CN113187314A - Hexagonal inflatable unfolding building module applied to moon building - Google Patents
Hexagonal inflatable unfolding building module applied to moon building Download PDFInfo
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- CN113187314A CN113187314A CN202110520161.3A CN202110520161A CN113187314A CN 113187314 A CN113187314 A CN 113187314A CN 202110520161 A CN202110520161 A CN 202110520161A CN 113187314 A CN113187314 A CN 113187314A
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H15/00—Tents or canopies, in general
- E04H15/20—Tents or canopies, in general inflatable, e.g. shaped, strengthened or supported by fluid pressure
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/34—Extraordinary structures, e.g. with suspended or cantilever parts supported by masts or tower-like structures enclosing elevators or stairs; Features relating to the elastic stability
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H15/00—Tents or canopies, in general
- E04H15/32—Parts, components, construction details, accessories, interior equipment, specially adapted for tents, e.g. guy-line equipment, skirts, thresholds
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H15/00—Tents or canopies, in general
- E04H15/20—Tents or canopies, in general inflatable, e.g. shaped, strengthened or supported by fluid pressure
- E04H2015/206—Details of inflation devices, e.g. valves, connections to fluid pressure source
Abstract
A hexagonal inflatable unfolding building module applied to a moon building belongs to the technical field of moon residential building construction. The invention solves the problem that the existing spherical and cylindrical cabin body structure is not beneficial to realizing modular expansion. The device comprises a folding and unfolding support and an inflatable membrane, wherein three top side plates are uniformly distributed in the circumferential direction of a regular hexagonal top plate, the three top side plates are correspondingly hinged with three side surfaces of the regular hexagonal top plate, three bottom side plates are uniformly distributed in the circumferential direction of a regular hexagonal bottom plate, and three groups of bottom slide rails are staggered with the three bottom side plates and correspondingly hinged with six side surfaces of the regular hexagonal bottom plate; under the building module folded state, top curb plate, bottom curb plate, push-and-pull hatch door, top slide rail and the equal vertical arrangement of bottom slide rail, under the building module expanded state, regular hexagon bottom plate, three bottom curb plate and three groups bottom slide rails all are located same horizontal plane, and three push-and-pull hatch doors slide to the other end of bottom slide rail, aerify the membrane and aerify and expand and the transversal hexagon structure of personally submitting of the membrane of aerifing after expanding.
Description
Technical Field
The invention relates to a hexagonal inflatable unfolding building module applied to a moon building, and belongs to the technical field of moon residential building construction.
Background
The moon exploration project in China is formally implemented according to the three-step planning of winding, falling and returning, the first two steps of targets are satisfactorily completed, and five war five times are realized. The task of Chang E five is implemented at present, and the lunar sampling return is completed. The construction of a lunar scientific research station is taken as an important target in the next-stage lunar exploration project. For human immigration, Mars are recognized as a more potential livable star, and the moon can be used as a transfer station for deep space exploration and space immigration.
How to realize the purpose of sending the space capsule into the space with lower cost, and building a space base on the moon, the mars and other stars is an important problem to be solved in the future. Compared with the conventional metal structure, the inflatable space capsule module is lighter in weight, smaller in occupied space in a rocket, lower in cost and easy to form, and can provide more activity space for astronauts.
Most of inflatable expansion type cabins in the prior art are spherical and cylindrical, and most of inflatable expansion type cabins are ideal for discussing the modeling and the expansion mode of off-site buildings. However, the cabin body has a complex unfolding structure, the connection between the cabin body and the cabin body requires a connecting channel, so that the connection and disconnection between the cabin body and the cabin body are inconvenient, and the cabin body is inconvenient for modular expansion due to the shape limitation of the cabin body.
Disclosure of Invention
The invention aims to solve the technical problems and further provides a hexagonal inflatable and expandable building module applied to a moon building.
The technical scheme adopted by the invention for solving the technical problems is as follows:
a hexagonal inflatable and expandable building module applied to a moon building comprises an inflatable and expandable support and an inflatable membrane, wherein the inflatable and expandable support comprises three push-pull cabin doors, three groups of top sliding rails, three groups of bottom sliding rails, a regular hexagonal top plate and a regular hexagonal bottom plate which are arranged in an up-and-down opposite mode, three top side plates are uniformly distributed in the circumferential direction of the regular hexagonal top plate and correspondingly hinged with three side surfaces of the regular hexagonal top plate, three bottom side plates are uniformly distributed in the circumferential direction of the regular hexagonal bottom plate, and the three groups of bottom sliding rails and the three bottom side plates are arranged in a staggered mode and correspondingly hinged with six side surfaces of the regular hexagonal bottom plate;
the building module is characterized in that a top side plate, a bottom side plate, a push-pull cabin door, a top sliding rail and a bottom sliding rail are vertically arranged in a folded state, the three push-pull cabin doors are correspondingly positioned right below the three top side plates and are correspondingly connected with the top side plate through the top sliding rail, and one end part of each top sliding rail is in sliding connection with the top side plate, the other end part of each top sliding rail is in sliding connection with the top of the push-pull cabin door, and the bottom of each push-pull cabin door is in sliding connection with the bottom sliding rail;
when the building module is unfolded, the regular hexagon bottom plate, the three bottom side plates and the three groups of bottom sliding rails are all positioned on the same horizontal plane, the three push-pull cabin doors slide to the other ends of the bottom sliding rails, the inflatable membrane is inflated and unfolded, and the cross section of the inflated membrane after unfolding is in a hexagon structure;
the lower part of the door frame of the push-pull cabin door is rotatably provided with a step, and the step extends to the outside of the building module and is erected on the surface of the moon ball when the building module is unfolded.
Furthermore, a plurality of first locating rods are installed at the bottom of the regular hexagon bottom plate, at least two second locating rods are installed at the bottom of the door frame of the push-pull cabin door, and the first locating rods and the second locating rods are axial telescopic rods.
Furthermore, each positioning rod is provided with a telescopic limiting claw at one end close to lunar soil in a vertical state.
Furthermore, a plurality of first locating rods are uniformly distributed along the circumferential direction of the regular hexagon bottom plate.
Furthermore, the top and the bottom of the inflatable membrane are respectively and correspondingly connected with the regular hexagon top plate and the regular hexagon bottom plate in a sealing mode, and the side face of the inflatable membrane is connected with the three push-pull cabin doors in a sealing mode.
Furthermore, the bottom slide rail is in an H-shaped structure in an unfolded state.
Furthermore, the push-pull cabin door and the top sliding rail and the push-pull cabin door and the bottom sliding rail are respectively connected through pulleys.
Further, the push-pull cabin door is of a rectangular structure.
Further, the inflatable membrane comprises an optical fiber system prefabricated layer, a flexible inner membrane layer, an inflatable structure reinforcing layer, a flexible heat insulation layer, a flexible protective layer, a lunar soil filling layer, a lunar soil reinforcing layer and a flexible solar energy surface skin layer which are sequentially arranged, wherein the optical fiber system prefabricated layer, the flexible inner film layer, the inflatable structure reinforcing layer, the flexible heat-insulating layer and the flexible protective layer are all prefabricated on the ground, the lunar soil filling layer, the lunar soil reinforcing layer and the flexible solar energy surface layer are all built in the moon, optical fibers are buried in the optical fiber system prefabricating layer and are connected with indoor equipment through connectors, the inner membrane of the flexible inner membrane layer surrounds to form a cavity under the action of pressure and continuously forms a pressure keeping shape, the air inflation structure reinforcing layer is made of polymer foam doped with simulated lunar soil and boron-containing compounds through foaming, the surface of the optical fiber system prefabricated layer is coated with an inner decoration layer, and the surface of the optical fiber system prefabricated layer is provided with a sampler chip and an inductor contact.
Compared with the prior art, the invention has the following effects:
the folding and unfolding support is simple in structure, and a hexagonal structure is formed by prefabricating, rooting on the surface of a moon in a standardized manner on the earth, mechanically unfolding the moon and then restarting and unfolding the moon, so that a hexagonal spliced structure system and a construction scheme are provided for a moon building.
Compared with a round or spherical inflatable unfolding structure in the prior art, the hexagonal-prism-shaped inflatable unfolding structure has the advantages that the construction mode of mechanical unfolding and inflatable unfolding is well combined, the requirements of the aerospace material on lightness and small occupied area during launching are met, and the hexagonal-prism-shaped inflatable unfolding structure is suitable for constructing moon and space buildings;
through the design of this application hexagon structure, realize the high-efficient connection between the cabin body. The cabin body is hexagonal after being completely unfolded, and is a structural form which is high in utilization rate, convenient for modular expansion, optimal in structure, most economical in material, low in form factor and excellent in sustainable performance and is suitable for construction of a lunar base. Strip-shaped inflation channels can be added between the cabin bodies for indirect connection, and the cabin bodies can also be directly connected through two parts outside the cabin doors, so that connection between the cabin bodies is realized, and the moon base with a certain scale can be expanded.
Drawings
FIG. 1 is a schematic perspective view of the present application in an expanded state;
FIG. 2 is a schematic perspective view of the folded state of the present application;
fig. 3 is a schematic perspective view of the present application when the bottom slide rail and the bottom side plate are in an unfolded state;
FIG. 4 is a schematic view of a mechanically deployed partially fully deployed state;
FIG. 5 is a schematic view of the connection of two adjacent building modules;
FIG. 6 is a schematic view of a splicing structure of an inflatable membrane;
FIGS. 7(a), (b) and (c) illustrate three connection modes of building modules;
FIG. 8 is a schematic cross-sectional view of an inflatable membrane;
fig. 9(a) shows an inverted hook structure with the tip of the telescopic limiting claw facing upwards, and (b) shows a gripper structure with the tip of the telescopic limiting claw facing downwards.
Detailed Description
The first embodiment is as follows: the present embodiment is described with reference to fig. 1 to 9, and a hexagonal inflatable unfolding building module applied to a lunar building comprises an unfolding bracket and an inflatable membrane, wherein the unfolding bracket comprises three push-pull doors 1, three sets of top slide rails 2, three sets of bottom slide rails 3, a regular hexagonal top plate 4 and a regular hexagonal bottom plate 5 which are arranged opposite to each other from top to bottom, wherein three top side plates 6 are uniformly distributed in the circumferential direction of the regular hexagonal top plate 4, the three top side plates 6 are correspondingly hinged to three side surfaces of the regular hexagonal top plate 4, three bottom side plates 7 are uniformly distributed in the circumferential direction of the regular hexagonal bottom plate 5, and the three sets of bottom slide rails 3 and the three bottom side plates 7 are arranged in a staggered manner and correspondingly hinged to six side surfaces of the regular hexagonal bottom plate 5;
in a folded state of the building module, a top side plate 6, a bottom side plate 7, a push-pull cabin door 1, a top sliding rail 2 and a bottom sliding rail 3 are vertically arranged, the three push-pull cabin doors 1 are correspondingly positioned right below the three top side plates 6, the push-pull cabin doors 1 are correspondingly connected with the top side plates 6 through the top sliding rail 2, and one end part of each top sliding rail 2 is in sliding connection with the top side plate 6, the other end part of each top sliding rail 2 is in sliding connection with the top of the push-pull cabin door 1, and the bottom of each push-pull cabin door 1 is in sliding connection with the bottom sliding rail 3; under folded state, the other end of the bottom side plate 7 is fixedly connected with the regular hexagon top plate 4, and the fixedly connected mode can be a buckle connection.
Under the unfolding state of the building module, the regular hexagon bottom plate 5, the three bottom side plates 7 and the three groups of bottom sliding rails 3 are all positioned on the same horizontal plane, the three push-pull cabin doors 1 slide to the other ends of the bottom sliding rails 3, the inflatable membrane is inflated and unfolded, and the cross section of the inflated membrane after being unfolded is of a hexagon structure. Under the folding state of the building module, the top sliding rail 2 is positioned between the push-pull cabin door 1 (or the top side plate 6) and the bottom sliding rail 3, so that the space is effectively saved. The three top side plates 6 and the three bottom side plates 7 are arranged in a staggered manner from top to bottom. The step 11 is rotatably installed at the lower part of the door frame of the push-pull cabin door 1, and in the unfolded state of the building module, the step 11 extends to the outside of the building module and is erected on the moon surface. The structure of the step 11 is prior art and will not be described herein. Under the folding state of the building module, the steps 11 are folded into the door frame of the push-pull cabin door 1 and are attached to the cabin door for placement.
The building module of this application can splice into the building community as required, and when every two building module concatenations that face each other, the accessible loops through the soft connection calibration of commonly used among the prior art of spaceflight and carries out zonulae occludens with the lapped mode of rigid fastener. When an emergency situation occurs in one of the cabins (i.e. the building module), the emergency alarm device informs the cabin door to close the adjacent cabin door and separate from the close connection.
As shown in fig. 5, the connection between the adjacent cabins a and B can be realized by directly connecting the two cabins, and the connection between the cabins a and C at a distance can also be realized by adding the strip-shaped passage D. The length and the style of D have no uniform requirement, and various connections can be realized. Figure 7 illustrates the splicing of three types of cabins. A plurality of capsule bodies can be connected in various modes to form a capsule body community with strong air tightness. The safety of each independent cabin body is guaranteed through an intelligent early warning mechanism between the cabin doors.
The hexagonal spliced structural system and the construction scheme are provided for a lunar building by prefabricating and rooting the earth on the surface of a moon in a standardized manner, mechanically unfolding the earth in the moon and then restarting and unfolding the earth to form a hexagonal structure.
Compared with a round or spherical inflatable unfolding structure in the prior art, the hexagonal-prism-shaped inflatable unfolding structure has the advantages that the construction mode of mechanical unfolding and inflatable unfolding is well combined, the requirements of the aerospace material on lightness and small occupied area during launching are met, and the hexagonal-prism-shaped inflatable unfolding structure is suitable for constructing moon and space buildings;
through the design of this application hexagon structure, realize the high-efficient connection between the cabin body. The cabin body is hexagonal after being completely unfolded, and is a structural form which is high in utilization rate, convenient for modular expansion, optimal in structure, most economical in material, low in form factor and excellent in sustainable performance and is suitable for construction of a lunar base. Strip-shaped inflation channels can be added between the cabin bodies for indirect connection, and the cabin bodies can also be directly connected through two parts outside the cabin doors, so that connection between the cabin bodies is realized, and the moon base with a certain scale can be expanded.
A plurality of first locating levers 8 are installed to the bottom of regular hexagon bottom plate 5, and two at least second locating levers 9 are installed to the door frame bottom of push-and-pull hatch door 1, and first locating lever 8 and second locating lever 9 are axial telescopic link. Because the lunar surface is often uneven surface, consequently, through the flexible length adjustment of first locating lever 8, realize the adjustment of whole building module horizontal position, play the fixed action when keeping whole building module level. This application is through setting up the locating lever for the cabin body is higher than the moon surface. The cabin body is lifted and fixed by penetrating the positioning rod into the lunar surface, so that the irregular surface of the moon is avoided.
The first positioning rod 8 can be an electric telescopic rod or any other rod-shaped structure capable of realizing the change of the telescopic state of the rod. The cross-section of the first positioning rod 8 may be circular, rectangular or any other shape. Can be fixed connection between first locating lever 8 and the regular hexagon bottom plate 5, also can be for rotating the connection, during fixed connection, the vertical setting of first locating lever 8 and top and the 5 rigid couplings of regular hexagon bottom plate, during the rotation connection, the one end rotation of first locating lever 8 is installed in the 5 bottoms of regular hexagon bottom plate. In building module folded state, first locating lever 8 level laminating regular hexagon bottom plate 5 arranges, and under building module unfolded state, first locating lever 8 turns over to vertical position, and the other end inserts and establishes in the lunar soil on moon surface. The second positioning rod 9 is axially and fixedly arranged at the bottom of the door frame of the push-pull cabin door 1.
The number of the first positioning rods 8 and the second positioning rods 9 is six.
And one end of each positioning rod, which is close to lunar soil, is provided with a telescopic limiting claw 10 in a vertical state. The telescopic limiting claw 10 can be a gripping structure with a downward pointed part or an inverted hook structure with an upward pointed part. Through telescopic spacing claw 10, can be so that the more firm cartridge of locating lever is at the lunar surface, prevent the unstable problem in building module position because of other external forces such as strong wind cause.
A plurality of first locating rods 8 are uniformly distributed along the circumferential direction of the regular hexagon bottom plate 5.
The top and the bottom of the inflatable membrane are respectively and correspondingly connected with the regular hexagon top plate 4 and the regular hexagon bottom plate 5 in a sealing way, and the side surface of the inflatable membrane is connected with the three push-pull cabin doors 1 in a sealing way. The splicing mode of the inflatable membrane can be various, and the cross section of the lower part of the inflatable membrane is ensured to be in a hexagonal structure. The splicing mode of the inflatable membrane is as follows: six pieces of trapezoidal membranes 12 are selected, the side faces of the trapezoidal membranes are sequentially spliced to form a ring shape, the top ends of the six pieces of trapezoidal membranes 12 are correspondingly connected with the regular hexagon top plate 4 in a sealing mode, nine pieces of rectangular membranes 13 with the same height as the push-pull cabin door 1 are selected to form a hexagon structure in a surrounding mode, and one piece of hexagonal membrane 14 is selected to serve as a cabin body bottom plate.
The bottom slide rail 3 is in an H-shaped structure in an unfolded state. So design, structural stability is better.
The push-pull cabin door 1 and the top sliding rail 2 and the push-pull cabin door 1 and the bottom sliding rail 3 are respectively connected through pulleys.
The push-pull hatch door 1 is of a rectangular structure.
The inflatable membrane comprises an optical fiber system prefabricated layer 15, a flexible inner membrane layer 16, an inflatable structure reinforced layer 17, a flexible heat-insulating layer 18, a flexible protective layer 19, a lunar soil filling layer 20, a lunar soil reinforced layer 21 and a flexible solar energy surface layer 22 which are sequentially arranged, wherein the optical fiber system prefabricated layer 15, the flexible inner membrane layer 16, the inflatable structure reinforced layer 17, the flexible heat-insulating layer 18 and the flexible protective layer 19 are prefabricated in the ground, the lunar soil filling layer 20, the lunar soil reinforced layer 21 and the flexible solar energy surface layer 22 are all built in the moon, optical fibers are buried in the optical fiber system prefabricated layer 15 and are connected with indoor equipment through joints, under the action of pressure, an inner membrane of the flexible inner membrane layer 16 surrounds a cavity and continuously forms a pressure maintaining shape, the inflatable structure reinforced layer 17 is made of polymer foam doped with simulated lunar soil and boron-containing compounds, the surface of the optical fiber system prefabricated layer 15 is coated with an inner decoration layer 23, the surface of the optical fiber system prefabricated layer 15 is provided with a sampler chip and an inductor joint. The lunar soil filling layer 20 is a filling layer with equal density of lunar soil or simulated lunar soil (such as lunar soil bags or lunar soil bricks), and each layer of structure prefabricated on the ground is attached to the surface of the inflatable living cabin.
The surface of the optical fiber system prefabrication layer 15 is coated with an inner decoration layer. The inner decoration layer adopts a ZS-1 high-temperature heat-insulation protective coating, and is added with a yellow-green warm-color additive. The space-saving decorative plate is suitable for human engineering, and the moods of tension and anxiety in the environment with relatively concentrated space are relieved to a certain extent through the material and the color of the inner decorative layer. The thickness is 0.1 mm.
The optical fiber system prefabrication layer 15 is used for embedding the optical fiber in the coating layer, and the polyimide coating is used for the coating layer, so that the optical fiber can still be normally used at 300 ℃. The light external interface adopts PC model. The connector for connecting the indoor equipment and the optical fiber is a standard connector and is arranged on the surface of the prefabricated layer 15 of the optical fiber system. The thickness of the optical fiber system preform layer 15 is about 300-.
The flexible inner film layer 16 is a spacer layer between the aerogel-like insulation layer and the optical fiber system prefabricated layer 15.
The flexible protective layer 19 mainly plays a role in protection, facilitates the monthly construction of the external layer, and prevents the machine from generating abrasion damage to the flexible insulating layer 18 when the external layer is constructed monthly; secondly, the lunar soil filling layer 20 can be more tightly fixed.
The solar surface layer positioned on the outermost side of the wall body mainly has the functions of absorbing sunlight and converting solar radiation energy into electric energy for the lunar building.
The lunar soil reinforcing layer 21 is made by 3D printing, forms a high-strength and high-density shell, and mainly plays a role in protecting an inner layer structure and bearing energy of space meteorite impact.
The lunar soil filling layer 20 has a low thermal conductivity and mainly functions to preserve heat and resist radiation. The material is lunar soil or simulated lunar soil, such as lunar soil bags or lunar soil bricks, and the lunar soil is prepared by utilizing collected lunar soil in the moon by a lunar robot.
The inflatable structure reinforcing layer 17 plays a role in structural reinforcement by utilizing the self-reaction principle of a foaming agent after inflation, and can play a role in secondary radiation protection and meteorite impact buffering through the application of aerogel materials. The boron-containing compound is boric acid and the polymer foam is polyimide foam. The particle size of the simulated lunar soil is 100 microns. After the inflatable cabin is inflated and unfolded, all the components are uniformly mixed, and foaming is carried out in the cavity of the cabin to form the inflatable structure reinforcing layer 17.
The flexible insulation layer 18 serves to protect the interior space of the building against extreme high and low temperature alternating environments during the day and night.
The flexible insulation 18 is preferably an aerogel-like insulation that is constructed of a lightweight insulating material.
By using the multilayer flexible composite material and the structure and utilizing lunar soil, multiple protection on space high-energy radiation, lunar surface high and low temperature and micro-fluidic stars can be realized, and a better protection effect is realized at the cost of smaller emission weight.
The utility model provides a composite wall structure can adapt to the folding and the expansion demand in the moon face deployable cabin of living. The inflatable structure reinforcing layer 17 in the wall body is filled by the moonface in-situ foaming process after the inflatable cabin body is completely unfolded, so that the launching weight can be effectively reduced, and the launching cost can be reduced.
After the organic foam material is doped with lunar soil and a boron-containing compound, the combined shielding effect of the high atomic number and low atomic number combined material and the efficient absorption of boron element to neutrons can form better protection effect on cosmic ray high-energy particles and a large amount of secondary neutrons generated by the effect of cosmic ray and lunar surface.
The flexible solar surface skin layer 22, the lunar soil reinforcing layer 21 and the lunar soil filling layer 20 are processed and built in the moon, so that lunar surface in-situ resource utilization can be fully realized, and the structural strength and the mechanical property of the composite wall body are enhanced.
The flexible inner film layer 16 is made of Kevlar composite material, and an aluminum layer is attached to the surface of the flexible inner film layer 16. In the aerated structure reinforcing layer 17, the dosage ratio of the simulated lunar soil, the boron-containing compound and the polymer foam material is 15:4: 31. The flexible heat-insulating layer 18 is made of silicon dioxide aerogel. The flexible protective layer 19 comprises a plurality of layers of high strength textile material. The lunar soil reinforcing layer 21 is made by printing through lunar soil and an adhesive by a 3D printer. The solar skin layer includes a plurality of flexible solar panels.
The working principle is as follows:
when the building module is in a folded state, namely the building module is in a hexagonal prism cabin structure, the building module is launched to the lunar surface, the first positioning rod 8 is unfolded and pricked into the lunar surface, the cabin body is lifted 500-600mm away from the lunar surface, and a horizontal calibrator can be arranged on the regular hexagonal base plate 5 to accurately adjust the horizontal position of the building module;
the three bottom side plates 7 and the three bottom slide rails 3 are respectively opened along the hinged edges in a clockwise rotating manner, and form the bottom surface of the cabin body together with the regular hexagonal bottom plate 5.
The three push-pull cabin doors 1 horizontally slide out along the bottom sliding rails 3, and meanwhile, the top sliding rails 2 are unfolded until the push-pull cabin doors 1 and the top side plates 6 are respectively positioned at two ends of the top sliding rails 2.
After the preliminary calibration, the second positioning rod 9 is unfolded and stabbed into the lunar surface, and at this point, the mechanical unfolding is completed to form a rigid structure.
The inflatable membrane is inflated by the inflating device to be completely unfolded to the hexagonal state. The step 11 is unfolded, and the whole building module is unfolded.
After the building modules are unfolded, a plurality of building modules (namely cabin bodies) can be connected according to actual needs to form a building group.
When only one building module is provided, the flexible solar surface skin layer 22, the lunar soil reinforcing layer 21 and the lunar soil filling layer 20 of the inflatable membrane are processed and built in the moon after the whole building module is unfolded. When there are a plurality of building modules, the flexible solar skin layer 22, the lunar soil reinforcing layer 21 and the lunar soil filling layer 20 of the inflatable membrane are processed and built in the moon after the building group is formed.
Claims (9)
1. The utility model provides a be applied to hexagon of moon building and aerify and expand building module which characterized in that: the folding and unfolding support comprises three push-pull cabin doors (1), three groups of top sliding rails (2), three groups of bottom sliding rails (3), and a regular hexagon top plate (4) and a regular hexagon bottom plate (5) which are arranged in an up-down opposite mode, wherein three top side plates (6) are uniformly distributed in the circumferential direction of the regular hexagon top plate (4), the three top side plates (6) are correspondingly hinged with three side faces of the regular hexagon top plate (4), three bottom side plates (7) are uniformly distributed in the circumferential direction of the regular hexagon bottom plate (5), and the three groups of bottom sliding rails (3) and the three bottom side plates (7) are arranged in a staggered mode and correspondingly hinged with six side faces of the regular hexagon bottom plate (5);
under a folded state of the building module, a top side plate (6), a bottom side plate (7), a push-pull cabin door (1), a top sliding rail (2) and a bottom sliding rail (3) are vertically arranged, the three push-pull cabin doors (1) are correspondingly positioned under the three top side plates (6), the push-pull cabin doors (1) are correspondingly connected with the top side plates (6) through the top sliding rail (2), and one end part of each top sliding rail (2) is in sliding connection with the top side plate (6), the other end part of each top sliding rail (2) is in sliding connection with the top of the push-pull cabin door (1), and the bottom part of each push-pull cabin door (1) is in sliding connection with the bottom sliding rail (3);
when the building module is unfolded, the regular hexagon bottom plate (5), the three bottom side plates (7) and the three groups of bottom sliding rails (3) are all positioned on the same horizontal plane, the three push-pull cabin doors (1) slide to the other ends of the bottom sliding rails (3), the inflatable membrane is inflated and unfolded, and the cross section of the inflated membrane after being unfolded is of a hexagon structure;
the lower part of the door frame of the push-pull cabin door (1) is rotatably provided with a step (11), and the step (11) extends to the outside of the building module and is erected on the surface of a moon ball when the building module is unfolded.
2. A hexagonal inflatable unfolding building module for moon building application according to claim 1, characterized in that: a plurality of first locating rods (8) are installed at the bottom of the regular hexagon bottom plate (5), at least two second locating rods (9) are installed at the bottom of a door frame of the push-pull cabin door (1), and the first locating rods (8) and the second locating rods (9) are axial telescopic rods.
3. A hexagonal inflatable unfolding building module for moon building application according to claim 2, characterized in that: and one end of each positioning rod, which is close to lunar soil, is provided with a telescopic limiting claw (10) in a vertical state.
4. A hexagonal inflatable unfolding building module for moon buildings according to claim 2 or 3, characterized in that: a plurality of first locating rods (8) are uniformly distributed along the circumferential direction of the regular hexagon bottom plate (5).
5. A hexagonal inflatable unfolding building module for moon building application according to claim 1, characterized in that: the top and the bottom of the inflatable membrane are respectively and correspondingly connected with the regular hexagon top plate (4) and the regular hexagon bottom plate (5) in a sealing way, and the side surface of the inflatable membrane is connected with the three push-pull cabin doors (1) in a sealing way.
6. A hexagonal inflatable unfolding building module for moon building application according to claim 1, characterized in that: the bottom slide rail (3) is in an H-shaped structure in an unfolded state.
7. A hexagonal inflatable unfolding building module for moon building application according to claim 1, characterized in that: the push-pull cabin door (1) is connected with the top sliding rail (2) and the push-pull cabin door (1) is connected with the bottom sliding rail (3) through pulleys.
8. A hexagonal inflatable unfolding building module for moon building application according to claim 1, characterized in that: the push-pull cabin door (1) is of a rectangular structure.
9. A hexagonal inflatable unfolding building module for moon building application according to claim 1, characterized in that: the inflatable membrane comprises an optical fiber system prefabricated layer (15), a flexible inner membrane layer (16), an inflatable structure reinforcing layer (17), a flexible heat insulation layer (18), a flexible protective layer (19), a lunar soil filling layer (20), a lunar soil reinforcing layer (21) and a flexible solar energy surface layer (22) which are sequentially arranged, wherein the optical fiber system prefabricated layer (15), the flexible inner membrane layer (16), the inflatable structure reinforcing layer (17), the flexible heat insulation layer (18) and the flexible protective layer (19) are all prefabricated in the ground, the lunar soil filling layer (20), the lunar soil reinforcing layer (21) and the flexible solar energy surface layer (22) are all built in the moon, optical fibers are buried in the optical fiber system prefabricated layer (15) and are connected with indoor equipment through joints, a cavity is enclosed by an inner membrane of the flexible inner membrane layer (16) under the action of pressure and the pressure is continuously kept, and the inflatable structure reinforcing layer (17) is made of foamed polymer foam doped with simulated lunar soil and boron-containing compounds, the surface of the optical fiber system prefabrication layer (15) is coated with an inner decoration layer (23), and the surface of the optical fiber system prefabrication layer (15) is provided with a sampler chip and an inductor contact.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110520161.3A CN113187314A (en) | 2021-05-12 | 2021-05-12 | Hexagonal inflatable unfolding building module applied to moon building |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113309227A (en) * | 2021-05-28 | 2021-08-27 | 哈尔滨工业大学建筑设计研究院 | Moon cabin body structure system combining mechanical expansion and inflation expansion and method |
| CN116084571A (en) * | 2023-02-20 | 2023-05-09 | 哈尔滨工业大学 | Annular base unit module and modularized annular lunar surface base built by using same |
Citations (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020190161A1 (en) * | 2001-06-18 | 2002-12-19 | Honeywell International, Law Dept. Ab2 | Deployable flexible airlock |
| JP2003237698A (en) * | 2002-02-20 | 2003-08-27 | Sakase Adtec Kk | Inflatable structure developing method, folded structure developing method and foldable structure |
| KR20090079863A (en) * | 2009-07-02 | 2009-07-22 | 강동우 | Construction method of buidlings using flexible form |
| CN103498579A (en) * | 2013-10-10 | 2014-01-08 | 苏运升 | House, inflatable house, container house and method for constructing container house |
| CN104196122A (en) * | 2014-07-24 | 2014-12-10 | 苏运升 | Folding box body type inflation mold house |
| CN104966892A (en) * | 2015-05-18 | 2015-10-07 | 西北工业大学 | Regularly-hexagonal plane unfolding mechanism |
| CN107933959A (en) * | 2017-10-13 | 2018-04-20 | 中国科学院深圳先进技术研究院 | Six-bar mechanism and what is be made from it open up module, extending arm, planar development truss |
| CN109991071A (en) * | 2019-04-22 | 2019-07-09 | 大连理工大学 | The portable far-reaching extra large seabed soil of ship base is come personally strength testing device |
| CN110258811A (en) * | 2019-07-25 | 2019-09-20 | 苏州嘉谷环保科技有限公司 | A kind of collapsible house and method for folding |
| CN110745257A (en) * | 2019-10-12 | 2020-02-04 | 上海宇航系统工程研究所 | Foldable supporting structure |
| CN110828964A (en) * | 2019-09-30 | 2020-02-21 | 中国空间技术研究院 | Torsion spring driven single-layer regular hexagon conical deployable truss antenna structure |
| CN110978680A (en) * | 2019-10-30 | 2020-04-10 | 北京空间飞行器总体设计部 | Space multifunctional inflatable sealed cabin skin structure suitable for manned environment |
| CN210563724U (en) * | 2019-05-25 | 2020-05-19 | 仪征龙兴塑胶有限公司 | Combined tent |
| CN111268179A (en) * | 2020-02-24 | 2020-06-12 | 四川航天系统工程研究所 | Protective structure for lunar surface living cabin body |
| CN111502008A (en) * | 2020-05-07 | 2020-08-07 | 中山大学 | Membrane-shell composition structure suitable for space base and construction method |
| CN211421391U (en) * | 2019-12-10 | 2020-09-04 | 重庆建筑工程职业学院 | Assembled membrane structure unit type component |
| CN111874272A (en) * | 2020-07-16 | 2020-11-03 | 北京空间技术研制试验中心 | Flexible deployable moon living cabin |
| CN212336322U (en) * | 2020-05-15 | 2021-01-12 | 易欣航 | Rapidly-unfolded large-space emergency combined unit and emergency combined system |
| CN112324236A (en) * | 2020-11-13 | 2021-02-05 | 长沙中联消防机械有限公司 | Tent and tent vehicle |
| CN112407333A (en) * | 2020-11-10 | 2021-02-26 | 哈尔滨工业大学 | Large-folding-aspect-ratio deployable cabin section mechanism |
| CN112482874A (en) * | 2020-12-17 | 2021-03-12 | 上海金标文化创意股份有限公司 | Telescopic device for folding house |
| CN112478199A (en) * | 2020-11-27 | 2021-03-12 | 南京航空航天大学 | Satellite flexible repeatable folding and unfolding defense device for resisting physical impact |
| CN112591145A (en) * | 2021-01-14 | 2021-04-02 | 哈尔滨工业大学 | Flexible film inflatable cylinder with reinforcing sheath and rectangular parallelepiped containing and folding method thereof |
| CN112644736A (en) * | 2021-01-05 | 2021-04-13 | 东南大学 | Deflection folding inflatable block point connection capsule shell structure |
| CN216142511U (en) * | 2021-05-12 | 2022-03-29 | 哈尔滨工业大学建筑设计研究院 | Hexagonal inflatable unfolding building module applied to moon building |
-
2021
- 2021-05-12 CN CN202110520161.3A patent/CN113187314A/en active Pending
Patent Citations (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020190161A1 (en) * | 2001-06-18 | 2002-12-19 | Honeywell International, Law Dept. Ab2 | Deployable flexible airlock |
| JP2003237698A (en) * | 2002-02-20 | 2003-08-27 | Sakase Adtec Kk | Inflatable structure developing method, folded structure developing method and foldable structure |
| KR20090079863A (en) * | 2009-07-02 | 2009-07-22 | 강동우 | Construction method of buidlings using flexible form |
| CN103498579A (en) * | 2013-10-10 | 2014-01-08 | 苏运升 | House, inflatable house, container house and method for constructing container house |
| CN104196122A (en) * | 2014-07-24 | 2014-12-10 | 苏运升 | Folding box body type inflation mold house |
| CN104966892A (en) * | 2015-05-18 | 2015-10-07 | 西北工业大学 | Regularly-hexagonal plane unfolding mechanism |
| CN107933959A (en) * | 2017-10-13 | 2018-04-20 | 中国科学院深圳先进技术研究院 | Six-bar mechanism and what is be made from it open up module, extending arm, planar development truss |
| CN109991071A (en) * | 2019-04-22 | 2019-07-09 | 大连理工大学 | The portable far-reaching extra large seabed soil of ship base is come personally strength testing device |
| CN210563724U (en) * | 2019-05-25 | 2020-05-19 | 仪征龙兴塑胶有限公司 | Combined tent |
| CN110258811A (en) * | 2019-07-25 | 2019-09-20 | 苏州嘉谷环保科技有限公司 | A kind of collapsible house and method for folding |
| CN110828964A (en) * | 2019-09-30 | 2020-02-21 | 中国空间技术研究院 | Torsion spring driven single-layer regular hexagon conical deployable truss antenna structure |
| CN110745257A (en) * | 2019-10-12 | 2020-02-04 | 上海宇航系统工程研究所 | Foldable supporting structure |
| CN110978680A (en) * | 2019-10-30 | 2020-04-10 | 北京空间飞行器总体设计部 | Space multifunctional inflatable sealed cabin skin structure suitable for manned environment |
| CN211421391U (en) * | 2019-12-10 | 2020-09-04 | 重庆建筑工程职业学院 | Assembled membrane structure unit type component |
| CN111268179A (en) * | 2020-02-24 | 2020-06-12 | 四川航天系统工程研究所 | Protective structure for lunar surface living cabin body |
| CN111502008A (en) * | 2020-05-07 | 2020-08-07 | 中山大学 | Membrane-shell composition structure suitable for space base and construction method |
| CN212336322U (en) * | 2020-05-15 | 2021-01-12 | 易欣航 | Rapidly-unfolded large-space emergency combined unit and emergency combined system |
| CN111874272A (en) * | 2020-07-16 | 2020-11-03 | 北京空间技术研制试验中心 | Flexible deployable moon living cabin |
| CN112407333A (en) * | 2020-11-10 | 2021-02-26 | 哈尔滨工业大学 | Large-folding-aspect-ratio deployable cabin section mechanism |
| CN112324236A (en) * | 2020-11-13 | 2021-02-05 | 长沙中联消防机械有限公司 | Tent and tent vehicle |
| CN112478199A (en) * | 2020-11-27 | 2021-03-12 | 南京航空航天大学 | Satellite flexible repeatable folding and unfolding defense device for resisting physical impact |
| CN112482874A (en) * | 2020-12-17 | 2021-03-12 | 上海金标文化创意股份有限公司 | Telescopic device for folding house |
| CN112644736A (en) * | 2021-01-05 | 2021-04-13 | 东南大学 | Deflection folding inflatable block point connection capsule shell structure |
| CN112591145A (en) * | 2021-01-14 | 2021-04-02 | 哈尔滨工业大学 | Flexible film inflatable cylinder with reinforcing sheath and rectangular parallelepiped containing and folding method thereof |
| CN216142511U (en) * | 2021-05-12 | 2022-03-29 | 哈尔滨工业大学建筑设计研究院 | Hexagonal inflatable unfolding building module applied to moon building |
Non-Patent Citations (6)
| Title |
|---|
| 于登云等: "月球基地结构形式设想", 《宇航学报》 * |
| 付新卫等: "柔性可展开太空舱研究进展", 《航天返回与遥感》 * |
| 冯鹏等: "基于月面原位资源的月球基地建造技术", 《工业建筑》 * |
| 徐彦等: "充气式月球基地防护结构技术综述", 《载人航天》 * |
| 杨宏等: "《载人航天器技术》", 31 May 2018, 北京理工大学出版社 * |
| 邓连印等: "月球基地工程研究进展与展望", 《导弹与航天运载技术》 * |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113309227A (en) * | 2021-05-28 | 2021-08-27 | 哈尔滨工业大学建筑设计研究院 | Moon cabin body structure system combining mechanical expansion and inflation expansion and method |
| CN113309227B (en) * | 2021-05-28 | 2022-11-15 | 哈尔滨工业大学建筑设计研究院 | Moon cabin body structure system combining mechanical expansion and inflation expansion and method |
| CN116084571A (en) * | 2023-02-20 | 2023-05-09 | 哈尔滨工业大学 | Annular base unit module and modularized annular lunar surface base built by using same |
| CN116084571B (en) * | 2023-02-20 | 2023-08-29 | 哈尔滨工业大学 | Annular base unit module and modularized annular lunar surface base built by using same |
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