A folding and folding method for a space inflatable deployment structure

Through the processes of energizing heating, flattening exhaust, flip folding and power outage, combined with the pressing roller, flip flat plate and folding mechanism, the problem of difficult state conversion of the space inflatable expansion structure during the ground test stage is solved, efficient folding and multiple state conversions are achieved, and operation efficiency is improved.

CN114715433BActive Publication Date: 2025-04-01AEROSPACE SCI & IND SPACE ENG DEV CO LTD
View PDF 3 Cites 0 Cited by

Patent Information

Application Number
CN202210212805.7
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2022-03-04
Publication Date
2025-04-01
Estimated Expiration
2042-03-04

AI Technical Summary

Technical Problem

The prior art is difficult to effectively realize multiple state transitions of the space inflatable expansion structure during the ground testing stage, resulting in long operation time and low efficiency.

Method used

The structure is softened by power-on heating, then flattened exhaust gas is used to make it flat, then flip and fold it so that it reaches a folding and closing state, and finally power is cut off. This method combines operating devices such as pressing rollers, flip plates and folding mechanisms to achieve efficient folding and closing of the structure.

Benefits of technology

The multiple conversions of the space inflatable expansion structure between softening, folding and unfolding and curing states are realized, saving operating time and improving working efficiency.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN114715433B_ABST
    Figure CN114715433B_ABST
Patent Text Reader

Abstract

The present invention provides a folding and folding method for a space inflatable deployment structure, comprising: applying electricity to heat the space inflatable deployment structure so that the space inflatable deployment structure is in a softened state; flattening and exhausting the space inflatable deployment structure in a softened state so that the space inflatable deployment structure is in a flat state; flipping and folding the space inflatable deployment structure in a flat state so that the space inflatable deployment structure is in a folded and folded state; and powering off the space inflatable deployment structure in a folded and folded state. The method can realize the folding and folding of the space inflatable deployment structure, meet the state conversion requirements of the space inflatable deployment structure in the ground test stage, and has the characteristics of reasonable method and strong feasibility.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The present invention relates to the field of aerospace technology, and more specifically to a folding and stowing method for a space inflatable deployment structure. Background Art

[0002] In recent years, the aerospace industry has been booming. Space inflatable deployable structures have been gradually applied to the construction of large solar wings, deployable antennas and space capsules due to their advantages of small folded volume, light weight and low cost. Space inflatable deployable structures can use heating to soften and solidify the flexible materials inside the structure, and control the power on and off to switch the structure between the softened and solidified states, thereby meeting the requirements of foldable structure when softened and high rigidity when solidified.

[0003] The space inflatable deployable structure needs to be tested multiple times during the ground verification phase, requiring the structure to be converted multiple times between the softened folded state and the unfolded solidified state. In order to meet the state conversion requirements of the space inflatable deployable structure during the ground testing phase, a simple, reasonable, and operable folding and collapsing method needs to be proposed. Summary of the invention

[0004] In view of the above problems, the present invention provides a folding and stowing method for a space inflatable deployment structure, which can achieve the folding and stowing of the space inflatable deployment structure and has the characteristics of reasonable method and strong feasibility.

[0005] To achieve the above object, the present invention adopts the following technical solutions:

[0006] The present invention provides a folding and collapsing method for a space inflatable deployment structure, comprising:

[0007] The space inflatable deployment structure is electrically heated so that the space inflatable deployment structure is in a softened state;

[0008] The space inflatable deployment structure in a softened state is flattened and exhausted so that the space inflatable deployment structure is in a flat state;

[0009] The space inflatable deployment structure in a flat state is flipped and folded so that the space inflatable deployment structure is in a folded and collapsed state;

[0010] The power supply to the space inflatable deployment structure in the folded and stowed state is cut off.

[0011] In addition, the preferred solution is that flattening and exhausting the softened space inflatable expansion structure to make the space inflatable expansion structure flat further includes: flattening the surface of the softened space inflatable expansion structure by a pressure roller and rolling it along the extension direction of the space inflatable expansion structure.

[0012] In addition, a preferred solution is that a buffer layer is provided on the surface of the pressure roller that contacts the space inflatable expansion structure.

[0013] In addition, a preferred solution is that flattening and exhausting the space inflatable expansion structure in a softened state so that the space inflatable expansion structure is in a flat state further includes: flattening and rolling the space inflatable expansion structure in a softened state on both sides by a pair of rollers.

[0014] In addition, a preferred solution is that the space inflatable expansion structure can move relative to a pair of rollers along the extension direction of the space inflatable expansion structure, and the pair of rollers includes two oppositely arranged cylindrical rollers; the space inflatable expansion structure is located between the two cylindrical rollers; the two cylindrical rollers are configured to be able to approach or move away from each other, so that the space inflatable expansion structure can be crimped between the two cylindrical rollers.

[0015] In addition, a preferred solution is that flipping and folding the flattened space inflatable expansion structure so that the space inflatable expansion structure is in a folded and retracted state further includes: positioning the space inflatable expansion structure by a flipping plate and then flipping and folding it.

[0016] In addition, a preferred solution is that positioning pins are provided on the flip flat plate, and the flip flat plate can position the space inflatable expansion structure through the positioning pins.

[0017] In addition, a preferred solution is that flipping and folding the space-inflatable expansion structure in a flat state so that the space-inflatable expansion structure is in a folded and retracted state further includes: flipping and folding the space-inflatable expansion structure by a folding mechanism.

[0018] In addition, a preferred solution is that the folding mechanism includes two oppositely arranged guide plates, a two-dimensional mobile platform and a lever configured on the two-dimensional mobile platform; the space inflatable expansion structure is located between the two guide plates and can move along the extension direction of the space inflatable expansion structure; the lever is configured to flip, fold and press the part of the space inflatable expansion structure that moves from between the two guide plates to outside the two guide plates under the drive of the two-dimensional mobile platform.

[0019] In addition, a preferred solution is that electrically heating the space inflatable expansion structure so that the space inflatable expansion structure is in a softened state further includes: electrically connecting a power source to the space inflatable expansion structure, and electrically heating the space inflatable expansion structure by supplying power to the power source.

[0020] The beneficial effects of the present invention are:

[0021] The folding and gathering method provided by the present invention realizes the folding and gathering function of the space inflatable deployment structure through power-on heating, flattening and exhausting, flipping and folding, and power-off processes in conjunction with corresponding operating devices. The method is reasonable and highly feasible, so that the space inflatable deployment structure can be converted multiple times between the softened folded state and the expanded and solidified state, meeting the state conversion requirements of the space inflatable deployment structure in the ground testing stage, saving operation time and improving work efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] The specific implementation modes of the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0023] Figure 1 It is a flow chart of the folding and gathering method of the present invention.

[0024] Figure 2 It is a schematic diagram of the space inflatable expansion structure in an expanded and solidified state.

[0025] Figure 3 It is one of the schematic diagrams of flattening, exhausting and flipping and folding of the present invention.

[0026] Figure 4 yes Figure 3 Schematic diagram of the pressure roller performing flattening and exhausting as shown in FIG.

[0027] Figure 5 yes Figure 4 Schematic diagram of the cross section of the press roller shown in .

[0028] Figure 6 yes Figure 3 Schematic diagram of flipping the flat plate for flipping and folding as shown in .

[0029] Figure 7 yes Figure 6 Schematic diagram of the structure of the flip plate shown in .

[0030] Figure 8 This is the second schematic diagram of the flattening, exhausting and flipping and folding of the present invention.

[0031] Fig. 9 yes Figure 8 The assembly diagram of the two-dimensional mobile platform and the lever is shown in .

[0032] Fig.10 This is the third schematic diagram of the flattening, exhausting and flipping and folding of the present invention.

[0033] Fig.11 This is the fourth schematic diagram of the flattening, exhausting and flipping and folding of the present invention.

[0034] Fig.12 It is a schematic diagram of the space inflatable expansion structure in a folded and collapsed state. DETAILED DESCRIPTION

[0035] Various exemplary embodiments of the present invention will now be described in detail with reference to the accompanying drawings. It should be noted that the relative arrangement of components and steps, numerical expressions and numerical values ​​set forth in these embodiments do not limit the scope of the present invention unless otherwise specifically stated.

[0036] The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses.

[0037] Techniques and equipment known to ordinary technicians in the relevant art may not be discussed in detail, but where appropriate, the techniques and equipment should be considered part of the specification.

[0038] In all examples shown and discussed herein, any specific values ​​should be interpreted as merely exemplary and not limiting. Therefore, other examples of the exemplary embodiments may have different values.

[0039] It should be noted that like reference numerals and letters refer to similar items in the following figures, and therefore, once an item is defined in one figure, it need not be further discussed in subsequent figures.

[0040] In order to realize the folding and stowing of the space inflatable deployment structure and meet the state conversion requirements of the space inflatable deployment structure during the ground test phase. The present invention provides a folding and stowing method for a space inflatable deployment structure, combined with Figures 1 to 12 As shown, the specific folding and collapsing method for the space inflatable expansion structure includes: electrically heating the space inflatable expansion structure 6 so that the space inflatable expansion structure 6 is in a softened state; further, electrically connecting a power source to the space inflatable expansion structure 6, and electrically heating the space inflatable expansion structure 6 by supplying power to the power source.

[0041] Combination Figure 2 , Figure 3 and Figure 8 As shown, the space inflatable expansion structure 6 in a softened state is flattened and exhausted so that the space inflatable expansion structure 6 is in a flat state; specifically, the flattening and exhausting process is to use a pressure roller 1 to manually flatten and roll the surface of the product or to use a roller device 3 to automatically flatten and roll both sides of the product.

[0042] In an alternative embodiment, referring to Figure 3 , Figure 4 and Figure 5 As shown, a pressure roller 1 is used to flatten the surface of the space inflatable expansion structure 6 in a softened state and roll along the extension direction of the space inflatable expansion structure 6. Furthermore, a buffer layer 11 is provided on the surface of the pressure roller 1 that contacts the space inflatable expansion structure 6.

[0043] In another alternative embodiment, referring to Figure 8 , Fig.10 and Fig.11 As shown, the space inflatable expansion structure 6 in a softened state is flattened and rolled on both sides by the roller device 3. The space inflatable expansion structure 6 can move relative to the roller device 3 along the extension direction of the space inflatable expansion structure 6. The roller device 3 includes two cylindrical rollers 31 arranged opposite to each other; the space inflatable expansion structure 6 is located between the two cylindrical rollers 31; the two cylindrical rollers 31 are configured to be able to approach or move away from each other, so that the space inflatable expansion structure 6 can be pressed between the two cylindrical rollers 31, refer to Fig.11 As shown, the arrow in the figure points to the direction of movement of the two cylindrical rollers 31 in a horizontal plane when they move away from each other in a direction perpendicular to the extension direction of the space inflatable expansion structure 6. When the space inflatable expansion structure 6 is crimped between the two cylindrical rollers 31, the space inflatable expansion structure 6 starts to move, driving the two cylindrical rollers 31 to roll and flatten the space inflatable expansion structure 6.

[0044] Combination Figure 6-Figure 11 As shown, the space inflatable expansion structure 6 in a flat state is flipped and folded so that the space inflatable expansion structure 6 is in a folded and gathered state; the flipping and folding process is to manually position the flattened product according to a certain size through the flipping plate 2 and then manually flip and fold it, or to automatically flip and fold the flattened product according to a certain size requirement through the folding mechanism 4.

[0045] In an alternative embodiment, referring to Figure 6 , Figure 7 As shown, the space inflatable expansion structure 6 is positioned by a flip plate 2 and then flipped and folded. The flip plate 2 is provided with positioning pins 21, and positioning holes are provided on both side edges of the space inflatable expansion structure 6. The flip plate 2 can position the space inflatable expansion structure 6 through the positioning pins 21.

[0046] In another alternative embodiment, referring to Figure 8-Figure 11As shown, the space inflatable expansion structure 6 is flipped and folded by a folding mechanism 4. Specifically, the folding mechanism 4 includes two oppositely arranged guide plates 5, a two-dimensional mobile platform 42 and a lever 41 configured on the two-dimensional mobile platform 42; the space inflatable expansion structure 6 is located between the two guide plates 5 and can move along the extension direction of the space inflatable expansion structure 6; the lever 41 is configured to flip, fold and press the part of the space inflatable expansion structure 6 that moves from between the two guide plates 5 to outside the two guide plates 5 under the drive of the two-dimensional mobile platform 42. It can be understood that the two guide plates 5 are fixed relative to the space inflatable expansion structure 6, and the two guide plates 5 can be fixed to other components through a support member (not shown in the figure). Through the above arrangement, the two-dimensional mobile platform 42 is used to drive the lever 41 to move, so that the part of the space inflatable expansion structure 6 located on the right side of the guide plate 5 is folded counterclockwise and pressed against the outer surface of the guide plate 5, and the space inflatable expansion structure 6 moves to the right for a certain distance, and the lever 41 is reset. The two-dimensional mobile platform 42 is used to drive the lever 41 to move, so that the part of the space inflatable expansion structure 6 located on the right side of the guide plate 5 is folded clockwise and pressed against the outer surface of the guide plate 5, and this cycle is repeated until the entire space inflatable expansion structure 6 is flipped and folded, and the space inflatable expansion structure 6 is in a folded and retracted state.

[0047] The space inflatable deployment structure 6 in the folded and collapsed state is powered off, and further, the space inflatable deployment structure 6 is powered off by power cut-off.

[0048] In actual use, the initial state of the space inflatable expansion structure 6 is the expansion and solidification state. Figure 1 As shown; at this time, the power is turned on to heat the space inflatable expansion structure 6. After a period of time, the space inflatable expansion structure 6 begins to soften; at this time, the pressure roller 1 or the roller device 3 is used to flatten and exhaust the space inflatable expansion structure 6, so that the space inflatable expansion structure 6 is flattened, as shown. Figure 3 , Figure 8 After the space inflatable expansion structure 6 is flattened and exhausted, the product is flipped and folded using the flip plate 2 or the folding mechanism 4 so that the product is in a folded and collapsed state, such as Fig.11 Turn off the power to cut off the power, take out the space inflatable expansion structure 6 in the folded state, as shown Fig.12 shown.

[0049] To sum up, the folding and gathering method provided by the present invention realizes the folding and gathering function of the space inflatable deployment structure through power-on heating, flattening and exhausting, flipping and folding, and power-off processes in conjunction with corresponding operating devices (such as the pressure roller, flipping plate, roller device and folding mechanism in the above-mentioned embodiment). It has the characteristics of reasonable method and strong feasibility, so that the space inflatable deployment structure can be converted multiple times between the softened folded state and the unfolded and solidified state, meeting the state conversion requirements of the space inflatable deployment structure during the ground testing stage, saving operation time and improving work efficiency.

[0050] Obviously, the above embodiments of the present invention are merely examples for clearly illustrating the present invention, and are not limitations on the implementation methods of the present invention. For ordinary technicians in the relevant field, other different forms of changes or modifications can be made based on the above description. It is impossible to list all the implementation methods here. All obvious changes or modifications derived from the technical solution of the present invention are still within the protection scope of the present invention.

Claims

1. A folding and collapsing method for a space inflatable deployment structure, characterized in that: include: The space inflatable deployment structure is electrically heated so that the space inflatable deployment structure is in a softened state; The space inflatable deployment structure in a softened state is flattened and exhausted so that the space inflatable deployment structure is in a flat state; The space inflatable deployment structure in a flat state is flipped and folded so that the space inflatable deployment structure is in a folded and collapsed state; Cutting off power to the space inflatable deployment structure in a folded and stowed state; Flattening and exhausting the space inflatable deployment structure in a softened state so that the space inflatable deployment structure is in a flat state further includes: flattening the surface of the space inflatable deployment structure in a softened state by a pressure roller and rolling it along the extension direction of the space inflatable deployment structure; The surface of the pressure roller in contact with the space inflation expansion structure is provided with a buffer layer; Flipping and folding the space inflatable deployment structure in a flat state so that the space inflatable deployment structure is in a folded and collapsed state further includes: flipping and folding the space inflatable deployment structure by a folding mechanism; The folding mechanism includes two oppositely arranged guide plates, a two-dimensional mobile platform and a lever configured on the two-dimensional mobile platform; the space inflatable expansion structure is located between the two guide plates and can move along the extension direction of the space inflatable expansion structure; the lever is configured to flip, fold and press the part of the space inflatable expansion structure that moves from between the two guide plates to outside the two guide plates under the drive of the two-dimensional mobile platform.

2. The folding and stowing method for a space inflatable deployment structure according to claim 1, characterized in that: Flattening and exhausting the softened space inflatable deployment structure to make the space inflatable deployment structure flat further includes: flattening and rolling the softened space inflatable deployment structure on both sides by a pair of rollers.

3. The folding and stowing method for a space inflatable deployment structure according to claim 2, characterized in that: The space inflatable expansion structure can move relative to the pair of rollers along the extension direction of the space inflatable expansion structure, and the pair of rollers includes two oppositely arranged cylindrical rollers; the space inflatable expansion structure is located between the two cylindrical rollers; the two cylindrical rollers are configured to be able to approach each other or move away from each other so that the space inflatable expansion structure can be crimped between the two cylindrical rollers.

4. The folding and stowing method for a space inflatable deployment structure according to claim 1, characterized in that: Flipping and folding the space-inflatable expansion structure in a flat state so that the space-inflatable expansion structure is in a folded and retracted state further includes: positioning the space-inflatable expansion structure by a flipping plate and then flipping and folding it.

5. The folding and stowing method for a space inflatable deployment structure according to claim 4, characterized in that: The flip flat plate is provided with positioning pins, and the flip flat plate can position the space inflation deployment structure through the positioning pins.

6. The folding and stowing method for a space inflatable deployment structure according to claim 1, characterized in that: Electrically heating the space-inflatable deployment structure so that the space-inflatable deployment structure is in a softened state further includes: electrically connecting a power source to the space-inflatable deployment structure, and electrically heating the space-inflatable deployment structure by supplying power to the power source.

Citation Information

Patent Citations

  • Folding machine with pressing device

    CN102060207A

  • Space film facility retraction and deployment support tube

    CN105474780B

  • Manufacturing method of solar sail capable of being unfolded controllably and orderly based on shape memory polymers

    CN105480436A