CN114104336B - An inflatable deployable sealed cabin with lunar soil-filled bulkheads - Google Patents
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- B—PERFORMING OPERATIONS; TRANSPORTING
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Abstract
Description
技术领域Technical field
本发明属于航天器结构技术领域,具体涉及一种具有月壤填充舱壁的充气展开式密封舱。The invention belongs to the technical field of spacecraft structures, and specifically relates to an inflatable deployable sealed cabin with a lunar soil-filled bulkhead.
背景技术Background technique
月球基地建设已成为月球探测的一个重要目标。月球居住舱作为航天员在月球生活和工作的主要密封场所,是月球基地建设的重要基础设施之一。目前的密封舱主要有刚性金属密封舱和充气展开密封舱(充气舱)两种结构形式,但都存在一些不足之处。The construction of lunar base has become an important goal of lunar exploration. As the main sealed place for astronauts to live and work on the moon, the lunar habitat module is one of the important infrastructures for the construction of the lunar base. The current sealed cabins mainly have two structural forms: rigid metal sealed cabins and inflatable deployable sealed cabins (inflatable cabins), but both have some shortcomings.
刚性金属密封舱是目前普遍采用的密封舱结构形式,但尚存在质量重、发射体积大、发射成本高、在轨组装难度大、居住空间狭小等缺陷,难以满足未来月球基地多人长期居留对大尺寸密封舱的需求。Rigid metal sealed cabins are currently commonly used sealed cabin structures, but they still have shortcomings such as heavy mass, large launch volume, high launch costs, difficult on-orbit assembly, and small living space, making it difficult to meet the long-term requirements of multiple people on the lunar base in the future. The need for large-sized sealed cabins.
与传统刚性金属密封舱相比,充气展开密封舱是一种新型的密封舱,具有可柔性折叠、发射体积小、质量轻、易于发射、发射成本低、可在轨充气展开成型、展开体积大等特点,易于构建大尺寸空间密封舱。但对于全柔性密封舱而言,局部漏气后易造成整体结构的坍塌,甚至威胁到内部工作人员及仪器设备的安全。此外,月面空间辐射强度高,需要具有足够厚度和足够质量的舱壁,才能实现对舱内人员和仪器设备的辐射防护,而单纯依靠由地球向月面运输材料或舱体实现对空间辐射的防护,不仅成本高昂,甚至难以实现。Compared with the traditional rigid metal sealed capsule, the inflatable deployable sealed capsule is a new type of sealed capsule that is flexible and foldable, has a small launch volume, is light in weight, is easy to launch, has low launch cost, can be inflated and deployed in orbit, and has a large deployment volume. and other features, making it easy to build a large-sized space sealed cabin. However, for fully flexible sealed cabins, local air leakage can easily cause the collapse of the entire structure, and even threaten the safety of internal staff, instruments and equipment. In addition, the radiation intensity of the lunar surface is high, and a bulkhead with sufficient thickness and quality is required to achieve radiation protection for personnel and instruments in the cabin. However, space radiation protection can only be achieved by simply transporting materials or cabins from the earth to the lunar surface. Protection is not only expensive, but even difficult to achieve.
发明内容Contents of the invention
本发明针对月球基地对大尺寸居住密封舱的需求,提出一种具有月壤填充舱壁的充气展开式密封舱。In view of the demand for large-sized residential sealed cabins in lunar bases, the present invention proposes an inflatable deployable sealed cabin with lunar soil-filled bulkheads.
本发明所采取的技术方案是:一种具有月壤填充舱壁的充气展开式密封舱,包括月壤填充舱壁、柔性蒙皮、可刚化充气展开式拱形支撑结构及半刚性地板;所述月壤填充舱壁设置在密封舱最外侧,其里侧为由柔性蒙皮两端与半刚性地板两端连接形成的舱室结构,所述半刚性地板由多个纵向铺设的刚性板之间通过柔性连接条带连接而成,可在柔性连接条带处进行折叠,所述可刚化充气展开式拱形支撑结构设置在舱室结构内,能够折叠以及在月面协同密封舱充气展开成型并刚化。The technical solution adopted by the present invention is: an inflatable deployable sealed cabin with a lunar soil-filled bulkhead, including a lunar soil-filled bulkhead, a flexible skin, a rigidizable inflatable deployable arch support structure and a semi-rigid floor; The lunar soil-filled bulkhead is arranged on the outermost side of the sealed cabin, and its inner side is a cabin structure formed by connecting the two ends of the flexible skin and the two ends of the semi-rigid floor. The semi-rigid floor is composed of a plurality of longitudinally laid rigid plates. are connected by flexible connecting strips and can be folded at the flexible connecting strips. The rigidizable inflatable deployable arch support structure is provided in the cabin structure and can be folded and inflated and deployed on the lunar surface in conjunction with the sealed cabin. And harden.
本发明与现有技术相比具有以下有益效果:Compared with the prior art, the present invention has the following beneficial effects:
1.本发明的密封舱柔性可折叠、折叠体积小、质量轻,可在月面展开成大尺寸居住舱结构,解决了由于发射载荷及发射包络的限制,难以发射居住空间大的刚性金属载人密封舱的问题。1. The sealed cabin of the present invention is flexible and foldable, has a small folding volume and is light in weight. It can be deployed on the lunar surface into a large-sized residential cabin structure, which solves the problem of difficulty in launching rigid metal with a large living space due to the limitations of launch load and launch envelope. The problem of manned sealed cabins.
2.本发明的密封舱采用月壤填充舱壁,具有良好的隔热和空间辐射防护效果。月壤就地取材,显著降低了密封舱的发射成本及发射难度。2. The sealed cabin of the present invention uses lunar soil to fill the cabin wall, which has good heat insulation and space radiation protection effects. The lunar soil is sourced from local materials, which significantly reduces the launch cost and launch difficulty of the sealed capsule.
3.本发明的密封舱的月壤填充舱壁,由月壤填充形成拱形结构,具有很高的结构刚度,能显著减轻所填充月壤对充气展开舱的压力,显著提高了密封舱的结构可靠性和稳定性。3. The lunar soil-filled bulkhead of the sealed cabin of the present invention is filled with lunar soil to form an arched structure, which has high structural rigidity, can significantly reduce the pressure of the filled lunar soil on the inflatable deployment cabin, and significantly improves the performance of the sealed cabin. Structural reliability and stability.
4.本发明的密封舱内部采用可刚化的充气展开式拱形支撑结构,刚化后结构刚度高、稳定性好,对密封舱起到支撑作用,并进一步提高密封舱的刚度,并可避免因为局部漏气造成的整体结构的坍塌。4. The interior of the sealed cabin of the present invention adopts a rigidizable inflatable expandable arch support structure. After stiffening, the structure has high stiffness and good stability, which plays a supporting role in the sealed cabin, further improves the stiffness of the sealed cabin, and can Avoid the collapse of the overall structure due to local air leakage.
附图说明Description of the drawings
图1是本发明结构示意图;Figure 1 is a schematic structural diagram of the present invention;
图2是本发明月壤填充舱壁结构示意图;Figure 2 is a schematic structural diagram of the lunar soil filling bulkhead of the present invention;
图3是本发明月壤填充模块结构示意图;Figure 3 is a schematic structural diagram of the lunar soil filling module of the present invention;
图4是本发明可刚化充气展开式拱形支撑结构结构示意图;Figure 4 is a schematic structural diagram of the rigidizable inflatable expandable arch support structure of the present invention;
图5是本发明密封舱展开示意图;Figure 5 is an unfolded schematic diagram of the sealed cabin of the present invention;
图6是本发明密封舱折叠示意图;Figure 6 is a schematic diagram of the folding of the sealed cabin of the present invention;
图7是本发明密封舱折叠方式图;Figure 7 is a diagram of the folding mode of the sealed cabin of the present invention;
图8是本发明刚性底板示意图;Figure 8 is a schematic diagram of the rigid base plate of the present invention;
图9是本发明月壤填充舱壁和柔性蒙皮示意图;Figure 9 is a schematic diagram of the lunar soil-filled bulkhead and flexible skin of the present invention;
其中:1、月壤填充舱壁;2、柔性蒙皮;3、柔性舱门;4、柔性密封拉链;5、可刚化充气展开式拱形支撑结构;6、半刚性地板;7、连接段一;8、连接段二;9、自由段;11、月壤填充模块;12、柔性连接布;21、气密层二;22、承力层二;61、刚性板;62、柔性连接条带;111、可刚化柔性月壤袋;112、底层刚板;113、气密层一;114、电热层一;115、刚化层一。Among them: 1. Lunar soil-filled bulkhead; 2. Flexible skin; 3. Flexible hatch; 4. Flexible sealing zipper; 5. Rigidizable inflatable expandable arch support structure; 6. Semi-rigid floor; 7. Connection Section one; 8. Connection section two; 9. Free section; 11. Lunar soil filling module; 12. Flexible connection cloth; 21. Airtight layer two; 22. Bearing layer two; 61. Rigid plate; 62. Flexible connection Strip; 111. Rigidizable flexible lunar soil bag; 112. Bottom rigid plate; 113. Airtight layer one; 114. Electric heating layer one; 115. Rigidizing layer one.
具体实施方式Detailed ways
具体实施方式一:参照图1至图9说明本实施方式,本实施方式提供了一种具有月壤填充舱壁的充气展开式密封舱,包括月壤填充舱壁1、柔性蒙皮2、可刚化充气展开式拱形支撑结构5及半刚性地板6;所述月壤填充舱壁1设置在密封舱最外侧,其里侧为由柔性蒙皮2两端与半刚性地板6两端连接形成的舱室结构,所述半刚性地板6由多个纵向铺设的刚性板61之间通过柔性连接条带62连接而成,可在柔性连接条带62处进行折叠,并随密封舱展开成型,使舱内底面平整,便于航天员生活、工作及设备的安放,具备很强的防刺扎作用,所述可刚化充气展开式拱形支撑结构5设置在舱室结构内,能够折叠以及在月面协同密封舱充气展开成型并刚化;Specific Embodiment 1: This embodiment will be described with reference to Figures 1 to 9. This embodiment provides an inflatable deployable sealed cabin with a lunar soil-filled bulkhead, including a lunar soil-filled bulkhead 1, a flexible skin 2, and a Rigidized inflatable expandable arch support structure 5 and semi-rigid floor 6; the lunar soil-filled bulkhead 1 is arranged on the outermost side of the sealed cabin, and its inner side is connected by two ends of the flexible skin 2 and two ends of the semi-rigid floor 6 The cabin structure formed, the semi-rigid floor 6 is composed of multiple longitudinally laid rigid plates 61 connected by flexible connecting strips 62, which can be folded at the flexible connecting strips 62 and unfolded and formed along with the sealed cabin. The bottom surface of the cabin is flat, which is convenient for astronauts' life, work and equipment placement, and has a strong anti-puncture effect. The rigidizable inflatable expandable arch support structure 5 is set in the cabin structure and can be folded and used on the moon. The surface cooperates with the sealed cabin to inflate, expand, form and stiffen;
密封舱外设置柔性舱门3,由柔性密封拉链4打开和关闭。A flexible hatch 3 is provided outside the sealed cabin, which is opened and closed by a flexible sealed zipper 4.
本实施方式中,密封舱初始为折叠状态,经折叠包装后发射至月球,可在月面充气展开成大型密封舱结构。In this embodiment, the sealed capsule is initially in a folded state. After being folded and packaged, it is launched to the moon and can be inflated and deployed on the lunar surface to form a large sealed capsule structure.
具体实施方式二:参照图1至图2说明本实施方式,本实施方式是对具体实施方式一作进一步限定,本实施方式中,所述月壤填充舱壁1包括由多个月壤填充模块11依次连接而成的拱形结构以及连接在拱形结构外侧的柔性连接布12,柔性连接布12使月壤填充模块11之间连接为一个整体,起到固定舱壁整体形状的作用,并进一步提高密封舱整体结构稳定性,月壤填充舱壁1设置在柔性蒙皮2的外侧,与柔性蒙皮2连接为一体。其它组成及连接方式与具体实施方式一相同。Specific Embodiment 2: This embodiment will be described with reference to Figures 1 to 2. This embodiment further limits Specific Embodiment 1. In this embodiment, the lunar soil filling bulkhead 1 includes a plurality of lunar soil filling modules 11. The arched structure is connected in sequence and the flexible connecting cloth 12 is connected to the outside of the arched structure. The flexible connecting cloth 12 connects the lunar soil filling modules 11 into a whole, which plays a role in fixing the overall shape of the bulkhead, and further To improve the overall structural stability of the sealed cabin, the lunar soil-filled bulkhead 1 is arranged on the outside of the flexible skin 2 and is connected to the flexible skin 2 as a whole. Other components and connection methods are the same as in the first embodiment.
本实施方式中,柔性连接布12由高强纤维布和防辐射涂层组成,具有很高的承力性能和防辐射性能。In this embodiment, the flexible connecting cloth 12 is composed of high-strength fiber cloth and radiation-proof coating, and has high load-bearing performance and radiation-proof performance.
具体实施方式三:参照图5至图7说明本实施方式,本实施方式是对具体实施方式二作进一步限定,本实施方式中,所述月壤填充舱壁1与柔性蒙皮2分段连接,从柔性蒙皮2一端开始至与半刚性地板6横向长度一样的区域为连接段一7,柔性蒙皮2剩余部分等分为二,分别为连接段二8和自由段9,连接段二8为与连接段一7相连的区域,折叠时,半刚性地板6向上与连接段一7重合,柔性蒙皮2的自由段9与连接段二8重合。其它组成及连接方式与具体实施方式二相同。Specific Embodiment 3: This embodiment will be described with reference to Figures 5 to 7. This embodiment further limits Specific Embodiment 2. In this embodiment, the lunar soil-filled bulkhead 1 is connected to the flexible skin 2 in sections. , starting from one end of the flexible skin 2 to the area with the same transverse length as the semi-rigid floor 6 is the connecting section 7. The remaining part of the flexible skin 2 is divided into two equal parts, namely the connecting section 2 8 and the free section 9. The connecting section 2 8 is the area connected to the connecting section 7. When folded, the semi-rigid floor 6 overlaps the connecting section 1 upward, and the free section 9 of the flexible skin 2 overlaps the connecting section 2 8. Other compositions and connection methods are the same as the second embodiment.
本实施方式中,舱体折叠时,先将半刚性地板6和拱形结构,以及部分与舱壁未连接的柔性蒙皮2一起重叠于拱形舱壁(月壤填充舱壁1)上,然后再一同进行卷绕折叠。In this embodiment, when the cabin is folded, the semi-rigid floor 6 and the arched structure, as well as part of the flexible skin 2 that is not connected to the bulkhead, are first overlapped on the arched bulkhead (lunar soil-filled bulkhead 1). Then roll and fold together.
具体实施方式四,参照图3说明本实施方式,本实施方式是对具体实施方式三作进一步限定,本实施方式中,所述月壤填充模块11包括可刚化柔性月壤袋111及与可刚化柔性月壤袋111外底面贴合连接的底层刚板112;所述可刚化柔性月壤袋111内填充有月壤,所述柔性蒙皮2与对应的底层刚板112连接,连接方式均为粘接、热合或者缝合连接。Specific Embodiment 4: This embodiment will be described with reference to Figure 3. This embodiment is a further limitation of Specific Embodiment 3. In this embodiment, the lunar soil filling module 11 includes a rigidizable flexible lunar soil bag 111 and a flexible lunar soil bag 111. The outer bottom surface of the rigidized flexible lunar soil bag 111 is attached to the connected underlying rigid plate 112; the rigidizable flexible lunar soil bag 111 is filled with lunar soil, and the flexible skin 2 is connected to the corresponding underlying rigid plate 112. The methods are all bonding, heat sealing or suture connection.
本实施方式中,月壤填充舱壁1月面展开成型时,首先随密封舱一起展开,然后向可刚化柔性月壤袋111内充入少量气体使之成型,然后对可刚化柔性月壤袋111进行电加热刚化并固定形状,最后向可刚化柔性月壤袋111内装填月壤形成舱壁结构。In this embodiment, when the lunar surface of the lunar soil-filled bulkhead 1 is unfolded and formed, it is first unfolded together with the sealed cabin, and then a small amount of gas is filled into the rigidizable flexible lunar soil bag 111 to form it, and then the rigidizable flexible lunar surface is molded. The soil bag 111 is electrically heated to stiffen and fix its shape. Finally, the rigidizable flexible lunar soil bag 111 is filled with lunar soil to form a bulkhead structure.
具体实施方式五:参照图9说明本实施方式,本实施方式是对具体实施方式四作进一步限定,本实施方式中,所述可刚化柔性月壤袋111为长条状楔形袋结构,其横截面为梯形,可刚化柔性月壤袋111由可刚化多层柔性复合材料制成,从内至外依次为气密层一113、电热层一114及刚化层一115;其中,气密层一113由气体阻隔性优良,且高强、耐磨的薄膜材料制成;电热层一114采用电热丝制成,用于对刚化层一115进行加热,使其刚化;刚化层一115采用纤维增强的热固性树脂材料制成,刚化后具有很高的强度和刚度。其它组成及连接方式与具体实施方式四相同。Specific Embodiment 5: This embodiment will be described with reference to Figure 9. This embodiment further limits Specific Embodiment 4. In this embodiment, the rigidizable flexible lunar soil bag 111 is a long wedge-shaped bag structure. The cross-section is trapezoidal, and the rigidizable flexible lunar soil bag 111 is made of rigidizable multi-layer flexible composite materials. From the inside to the outside, there are an airtight layer 113, an electric heating layer 114 and a rigid layer 115; among them, The airtight layer 113 is made of a film material with excellent gas barrier properties and high strength and wear resistance; the electric heating layer 114 is made of electric heating wire and is used to heat the rigid layer 115 to make it rigid; rigidization Layer 115 is made of fiber-reinforced thermosetting resin material, which has high strength and stiffness after stiffening. Other compositions and connection methods are the same as those in the fourth embodiment.
具体实施方式六:参照图9说明本实施方式,本实施方式是对具体实施方式五作进一步限定,本实施方式中,所述柔性蒙皮2是由气密层二21和承力层二22组成的柔性多层复合结构;所述气密层二21设置在承力层二22内侧,采用气体阻隔薄膜制成,具有良好的气体阻隔性能和一定的承力性能,可保障密封舱充气展开成型,并长期维持航天员生活、工作的正常气压;承力层二22采用高强、高模的纤维材料编织而成,可承受内部高压,防止气密层二21过度膨胀,造成密封舱破坏。其它组成及连接方式与具体实施方式五相同。Specific Embodiment 6: This embodiment will be described with reference to Figure 9. This embodiment further limits Specific Embodiment 5. In this embodiment, the flexible skin 2 is composed of an airtight layer 21 and a load-bearing layer 22. It is a flexible multi-layer composite structure; the second airtight layer 21 is arranged inside the second load-bearing layer 22 and is made of gas barrier film. It has good gas barrier performance and certain load-bearing performance, and can ensure the inflatable deployment of the sealed cabin. The airtight layer 22 is formed and maintains the normal air pressure for astronauts' life and work for a long time; the load-bearing layer 22 is woven with high-strength and high-modulus fiber materials, which can withstand the internal high pressure and prevent the airtight layer 21 from over-expanding and causing damage to the sealed cabin. Other components and connection methods are the same as the fifth embodiment.
具体实施方式七:参照图4说明本实施方式,本实施方式是对具体实施方式一作进一步限定,本实施方式中,所述可刚化充气展开式拱形支撑结构5由数根可刚化充气展开式支撑管连通搭建而成的拱形结构,可刚化充气展开式支撑管的管壁采用可刚化的多层柔性复合材料制成,由内至外依次为气密层三、电热层三、刚化层三。其它组成及连接方式与具体实施方式一相同。Specific Embodiment 7: This embodiment is described with reference to Figure 4. This embodiment is a further limitation of Specific Embodiment 1. In this embodiment, the rigidizable and inflatable expandable arch support structure 5 is composed of several rigidizable and inflatable arched support structures. An arched structure formed by connected expandable support tubes. The wall of the rigidizable inflatable expandable support tube is made of multi-layer flexible composite materials that can be rigidified. From the inside to the outside, there are three airtight layers and an electric heating layer. 3. Stiffening layer three. Other components and connection methods are the same as in the first embodiment.
具体实施方式八:本实施方式是对具体实施方式七作进一步限定,本实施方式中,所述气密层三采用气体阻隔性良好的薄膜材料制成,用于可刚化充气展开式支撑管的初始展开成型;所述电热层三采用电热丝制成,用于对可刚化充气展开式支撑管的刚化层三进行加热,使其刚化;所述刚化层三采用纤维增强的热固性树脂材料制成,可在充气展开成型后由电热层三加热刚化,具有很高的刚度。其它组成及连接方式与具体实施方式七相同。Specific Embodiment 8: This embodiment is a further limitation of Specific Embodiment 7. In this embodiment, the airtight layer three is made of a film material with good gas barrier properties and is used for a rigidizable inflatable expandable support tube. The initial expansion molding; the electric heating layer 3 is made of electric heating wire, used to heat the rigid layer 3 of the rigidizable inflatable expandable support tube to make it rigid; the rigid layer 3 is made of fiber reinforced Made of thermosetting resin material, it can be heated and stiffened by the electric heating layer three after inflating and unfolding, and has high stiffness. Other components and connection methods are the same as the seventh embodiment.
本实施方式中,所述可刚化充气展开式拱形支撑结构5内部设置舱内电线电缆、气液管路,有效节约空间并保护管路系统。In this embodiment, the rigidizable inflatable expandable arch support structure 5 is equipped with in-cabin wires, cables, and gas-liquid pipelines, which effectively saves space and protects the pipeline system.
具体实施方式九:本实施方式是对具体实施方式一作进一步限定,本实施方式中,所述可刚化充气展开式拱形支撑结构5底部设有的多根可刚化充气展开式支撑管与半刚性地板6的上表面连接,多根可刚化充气展开式支撑管充气展开并刚化后,可约束并固定半刚性地板6,使之成为刚性的地板结构。Specific Embodiment 9: This embodiment is a further limitation of Specific Embodiment 1. In this embodiment, the bottom of the rigidizable inflatable expandable arch support structure 5 is provided with a plurality of rigidizable inflatable expandable support tubes and The upper surface of the semi-rigid floor 6 is connected, and after a plurality of rigidizable inflatable deployable support tubes are inflated, deployed and stiffened, the semi-rigid floor 6 can be constrained and fixed to make it a rigid floor structure.
密封舱内置有气瓶,用于密封舱的充气展开及内部气压的保持;密封舱内置有充气床垫、置物台及相应的电路、管路系统等附属系统。其它组成及连接方式与具体实施方式一相同。The sealed cabin has a built-in gas bottle, which is used to inflate and expand the sealed cabin and maintain the internal air pressure; the sealed cabin has built-in air mattresses, storage tables and corresponding circuits, piping systems and other ancillary systems. Other components and connection methods are the same as in the first embodiment.
可以理解,本发明是通过一些实施例进行描述的,本领域技术人员知悉的,在不脱离本发明的精神和范围的情况下,可以对这些特征和实施例进行各种改变或等效替换。另外,在本发明的教导下,可以对这些特征和实施例进行修改以适应具体的情况及材料而不会脱离本发明的精神和范围。因此,本发明不受此处所公开的具体实施例的限制,所有落入本申请的权利要求范围内的实施例都属于本发明所保护的范围内。It is understood that the present invention has been described through some embodiments. Those skilled in the art know that various changes or equivalent substitutions can be made to these features and embodiments without departing from the spirit and scope of the present invention. In addition, the features and embodiments may be modified to adapt a particular situation and material to the teachings of the invention without departing from the spirit and scope of the invention. Therefore, the present invention is not limited to the specific embodiments disclosed here, and all embodiments falling within the scope of the claims of the present application are within the scope of protection of the present invention.
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