Unpowered gliding shelter unfolding and folding structure

Abstract

The invention discloses an unpowered gliding square cabin unfolding and folding structure, and relates to the technical field of gliding square cabins, and the unpowered gliding square cabin unfolding and folding structure comprises a square cabin unit which comprises a machine head, a square cabin assembly arranged at one end of the machine head, and a balance empennage arranged at the other end of the square cabin assembly; the unfolding unit comprises an unfolding assembly arranged at the top of the shelter assembly and a hang glider assembly arranged on the unfolding assembly; the fixed mounting unit comprises a fixing assembly arranged on the square cabin assembly, and the gliding square cabin adopts an efficient unfolding and folding structure, so that the gliding wings can be retracted into the cabin during storage, and the space can be saved and the gliding wings can be stacked and placed conveniently. During use, the hang glider can be rapidly fixed and unfolded through simple operation, synchronous unfolding of the four wings is achieved, and the gliding stability is improved. The design simplifies the operation process, the structure is simple and efficient, the cost is low, and meanwhile the engineering application value is improved.

Description

Technical Field

[0001] The invention relates to the technical field of gliding cabins, and in particular to an unfolding and folding structure of an unpowered gliding cabin. Background Art

[0002] Today's gliding container material delivery technology is an advanced material transportation method that combines rapid aviation delivery and the long-distance gliding capability of gliding aircraft. It plays an important role in disaster relief and material delivery in remote areas.

[0003] The deployment of the existing gliding cabin wings requires manual installation and adjustment, and if the limit installation of the upper and lower wings is not good, it will be difficult to achieve the synchronous deployment of the wings on both sides. At the same time, the assembling of the gliding cabin requires professionals to install it for a long time, which makes the operation complicated. There are time requirements when using the gliding cabin, so professionals are required to assemble and fly it in a short time, which makes it easy to make assembly errors and cause damage. It is also inconvenient to store when not in use, and its use is limited. Summary of the invention

[0004] In view of the problems existing in the deployment and folding structure of the existing unpowered gliding cabin, the present invention is proposed.

[0005] Therefore, the present invention provides an unpowered gliding cabin deployment and folding structure, the purpose of which is to solve the problem that manual installation and adjustment are required, and if the limit installation of the upper and lower wings is not good, it will be difficult to achieve the synchronous deployment of the wings on both sides. At the same time, when assembling the gliding cabin, professional personnel are required to install it for a long time, which makes the operation complicated. When using the gliding cabin, there is a time requirement, so professional personnel are required to assemble and fly it in a short time, which makes it easy to make assembly errors and cause damage. It is also inconvenient to store when not in use, and its use is limited.

[0006] In order to solve the above technical problems, the present invention provides the following technical solutions: a cabin unit comprises a nose, a cabin assembly arranged at one end of the nose, and a balancing tail arranged at the other end of the cabin assembly;

[0007] an unfolding unit, comprising an unfolding assembly arranged on the top of the shelter assembly, and a glider assembly arranged on the unfolding assembly; and,

[0008] The fixed installation unit includes a fixed component arranged on the shelter component.

[0009] As a preferred solution of the unfolding and folding structure of the unpowered gliding cabin of the present invention, the cabin assembly includes a cabin body arranged at one end of the nose, a fixed top plate arranged on the top of the cabin body, and a fixed slot arranged inside the fixed top plate.

[0010] As a preferred solution of the unfolding and folding structure of the non-powered gliding cabin described in the present invention, the unfolding component includes a fixed rod arranged on the top of the fixed top plate, a compression spring arranged on the outer diameter of the fixed rod, a fixed clamping plate arranged on the top of the compression spring, a rotating sleeve arranged on the fixed clamping plate, and a limiting slide groove arranged on the rotating sleeve, and the rotating sleeve is rotatably connected to the fixed rod.

[0011] As a preferred solution of the unfolding and folding structure of the non-powered gliding cabin described in the present invention, a sliding pad sleeve is arranged on the top of the fixed clamping plate 1, a fixed clamping plate 2 is arranged on the top of the sliding pad sleeve, and the sliding pad sleeve and the fixed clamping plate 2 are both rotatably connected to the fixed rod.

[0012] As a preferred solution of the unfolding and folding structure of the non-powered gliding cabin described in the present invention, wherein: a rotating sleeve 2 is arranged inside the fixed clamping plate 2, a limiting slide groove 2 is arranged on the rotating sleeve 2, and the rotating sleeve 2 and the limiting slide groove 2 are both rotatably connected to the outer diameter of the fixed rod.

[0013] As a preferred solution of the unfolding and folding structure of the non-powered gliding cabin described in the present invention, a limiting sleeve is arranged on the top of the second fixed clamping plate, an explosive bolt is arranged on the top of the limiting sleeve, and the limiting sleeve and the explosive bolt are connected to the fixing rod.

[0014] As a preferred solution of the unfolding and folding structure of the non-powered gliding cabin described in the present invention, the outer diameter of the fixed rod is provided with a limit block 1 and a limit block 2, and the limit block 1 moves inside the limit slide groove 1, and the limit block 2 moves inside the limit slide groove 2, and a fixed circular plate is provided on the top of the fixed rod.

[0015] As a preferred solution of the unfolding and folding structure of the non-powered gliding cabin of the present invention, the glider assembly includes a glider 1 arranged on the fixed clamping plate 2, and a glider 2 arranged on the fixed clamping plate 1.

[0016] As a preferred solution of the unfolding and folding structure of the non-powered gliding cabin described in the present invention, the fixing assembly includes a rotating rod arranged inside the cabin body, a return spring arranged inside the rotating rod, and fixed blocks arranged at both ends of the return spring, and the fixed blocks cooperate with the fixed slots.

[0017] As a preferred solution of the unpowered gliding cabin deployment and folding structure of the present invention, a rotating knob is rotatably provided at the other end of the rotating rod, a fixing clamp ring is provided on the outer diameter of the rotating rod, and the fixing clamp ring is connected to the cabin body.

[0018] Beneficial effects of the present invention: The glider cabin adopts an efficient unfolding and folding structure, so that the glider can be retracted into the cabin during storage, which is convenient for saving space and stacking. When in use, the glider can be quickly fixed and unfolded through simple operations, so that the four wings can be unfolded synchronously, and the gliding stability is increased. This design simplifies the operation process, has a simple and efficient structure, low cost, and improves the engineering application value. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the following briefly introduces the drawings required for use in the description of the embodiments. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative work.

[0020] Figure 1 It is a schematic diagram of the folding structure of the unpowered gliding cabin of the present invention.

[0021] Figure 2 It is a schematic diagram of the explosion structure of the unpowered gliding cabin of the present invention when it is deployed and folded.

[0022] Figure 3 The invention provides a non-powered gliding cabin with an unfolding and folding structure. Figure 2 An enlarged schematic diagram of point A.

[0023] Figure 4 It is a schematic diagram of the top plate cross-sectional structure of the unpowered gliding cabin of the present invention when the structure is unfolded and folded.

[0024] Figure 5 It is a schematic diagram of the internal structure of the cabin of the unpowered gliding cabin of the present invention when the structure is unfolded and folded.

[0025] Figure 6 The invention provides a non-powered gliding cabin with an unfolding and folding structure. Figure 5 An enlarged schematic diagram of point B.

[0026] Figure 7 It is a schematic diagram of the overall cross-sectional structure of the unfolding and folding structure of the unpowered gliding cabin of the present invention.

[0027] Figure 8 It is a schematic diagram of the gliding structure of the unpowered gliding cabin of the present invention when the structure is unfolded and folded. DETAILED DESCRIPTION

[0028] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, the specific embodiments of the present invention are described in detail below in conjunction with the accompanying drawings.

[0029] In the following description, many specific details are set forth to facilitate a full understanding of the present invention, but the present invention may also be implemented in other ways different from those described herein, and those skilled in the art may make similar generalizations without violating the connotation of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed below.

[0030] Secondly, the term "one embodiment" or "embodiment" as used herein refers to a specific feature, structure or characteristic that may be included in at least one implementation of the present invention. The term "in one embodiment" that appears in different places in this specification does not necessarily refer to the same embodiment, nor is it an embodiment that is mutually exclusive with other embodiments, either individually or selectively.

[0031] Secondly, the present invention is described in detail with reference to the schematic diagram. When describing the embodiments of the present invention in detail, for the sake of convenience, the cross-sectional diagrams showing the device structure will not be partially enlarged according to the general scale, and the schematic diagrams are only examples, which should not limit the scope of protection of the present invention. In addition, in actual production, the three-dimensional dimensions of length, width and depth should be included.

[0032] Example 1, reference Figure 1 - Figure 2 , which is the first embodiment of the present invention, provides a structure for unfolding and folding a non-powered gliding cabin, the device comprising: a cabin unit 100, comprising a nose 102, a cabin assembly 101 arranged at one end of the nose 102, and a balancing tail 103 arranged at the other end of the cabin assembly 101, the gliding direction is fixed by the nose 102 at the front end of the cabin assembly 101, and the balancing tail 103 at the other end of the cabin assembly 101 is used to balance and stabilize the entire cabin assembly during gliding;

[0033] The unfolding unit 200 includes an unfolding assembly 201 disposed on the top of the shelter assembly 101, and a glider assembly 202 disposed on the unfolding assembly 201. The unfolding assembly 201 on the shelter assembly 101 can unfold the glider shelter wing when the shelter assembly 101 is released, so that the glider assembly 202 can be unfolded at the same time to ensure the normal gliding of the shelter assembly 101; and

[0034] The fixed installation unit 300 includes a fixed component 301 arranged on the cabin component 101. When the gliding cabin is not in use, the fixed component 301 on the cabin component 101 can be used to collect the gliding wing components 202 on the deployment component 201 into the cabin component 101, so as to facilitate the storage of the main body of the gliding cabin.

[0035] Among them, the cabin assembly 101 includes a cabin body 101a arranged at one end of the nose 102, a fixed top plate 101b arranged on the top of the cabin body 101a, and a fixed card slot 101c arranged inside the fixed top plate 101b. The cabin assembly 101 can be quickly installed and disassembled through the fixed top plate 101b on the top of the cabin body 101a and the fixed card slot 101c inside the fixed top plate 101b, so that the gliding cabin can be stored conveniently when not in use.

[0036] During use, when using the gliding cabin, the operator rotates the rotating knob 301a to rotate the rotating rod 301b and the fixed block 301d inside the cabin body 101a, so that the fixed block 301d slides out from the fixed slot 101c. After disassembling the fixing component 301, the fixed top plate 101b is reversed, and the side provided with the unfolding component 201 and the glider component 202 is set to the top, and then the fixed top plate 101b is lowered again, and the rotating knob 301a is rotated again, so that the fixed block 301d is re-engaged in the fixed slot 101c to fix the fixed top plate 101b, so that the installation is completed, so that the cabin component 101 can be quickly installed and disassembled, which is convenient for operation.

[0037] After installation is completed, the cabin assembly 101 is released, and at the same time, the explosive bolt 201q inside the glider assembly 202 is detonated, so that the compression spring 201b is released from compression and expands upward, so that the compression spring 201b can simultaneously push the rotating sleeve 1 201d and the fixed card plate 1 201c to move upward, and the rotating sleeve 2 201l and the fixed card plate 2 201h at the top of the moving rotating sleeve 1 201d also move upward at the same time, and at the same time, through the limiting of the limiting block 1 201f and the limiting block 2 201n on the fixed rod 201a, the glider assembly 202 can be simultaneously unfolded in different directions, so that the four glider cabin wings can be simultaneously unfolded, stabilizing the flight balance and flight stability of the glider, and the glider can be quickly fixed and unfolded through simple operation, so that the four wings can be synchronously unfolded, and the gliding stability is increased. This design simplifies the operation process, has a simple and efficient structure, low cost, and improves the engineering application value.

[0038] Example 2, reference Figure 1 - Figure 4, which is the second embodiment of the present invention. This embodiment is different from the first embodiment in that: the unfolding component 201 includes a fixed rod 201a arranged on the top of the fixed top plate 101b, a compression spring 201b arranged on the outer diameter of the fixed rod 201a, a fixed clamping plate 201c arranged on the top of the compression spring 201b, a rotating sleeve 201d arranged on the fixed clamping plate 201c, and a limiting slide groove 201e arranged on the rotating sleeve 201d, and the rotating sleeve 201d is rotatably connected to the fixed rod 201a. The rotating sleeve 201d can be limited and fixed by the fixed rod 201a inside the unfolding component 201, and the compression spring 201b can be supported. When the glider wing is unfolded, the fixed rod 201a supports and stabilizes the overall unfolding.

[0039] Compared with Example 1, further, a sliding pad sleeve 201g is provided on the top of the fixed card plate 1 201c, and a fixed card plate 201h is provided on the top of the sliding pad sleeve 201g, and the sliding pad sleeve 201g and the fixed card plate 2 201h are both rotatably connected to the fixed rod 201a, and the sliding pad sleeve 201g between the fixed card plate 1 201c and the fixed card plate 2 201h can make the fixed card plate 1 201c and the fixed card plate 2 201h be unfolded at the same time, and isolate and stabilize without disturbing each other.

[0040] Furthermore, a rotating sleeve 2011 is provided inside the fixed clamp plate 201h, and a limiting slide groove 201m is provided on the rotating sleeve 201l, and the rotating sleeve 201l and the limiting slide groove 201m are both rotatably connected to the outer diameter of the fixed rod 201a. The limiting slide groove 201m on the rotating sleeve 201l can limit the glider assembly 202 when the glider wing is unfolded.

[0041] Furthermore, a limiting sleeve 201o is arranged on the top of the second fixed clamping plate 201h, and an explosive bolt 201q is arranged on the top of the limiting sleeve 201o, and the limiting sleeve 201o, the explosive bolt 201q and the fixing rod 201a are connected, and the entire unfolding assembly 201 is limited by the limiting sleeve 201o, and the compression spring 201b is compressed at the same time to ensure that the compression spring 201b is always in a compressed state.

[0042] Furthermore, a limit block 201f and a limit block 201n are provided on the outer diameter of the fixed rod 201a, and the limit block 201f moves inside the limit slide 201e, and the limit block 201n moves inside the limit slide 201m. A fixed circular plate 201p is provided on the top of the fixed rod 201a. After the explosive bolt 201q causes the limit sleeve 201o to explode and fall off, the limit slide 201e and the limit slide 201m begin to be squeezed upward by the compression spring 201b, and at the same time, through the limitation of the limit block 201f and the limit block 201n, the glider wings on both sides are unfolded at the same time.

[0043] Preferably, the glider assembly 202 includes a glider 202a disposed on a fixed card plate 201h, and a glider 202b disposed on a fixed card plate 201c. The glider 202a on the glider assembly 202 and the glider 202b on the fixed card plate 201c are deployed to keep the gliding of the gliding cabin smooth and stable.

[0044] During use, when the gliding cabin is used and released, after the operator completes the installation, the gliding cabin is released, and then the fixed circular plate 201p inside the deployment assembly 201 is controlled to perform a small-scale explosion, so that the limiting sleeve 201o is shattered by the explosion. At the same time when the limiting sleeve 201o is shattered, the compression spring 201b on the fixed rod 201a loses its extrusion and begins to rebound upward. When the compression spring 201b rebounds upward, the compression spring 201b squeezes the rotating sleeve 1 201d and the rotating sleeve 2 201l and moves upward at the same time. When the rotating sleeve 1 201d and the rotating sleeve 2 201l move upward, the limiting block 1 201f and the limiting block 2 201n on the outer diameter of the fixed rod 201a are in the limit position. The slide groove 1 201e and the limiting slide groove 201m are limited, so that the rotating sleeve 1 201d and the rotating sleeve 2 201l are rotated and moved upward, and the fixed card plate 1 201c and the fixed card plate 201h are rotated at the same time. Through the rotation path of the limiting slide groove 201m and the limiting slide groove 1 201e, the rotating sleeve 1 201d and the rotating sleeve 2 201l can only rotate to both sides, and rotate to the specified stability, and are limited again by the limiting block 1 201f and the limiting block 201n, so that the glider 1 202a and the glider 2 202b on the fixed card plate 1 201c and the fixed card plate 2 201h can be unfolded to the left and right sides at the same time, so that the wings can be unfolded quickly and simultaneously, ensuring the stability and balance of the gliding cabin during the gliding process.

[0045] The deployment structure of the gliding shelter realizes the rapid and synchronous deployment of the wings through the built-in explosive release mechanism and spring drive system, which greatly improves the deployment speed and operational safety of the gliding shelter. This design not only simplifies the maintenance process and reduces production and maintenance costs, but also enhances the reliability and durability of the system. In addition, it improves the adaptability of the gliding shelter under changing environmental conditions, ensures the accuracy and balance of material delivery, and reduces the dependence on electronic or hydraulic systems, improving the environmental friendliness of the overall structure. This efficient, economical and reliable gliding shelter deployment technology provides strong support for emergency material delivery and large-scale operations.

[0046] The remaining structures are the same as those of Example 1.

[0047] Example 3, reference Figure 1 - Figure 8 , which is the third embodiment of the present invention. This embodiment is different from the second embodiment in that: the fixing component 301 includes a rotating rod 301b arranged inside the cabin body 101a, a return spring 301c arranged inside the rotating rod 301b, and fixed blocks 301d arranged at both ends of the return spring 301c, and the fixed blocks 301d cooperate with the fixed slots 101c. Through the fixing component 301 inside the cabin body 101a, the fixed top plate 101b can be quickly fixed and quickly disassembled, ensuring the rapid installation of the gliding cabin during storage and use.

[0048] Compared with Example 2, further, a rotating knob 301a is rotatably provided on the other end of the rotating rod 301b, a fixing clamp 301e is provided on the outer diameter of the rotating rod 301b, and the fixing clamp 301e is connected to the cabin body 101a. By rotating the rotating knob 301a, the rotating rod 301b and the fixing clamp 301e are rotated, thereby achieving the fixation and installation of the fixed top plate 101b.

[0049] During use, when the gliding cabin is not in use and is collected and stored, the rotating knob 301a is rotated to squeeze the rotating rod 301b with the fixed card block 301d in the fixed card slot 101c inside the fixed top plate 101b. By squeezing the fixed card block 301d, the fixed card blocks 301d on both sides are squeezed into the rotating rod 301b, and then the rotating rod 301b is stretched outward, so that the fixed top plate 101b can be quickly disassembled. After the disassembly is completed, the fixed top plate 101b is turned over to remove the expansion assembly 201 and the glider assembly 201. 02 is reversed and placed inside the cabin body 101a, and then the rotating knob 301a is rotated again, so that the rotating rod 301b with the fixed card block 301d is re-engaged in the fixed card slot 101c, and at the same time, the return spring 301c inside the rotating rod 301b makes the fixed card blocks 301d on both sides re-engage in the fixed card slot 101c, thereby completing the fixation of the fixed top plate 101b. At the same time, multiple gliding cabins can be stacked and stored, which is convenient for storage and storage. When using the gliding cabin, you only need to reinstall it in reverse to use it quickly, so as to achieve quick installation and disassembly.

[0050] The design of quick disassembly and installation of the gliding cabin significantly improves operational efficiency and storage convenience. By rotating the knob, the fixed card block can be quickly squeezed to achieve quick disassembly of the cabin, and flipping the fixed top plate and reinstalling it facilitates compact storage of the cabin. At the same time, it supports the stacking of multiple cabins to optimize space utilization. This design reduces labor intensity, reduces wear and tear during loading and unloading, extends service life, and improves maintainability and safety. It also enhances the modularity of the cabin, facilitates customization and upgrading, and improves adaptability and flexibility in changing environments and mission requirements. In addition, simplified operating procedures and low-cost maintenance also improve the user experience, making the deployment and contraction of the gliding cabin an efficient and economical solution.

[0051] The remaining structure is the same as that of Example 2.

[0052] Importantly, it should be noted that the construction and arrangement of the present application shown in a plurality of different exemplary embodiments are only exemplary. Although only a few embodiments are described in detail in this disclosure, it should be readily understood by those who refer to this disclosure that many modifications are possible (e.g., the size, scale, structure, shape and proportion of various elements, as well as parameter values ​​(e.g., temperature, pressure, etc.), mounting arrangements, use of materials, color, directional changes, etc.) without substantially departing from the novel teachings and advantages of the subject matter described in the application. For example, the element shown as integrally formed can be composed of multiple parts or elements, the position of the element can be inverted or otherwise changed, and the nature or number or position of the discrete element can be changed or changed. Therefore, all such modifications are intended to be included in the scope of the present invention. The order or sequence of any process or method steps can be changed or reordered according to alternative embodiments. In the claims, any "device plus function" clause is intended to cover the structure described herein that performs the function, and is not only structurally equivalent but also equivalent structure. Without departing from the scope of the present invention, other replacements, modifications, changes and omissions can be made in the design, operating conditions and arrangement of the exemplary embodiments. Therefore, the invention is not limited to a specific embodiment, but extends to several modifications still falling within the scope of the appended claims.

[0053] Additionally, in order to provide a concise description of exemplary embodiments, all features of an actual embodiment (ie, those features that are not relevant to the best mode presently contemplated for carrying out the invention or those that are not relevant to implementing the invention) may not be described.

[0054] It should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention rather than to limit it. Although the present invention has been described in detail with reference to the preferred embodiments, those skilled in the art should understand that the technical solutions of the present invention may be modified or replaced by equivalents without departing from the spirit and scope of the technical solutions of the present invention, which should all be included in the scope of the claims of the present invention.

Claims

1. A non-powered gliding cabin deployment and folding structure, characterized by: include: A cabin unit (100) comprises a nose (102), a cabin assembly (101) arranged at one end of the nose (102), and a balancing tail (103) arranged at the other end of the cabin assembly (101); The unfolding unit (200) comprises an unfolding assembly (201) arranged on the top of the shelter assembly (101), and a glider assembly (202) arranged on the unfolding assembly (201); and, The fixed installation unit (300) comprises a fixed assembly (301) arranged on the cabin assembly (101).

2. The unpowered gliding cabin deployment and folding structure according to claim 1 is characterized in that: The cabin assembly (101) comprises a cabin body (101a) arranged at one end of the nose (102), a fixed top plate (101b) arranged on the top of the cabin body (101a), and a fixed slot (101c) arranged inside the fixed top plate (101b).

3. The unpowered gliding cabin deployment and folding structure according to claim 2 is characterized in that: The unfolding assembly (201) comprises a fixed rod (201a) arranged on the top of the fixed top plate (101b), a compression spring (201b) arranged on the outer diameter of the fixed rod (201a), a fixed clamping plate (201c) arranged on the top of the compression spring (201b), a rotating sleeve (201d) arranged on the fixed clamping plate (201c), and a limiting sliding groove (201e) arranged on the rotating sleeve (201d), and the rotating sleeve (201d) is rotatably connected to the fixed rod (201a).

4. The unpowered gliding cabin deployment and folding structure according to claim 3 is characterized in that: A sliding pad sleeve (201g) is arranged on the top of the fixed clamping plate 1 (201c), and a fixed clamping plate 2 (201h) is arranged on the top of the sliding pad sleeve (201g), and the sliding pad sleeve (201g) and the fixed clamping plate 2 (201h) are both rotatably connected to the fixed rod (201a).

5. The unpowered gliding cabin deployment and folding structure according to claim 4 is characterized in that: A second rotating sleeve (201l) is arranged inside the second fixed clamping plate (201h), a second limiting sliding groove (201m) is arranged on the second rotating sleeve (201l), and the second rotating sleeve (201l) and the second limiting sliding groove (201m) are both rotatably connected to the outer diameter of the fixed rod (201a).

6. The unpowered gliding cabin deployment and folding structure according to claim 5 is characterized in that: A limiting sleeve (201o) is arranged on the top of the second fixed clamping plate (201h), an explosive bolt (201q) is arranged on the top of the limiting sleeve (201o), and the limiting sleeve (201o) and the explosive bolt (201q) are connected to the fixing rod (201a).

7. The unpowered gliding cabin deployment and folding structure according to claim 6 is characterized in that: The outer diameter of the fixed rod (201a) is provided with a limit block 1 (201f) and a limit block 2 (201n), and the limit block 1 (201f) moves inside the limit slide groove 1 (201e), and the limit block 2 (201n) moves inside the limit slide groove 2 (201m), and a fixed circular plate (201p) is provided on the top of the fixed rod (201a).

8. The unpowered gliding cabin deployment and folding structure according to claim 7 is characterized in that: The hang glider assembly (202) comprises a hang glider 1 (202a) arranged on the second fixing card plate (201h), and a hang glider 2 (202b) arranged on the first fixing card plate (201c).

9. The unpowered gliding cabin deployment and folding structure according to claim 8 is characterized in that: The fixing assembly (301) comprises a rotating rod (301b) arranged inside the cabin body (101a), a return spring (301c) arranged inside the rotating rod (301b), and fixed blocks (301d) arranged at both ends of the return spring (301c), and the fixed blocks (301d) cooperate with the fixed slots (101c).

10. The unpowered gliding cabin deployment and folding structure according to claim 9, characterized in that: A rotating knob (301a) is rotatably provided at the other end of the rotating rod (301b), a fixing clamp ring (301e) is provided on the outer diameter of the rotating rod (301b), and the fixing clamp ring (301e) is connected to the cabin body (101a).

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