed as a primary parking and protection facility for mission assets(e.g., rovers, habitation modules) during the initial phase of lunar missions. The structural configuration draws inspiration from pyramid-shaped camping tents, featuring exceptional stability and space efficiency. The core design integrates three functional layers: a foldable internal frame made of aluminum alloy T6-7075, a flexible Kevlar-49 envelope, and an in-situ lunar regolith shielding layer, leveraging In Situ Resource Utilization(ISRU) to minimize launch mass and enhance cost-effectiveness. The modular internal frame consists of four central main rods connected by long hinge straps, paired with diagonal secondary support rods to ensure uniform load distribution. The Kevlar-49 envelope serves as an airtight barrier, with a sophisticated folding mechanism that enables a high volume compression ratio of 1:4, facilitating compact storage during launch and synchronized deployment with the frame on the lunar surface. The deployment process involves two controlled phases: retraction of external rods for transport and sequential extension guided by hinges to form the complete pyramid geometry, ensuring wrinkle-free coverage of the internal frame by the Kevlar membrane. Compared with existing rigid and inflatable lunar structures, this hybrid design integrates the advantages of portability(high compression ratio) and robustness(superior radiation, thermal, and micrometeorite protection). Key innovations include the pyramid configuration with efficient space utilization, a thermomechanical analysis model for performance prediction, and the synergistic materials application. The structure effectively shields against extreme temperatures, intense radiation, and micrometeorite impacts, providing a stable platform for early lunar operations.To validate structural performance, comprehensive thermal and solid mechanics simulations were conducted, employing the Finite Element Method(FEM). Thermal analysis focused on temperature distribution and variations across a lunar day under different solar elevation angles. Results indicated that while the outer surface of the structure experienced extreme temperature fluctuations from 113 K(night) to 397 K(daytime), the internal thermal environment remained stable, demonstrating the regolith’s superior thermal insulation capability attributed to its ultra-low thermal conductivity. The surface temperature distribution and variations across a lunar day at different solar elevation angles are explained to demonstrate the thermal behavior of the structure. Mechanical simulations optimized the Kevlar layer thickness and evaluated the load-bearing capacity of the aluminum frame. The internal frame exhibited exceptional load-bearing capacity under different boundary loads.Future research will focus on material durability under combined lunar environmental stresses(radiation, thermal cycling, lunar dust abrasion), geometric optimization of asymmetric pyramid configurations for different lunar latitudes, development of intelligent monitoring and in-situ repair systems, and ground validation tests using lunar environment simulators. This study offers a resource-efficient, deployable solution for early lunar infrastructure, laying a solid foundation for future lunar exploration and settlement.更多还原