Quick-assembly connecting structure of space capsule framework

Abstract

The utility model discloses a space capsule framework fast-assembly connecting structure, which belongs to the technical field of civil space capsules and comprises wall surface frameworks, a plurality of groups of wall surface connecting mechanisms, a top cover framework and a top cover connecting mechanism, the wall surface frameworks are formed by sequentially splicing a plurality of wall surface frameworks, and two connecting frameworks are arranged between the wall surface frameworks. The connecting frames are arranged at the two opposite ends of the wall face framework, the wall face connecting mechanisms are arranged between the adjacent wall face frameworks and between the connecting frames and the adjacent wall face frameworks respectively, and each wall face connecting mechanism is composed of a stud and two wall face connecting nuts. The top cover framework is arranged at the top of the wall surface framework and is formed by sequentially splicing a plurality of top cover frames; the top cover connecting mechanism is composed of a multi-section threaded screw and a plurality of top cover connecting nuts. The multi-section threaded screw penetrates through the top cover framework at one end of the top cover framework to the top cover framework at the other end of the top cover framework. According to the utility model, the assembling or disassembling efficiency of the internal framework of the space capsule can be improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to the technical field of civilian space cabin, concretely relates to a space cabin framework fast -assembling connecting structure. BACKGROUND

[0002] The civilian space cabin, also known as an outdoor sunlight room, is a kind of fabricated building, which is used for people to carry out leisure and entertainment or accommodation at outdoor scenic spots. As a new accommodation mode, the civilian space cabin has attracted much attention in recent years due to its unique design and accommodation experience. Since the civilian space cabin usually needs to be frequently replaced and installed at outdoor locations, the civilian space cabin usually has the advantage of being convenient to disassemble and reassemble, which facilitates the disassembly and reinstallation of the space cabin and the transportation of the civilian space cabin.

[0003] Based on the above situation, the Chinese patent with publication number CN220908702U discloses a framework of a civilian space cabin, which comprises a base, vertical beams, a top cover assembly, a window frame, a door frame, an air conditioner outdoor unit mounting rack and a fine adjustment foot assembly. The base is horizontally arranged and is a frame body welded by a plurality of metal pipes and plates. The upper surface of the base is flat, and the bottom thereof is provided with a plurality of fine adjustment foot assemblies. The front and rear sides of the upper surface of the base are respectively connected with the vertical beams arranged vertically. The two vertical beams are arranged in parallel and at intervals. The vertical beams are flat frame bodies, and the upper and lower surfaces thereof are composed of flat square tubes. The square tubes are provided with two limiting grooves. The limiting grooves are strip-shaped through holes penetrating through the upper and lower surfaces of the square tubes. The top cover assembly is horizontally arranged and is arranged on the top of the vertical beams and aligned with the base.

[0004] The above patent document discloses a firm and stable framework structure of a civilian space cabin. The metal pipes and plates in the framework of the civilian space cabin are fixed by welding, which ensures the firmness of the civilian space cabin. However, this increases the difficulty of on-site installation of the civilian space cabin. If the civilian space cabin is transported after being completely assembled, the transportation difficulty will be increased due to the large occupied area of the civilian space cabin. In addition, the welded fixation also makes it difficult to disassemble and transfer the framework structure of the civilian space cabin, which affects the convenience of the civilian space cabin during use. Therefore, the framework of the civilian space cabin still has room for improvement. UTILITY MODEL CONTENTS

[0005] In view of the technical defects in the background art, the utility model provides a space cabin framework fast-assembling connecting structure, which solves the above technical problems and meets the actual needs. The specific technical solution is as follows:

[0006] The utility model provides a space cabin framework fast -assembling connecting structure, including wall surface framework, a plurality of wall surface connecting mechanism, top cover framework, top cover connecting mechanism, the wall surface framework is by a plurality of wall surface frame and connects and is sequentially spliced, the wall surface framework is equipped with two and is equipped with two connecting frame between two wall surface frameworks, the connecting frame is located wall surface framework opposite both ends, wall surface connecting mechanism is respectively arranged between adjacent wall surface frame and connecting frame and adjacent wall surface frame, wall surface connecting mechanism is by the two wall surface connecting nut of matched double -end bolt, top cover framework is located two wall surface framework top, top cover framework is by a plurality of top cover frame and connects and is sequentially spliced, top cover connecting mechanism is by the several top cover connecting nut of matched multistage thread screw rod, multistage thread screw rod is from top cover framework one end's top cover frame and is penetrated to another end's top cover framework.

[0007] Top cover framework is located two wall surface framework top, top cover framework is by a plurality of top cover frame and connects and is sequentially spliced, top cover connecting mechanism is by the several top cover connecting nut of matched multistage thread screw rod, multistage thread screw rod is from top cover framework one end's top cover frame and is penetrated to another end's top cover framework.

[0008] As a further technical scheme of the utility model, the double-end bolt penetrates through the adjacent two wall surface frames or the adjacent connecting frame and wall surface frame, and the double-end bolt is provided with a first thread matched with the wall surface connecting nut at both ends.

[0009] As a further technical scheme of the utility model, the multistage thread screw rod is provided with a second thread matched with the top cover connecting nut between the adjacent top cover frames, two top cover connecting nuts are sleeved on the surface of each second thread, and the two top cover connecting nuts are respectively abutted against the surfaces of the adjacent two top cover frames.

[0010] As a further technical scheme of the utility model, the wall surface framework is provided with a plurality of connecting slots at the top, the top cover framework is provided with a plurality of connecting pins matched with the connecting slots at the bottom, and the connecting slots and the connecting pins are penetrated by the mutually matched fixing through holes.

[0011] As a further technical scheme of the utility model, the top cover frames at both ends of the top cover framework are arranged at the top of the connecting frame and the wall surface frame adjacent to the connecting frame, and the remaining top cover frames are arranged at the top of the two adjacent wall surface frames.

[0012] The utility model has the beneficial effects that:

[0013] The utility model is spliced by the wall surface framework and the top cover framework, has good structural stability, the wall surface framework is spliced by a plurality of wall surface frames and connecting frame frames through the wall surface connecting mechanism, the top cover framework is sequentially spliced by a plurality of top cover frames through the top cover connecting mechanism, the wall surface framework can be quickly assembled or disassembled through the wall surface connecting mechanism, the top cover framework can also be quickly assembled or disassembled through the top cover connecting mechanism, and the efficiency of the internal framework assembly or disassembly of the space cabin is improved. BRIEF DESCRIPTION OF DRAWINGS

[0014] Figure 1 It is a front view of a space cabin framework fast-assembly connecting structure.

[0015] Figure 2 It is a top view of a wall framework of a space cabin framework fast-assembly connecting structure.

[0016] Figure 3 It is a top view of a top cover framework of a space cabin framework fast-assembly connecting structure.

[0017] Figure 4 It is Figure 1 a partial schematic view at A in the figure.

[0018] Figure 5 It is Figure 1 a partial schematic view at B in the figure.

[0019] Figure 6 It is Figure 3 a partial schematic view at C in the figure.

[0020] Figure 7 It is Figure 3 a partial schematic view at D in the figure.

[0021] Figure 8 It is a structure schematic of a connecting slot and a connecting bolt of a space cabin framework fast-assembly connecting structure Figure 1 .

[0022] Figure 9 It is a structure schematic of a connecting slot and a connecting bolt of a space cabin framework fast-assembly connecting structure Figure 2 .

[0023] Wherein: 1-wall framework, 11-wall frame, 12-connecting frame, 13-connecting slot, 2-wall connecting mechanism, 21-double head bolt, 22-wall connecting nut, 3-top cover framework, 31-top cover frame, 32-connecting bolt, 4-top cover connecting mechanism, 41-multi-section threaded screw rod, 42-top cover connecting nut, 5-fixing through hole. DETAILED DESCRIPTION

[0024] The embodiments of the present application will be described below in conjunction with the accompanying drawings and related embodiments, and the embodiments of the present application are not limited to the following embodiments, and the present application relates to the necessary components in the related technical field, which should be regarded as the known technology in the technical field, and can be known and mastered by the skilled in the art.

[0025] The utility model provides a space cabin framework fast -assembling connecting structure, including wall surface framework 1, a plurality of wall surface connecting mechanisms 2, top cover framework 3, top cover connecting mechanism 4, wall surface framework 1 is by a plurality of wall surface frame 11 sequentially spliced, and wall surface framework 1 is equipped with two and is equipped with two connecting frames 12 between two wall surface framework 1, and connecting frame 12 is located at the opposite ends of wall surface framework 1, and wall surface connecting mechanism 2 is respectively arranged between adjacent wall surface frame 11 and between connecting frame 12 and adjacent wall surface frame 11, and wall surface connecting mechanism 2 is composed of two wall surface connecting nuts 22 and double -end bolt 21 matched with each other, and top cover framework 3 is arranged at the top of two wall surface framework 1, and top cover framework 3 is by a plurality of top cover frame 31 sequentially spliced, and top cover connecting mechanism 4 is composed of a plurality of top cover connecting nuts 42 and multi -segment screw rod 41 matched with each other, and multi -segment screw rod 41 is from the top cover frame 31 of one end of top cover framework 3 and penetrates to the top cover framework 3 of the other end.

[0026] Referring to Figure 1 、 Figure 2 、 Figure 3 , the utility model mainly is as the framework structure inside civil space cabin, wherein, wall surface framework 1 is the framework structure in the length direction side wall of civil space cabin, and the outline of wall surface framework 1 is rectangular, and wall surface frame 11 and connecting frame 12 preferably adopt section steel as raw material and are welded, and the shape of wall surface frame 11 is square or rectangular, and wall surface framework 1 is formed by sequentially splicing a plurality of wall surface frame 11 along a straight line, and adjacent wall surface frame 11 is fixed through wall surface connecting mechanism 2, so that the wall surface framework 1 with firm structure is obtained, and two wall surface framework 1 is distributed as the framework structure in the length direction two side walls of civil space cabin, and the end of two wall surface framework 1 is fixed through connecting frame 12 and wall surface connecting mechanism 2, so that two wall surface framework 1 and two connecting frames 12 form the outline of cuboid and are as the internal framework structure of four side walls of civil space cabin, and wall surface framework 1 is used for fixing the wall body board, door and window of four side walls of civil space cabin and other structures.

[0027] In addition, top cover frame 31 preferably adopts section steel as raw material and is welded, and the shape of top cover frame 31 is square or rectangular, and top cover framework 3 is formed by sequentially splicing a plurality of top cover frame 31 along a straight line and is fixed through top cover connecting mechanism 4, and the fixed top cover framework 3 is erected on the top of wall surface framework 1, and the roof, ventilation system and other structures of the top of civil space cabin are fixed through top cover framework 3, and after wall surface framework 1 is fixed on the surface of the base of civil space cabin, civil space cabin can be assembled.

[0028] After adopting the above structure, it needs to be further explained that referring to Figure 1 、 Figure 2 、 Figure 3 、 Figure 4 、 Figure 5The two ends of the stud bolt 21 respectively penetrate through two adjacent wall surface frames 11 or the adjacent connecting frame 12 and the wall surface frame 11, and the two ends of the stud bolt 21 are respectively provided with a first thread matched with the wall connecting nut 22; the adjacent wall surface frames 11 and the adjacent connecting frame 12 and the wall surface frame 11 are respectively provided with a mounting hole matched with each other and allowing the stud bolt 21 to be inserted, after the stud bolt 21 is inserted into the mounting hole, the two wall connecting nuts 22 are respectively screwed inward from the threads at the two ends of the stud bolt 21, and during the screwing of the wall connecting nuts 22, the two wall connecting nuts 22 respectively abut against the surfaces of the two adjacent wall surface frames 11 or the adjacent connecting frame 12 and the wall surface frame 11, so that the wall surface frames 11 are sequentially fixed into the wall skeleton 1 through the wall connecting mechanism 2, and the two wall skeletons 1 and the two connecting frames 12 are fixed into the side wall skeleton structure of the civil space cabin through the wall connecting mechanism 2, the connecting and fixing mode of the side wall skeleton structure is simple and fast, the wall surface frames 11 and the two connecting frames 12 can be quickly connected and fixed into the side wall skeleton structure of the civil space cabin after being spliced, and the wall connecting mechanism 2 can also enable the side wall skeleton structure to be quickly disassembled, thereby improving the convenience of disassembling and transferring the civil space cabin.

[0029] After the above structure is adopted, it is further needed to be explained that, referring to Figure 1 、 Figure 3 、 Figure 6 、 Figure 7 The multi-section threaded screw rod 41 is provided with a second thread matched with the top cover connecting nut 42 between the adjacent top cover frames 31, each second thread surface is sleeved with two top cover connecting nuts 42, and the two top cover connecting nuts 42 respectively abut against the surfaces of the two adjacent top cover frames 31; the surface of the top cover frame 31 penetrates a mounting hole matched with each other and allowing the multi-section threaded screw rod 41 to be inserted, and the surface of the multi-section threaded screw rod 41 is provided with a plurality of threads matched with the top cover connecting nut 42, the multi-section threaded screw rod 41 is inserted into the mounting hole of the top cover frame 31, and the top cover connecting nut 42 is sleeved on the surface of the multi-section threaded screw rod 41 at the same time, the threads on the surface of the multi-section threaded screw rod 41 are located at the intersection of the adjacent top cover frames 31, and each two adjacent top cover frames 31 are fixed through the two top cover connecting nuts 42 at each thread, so that the top cover frames 31 are connected and fixed into the top cover skeleton 3 through the top cover connecting mechanism 4, and the top cover connecting mechanism 4 enables the top cover skeleton 3 to be quickly installed or disassembled, thereby improving the convenience of installing or disassembling and transferring the civil space cabin.

[0030] As one of the preferred embodiments of the utility model, referring to Figure 8 、 Figure 9The wall surface framework 1 is provided with a plurality of connecting slots 13 at the top, and the top cover framework 3 is provided with a plurality of connecting plugs 32 matched with the connecting slots 13, and the connecting slots 13 and the connecting plugs 32 are penetrated by the mutually matched fixing through holes 5; the wall surface framework 1 and the top cover framework 3 are connected and fixed through the connecting slots 13 and the connecting plugs 32, after the wall surface framework 1 and the top cover framework 3 are installed and fixed, the top cover framework 3 is inserted into the connecting slots 13 through the connecting plugs 32, so that the top cover framework 3 is erected on the top of the wall surface framework 1, and then the connecting plugs 32 and the connecting slots 13 are fixed through the fixing through holes 5 by means of fixing bolts, nuts and the like, so as to realize the fixation of the wall surface framework 1 and the top cover framework 3, and the mutual connection and fixation of the wall surface framework 1 and the top cover framework 3 is simple and fast, and the convenience of installation or disassembly of the internal framework structure of the civil space cabin can be improved.

[0031] As one of the preferred embodiments of the utility model, referring to Figure 1 The top cover framework 31 at both ends of the top cover framework 3 is erected on the top of the connecting frame 12 and the wall surface frame 11 adjacent to the connecting frame 12, and the remaining top cover frames 31 are erected on the top of two adjacent wall surface frames 11; after the above structure is adopted, one top cover frame 31 is fixed with two wall surface frames 11, or one top cover frame 31 is fixed with the adjacent connecting frame 12 and wall surface frame 11, so that the gap between the top cover frames 31 and the gap between the wall surface frames 11 or the gap between the wall surface frames 11 and the connecting frames 12 are staggered, and the structural stability of the internal framework of the civil space cabin is improved.

[0032] In summary, the utility model is composed of the wall surface framework 1 and the top cover framework 3, has good structural stability, the wall surface framework 1 is composed of a plurality of wall surface frames 11 and connecting frames 12 and is spliced through the wall surface connecting mechanism 2, the top cover framework 3 is composed of a plurality of top cover frames 31 and is spliced through the top cover connecting mechanism 4 in turn, the wall surface framework 1 can be quickly assembled or disassembled through the wall surface connecting mechanism 2, and the top cover framework 3 can also be quickly assembled or disassembled through the top cover connecting mechanism 4, so that the efficiency of the assembly or disassembly of the internal framework of the space cabin is improved.

[0033] The above only describes the preferred embodiments of the utility model, and it should be noted that, for ordinary technical personnel in the technical field, some improvements and refinements can be made without departing from the principles of the utility model, and these improvements and refinements should also be regarded as the protection range of the utility model.

Claims

1. A quick-assembly connection structure for a space capsule frame, comprising a wall frame (1), several sets of wall connection mechanisms (2), a top cover frame (3), and a top cover connection mechanism (4), characterized in that, The wall frame (1) is composed of several wall frames (11) spliced ​​together in sequence. There are two wall frames (1) and two connecting frames (12) are provided between the two wall frames (1). The connecting frames (12) are located at opposite ends of the wall frames (1). The wall connection mechanism (2) is located between adjacent wall frames (11) and between the connecting frame (12) and adjacent wall frames (11). The wall connection mechanism (2) is composed of matching double-headed bolts (21) and two wall connection nuts (22). The top cover frame (3) is located on top of the two wall frames (1). The top cover frame (3) is formed by splicing together several top cover frames (31) in sequence. The top cover connecting mechanism (4) is composed of a multi-segment threaded screw (41) that matches each other and several top cover connecting nuts (42). The multi-segment threaded screw (41) passes through the top cover frame (31) at one end of the top cover frame (3) to the top cover frame (3) at the other end.

2. The quick-assembly connection structure for the space capsule frame according to claim 1, characterized in that, The two ends of the double-ended bolt (21) pass through two adjacent wall frames (11) or adjacent connecting frames (12) and wall frames (11), and both ends of the double-ended bolt (21) are provided with a first thread that matches the wall connecting nut (22).

3. The quick-assembly connection structure for the space capsule frame according to claim 1, characterized in that, The multi-segment threaded screw (41) has a second thread that matches the top cover connecting nut (42) between adjacent top cover frames (31). Each second thread surface is fitted with two top cover connecting nuts (42), and the two top cover connecting nuts (42) respectively abut against the surfaces of two adjacent top cover frames (31).

4. The quick-assembly connection structure for the space capsule frame according to claim 1, characterized in that, The top of the wall frame (1) is provided with several connecting slots (13), and the bottom of the top cover frame (3) is provided with several connecting pins (32) that match the connecting slots (13). The connecting slots (13) and the connecting pins (32) are connected by matching fixing holes (5).

5. The quick-assembly connection structure for the space capsule frame according to claim 1, characterized in that, The top cover frames (31) at both ends of the top cover frame (3) are mounted on the top of the connecting frame (12) and the wall frame (11) adjacent to the connecting frame (12), and the remaining top cover frames (31) are mounted on the top of the two adjacent wall frames (11).

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