Wing assembly and appearance modeling clothes
By designing a quadrilateral linkage mechanism and drive unit, the problem of loose wing assembly folding was solved, achieving compact folding and coordinated unfolding of the wings, thus improving the simulation effect.
Patent Information
- Application Number
- CN202520488876.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-18
- Publication Date
- 2026-02-27
- Estimated Expiration
- 2035-03-18
AI Technical Summary
The existing wing components are prone to loosening when folded, take up a lot of space, and are not coordinated when unfolding and folding.
The design employs a quadrilateral linkage mechanism, which drives the linkage between the push rod and the wing rod through a drive unit to move the wings closer or further apart in the left and right directions. Combined with an electric cylinder and slide rail structure, it ensures synchronous movement, and is equipped with a cover and support rods to enhance the simulation effect.
The wings are more compact when folded, taking up less space, and have a longer wingspan when unfolded, resulting in coordinated and more realistic movements.
Smart Images

Figure CN223943851U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to performance costume technical field, especially in wing assembly and appearance modelling costume. BACKGROUND
[0002] Part of the role playing clothes has the wing, in order to improve lively, realistic effect, most of the prior art is the structure that part imitates the wing joint of bird class to be made, to imitate the wing, and the display of wing is quite limited.
[0003] And most wing assembly of prior art has the wing unfolding, but some have the wing that cannot be folded, or there is the problem that after folding, it is still relatively loose, and occupies larger space. INVENTION CONTENTS
[0004] The utility model discloses a wing assembly and appearance modelling costume, to improve the problem of wing assembly folding loose.
[0005] To achieve the above object, the utility model provides a wing assembly, which comprises a main body, an unfolding assembly and a driving unit, the unfolding assembly is arranged on one side of the main body in the left-right direction, the unfolding assembly comprises a push rod, a wing rod and a plurality of connecting rods, the plurality of connecting rods are arranged between the push rod and the wing rod to form at least one quadrilateral connecting rod mechanism, the driving unit is installed on the main body and is in driving connection with the push rod to enable the wing rod and the plurality of connecting rods to have an activity stroke of approaching or moving away from the main body in the left-right direction.
[0006] In an embodiment, the unfolding assembly comprises:
[0007] A first connecting rod is rotatably installed at one end on the main body.
[0008] A second connecting rod is arranged opposite to the first connecting rod.
[0009] A third connecting rod is rotatably connected to the first connecting rod and the second connecting rod respectively.
[0010] The push rod is rotatably connected at one end to the first connecting rod and coaxially rotatably installed at the other end on the driving unit.
[0011] A fourth connecting rod is arranged opposite to the third connecting rod and rotatably connected to the first connecting rod and the second connecting rod respectively.
[0012] The wing rod is rotatably connected with the third connecting rod and the fourth connecting rod respectively, and is arranged opposite to the second connecting rod, and the second connecting rod, the third connecting rod, the fourth connecting rod and the wing rod constitute a second quadrilateral connecting rod mechanism.
[0013] In an embodiment, the distance between the intersection of the push rod and the first connecting rod and the intersection of the push rod and the second connecting rod is L ab ;
[0014] The distance between the intersection of the third connecting rod and the first connecting rod and the intersection of the third connecting rod and the second connecting rod is L cd ;
[0015] The distance between the intersection of the fourth connecting rod and the first connecting rod and the intersection of the fourth connecting rod and the second connecting rod is L ef ;
[0016] The distance between the intersection of the first connecting rod and the third connecting rod and the intersection of the first connecting rod and the fourth connecting rod is L ce ;
[0017] The distance between the intersection of the second connecting rod and the third connecting rod and the intersection of the second connecting rod and the fourth connecting rod is L df ;
[0018] The distance between the intersection of the wing rod and the third connecting rod and the intersection of the wing rod and the fourth connecting rod is L gh ;
[0019] Wherein, L ab >L cd , L ab >L ef , L ce >L gh , L df >L gh .
[0020] In an embodiment, the unfolding assembly is provided with two groups, which are arranged on the left and right sides of the main body respectively; the driving unit is drivingly connected with the push rods of the two groups of unfolding assemblies respectively.
[0021] In an embodiment, the driving unit comprises:
[0022] An electric cylinder extends in the up-down direction, is fixedly installed on the main body, and has a connecting portion movably arranged in the up-down direction;
[0023] The ends of the two push rods away from the first connecting rod are rotatably installed on the connecting portion, and the end of the second connecting rod close to the push rod is rotatably installed on the connecting portion.
[0024] In one embodiment, the main body has a slide rail extending in the vertical direction, and the connecting portion is slidably connected to the slide rail.
[0025] In one embodiment, the deployment assembly includes a plurality of support rods, a third connecting rod and a fourth connecting rod, for rotatably mounting one end of each support rod, and the plurality of support rods are spaced apart along the extension direction of the fourth connecting rod.
[0026] In one embodiment, the wing assembly further includes a cover fabric, which is fixedly connected to the main body, the first connecting rod, the fourth connecting rod, the wing rod, and the plurality of the support rods.
[0027] In one embodiment, the wing assembly further includes a shoulder strap disposed on the body.
[0028] This utility model also proposes an appearance-designed garment, including a wing assembly. The wing assembly includes a main body, a deployment assembly, and a drive unit. The deployment assembly includes a push rod, a wing rod, and multiple connecting rods. The multiple connecting rods are disposed between the push rod and the wing rod to form at least one quadrilateral linkage mechanism. The drive unit is installed on the main body and is drivenly connected to the push rod, so that the wing rod and the multiple connecting rods have a range of motion that moves towards or away from the main body in the left and right directions.
[0029] The technical solution of this utility model improves the problem of loose wings after folding by building at least one quadrilateral mechanism between the push rod and the wing rod, so that the push rod and the wing rod can be closer together when folding. Attached Figure Description
[0030] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on the structures shown in these drawings without creative effort.
[0031] Figure 1 A schematic diagram of the structure of an embodiment of the wing assembly provided by this utility model in the deployed state;
[0032] Figure 2 for Figure 1 A partial structural diagram of the middle wing assembly;
[0033] Figure 3 for Figure 1 A schematic diagram of the middle wing assembly in the folded-up state.
[0034] Explanation of icon numbers:
[0035] 100, wing assembly; 1, main body; 2, unfolding assembly; 21, push rod; 22, wing rod; 23, first connecting rod; 24, second connecting rod; 25, third connecting rod; 26, fourth connecting rod; 27, supporting rod; 3, driving unit; 31, electric cylinder; 311, connecting part.
[0036] The realization, functional features and advantages of the utility model will be further explained in combination with embodiments and with reference to the drawings. DETAILED DESCRIPTION
[0037] The technical solutions in the embodiments of the utility model will be clearly and completely described below in combination with the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor belong to the protection scope of the utility model.
[0038] It should be noted that if the embodiments of the utility model involve directional indications (such as up, down, left, right, front, back, etc.), the directional indications are only used to explain the relative position relationship, movement condition, etc. between components in a certain posture, and if the certain posture changes, the directional indications also change accordingly.
[0039] In addition, if the embodiments of the utility model involve descriptions such as "first", "second", etc., the descriptions of "first", "second", etc. are only for description purposes, and cannot be understood as indicating or implying the relative importance or implicitly indicating the number of indicated technical features. Therefore, the features limited by "first", "second" can explicitly or implicitly include at least one feature. In addition, "and / or" or "and / or" appearing throughout the text means that the three parallel schemes are included, taking "A and / or B" as an example, including A scheme, or B scheme, or A and B simultaneously meet the scheme. In addition, the technical solutions of each embodiment can be combined with each other, but it must be based on the realization of ordinary skilled in the art, when the combination of technical solutions appears contradictory or unachievable, it should be considered that the combination of technical solutions does not exist, and is not within the protection scope required by the utility model.
[0040] Moreover, most of the existing wing assemblies have the problem that the wings cannot be folded or are still loose after being folded.
[0041] The utility model provides a kind of wing assembly.
[0042] Please refer to Figures 1 to 2In an embodiment of the utility model, wing assembly 100 includes: main body 1, unfolding assembly 2 and drive unit 3, unfolding assembly 2 is set up in the left and right direction of main body 1 one side, unfolding assembly 2 includes push rod 21, wing lever 22 and multiple connecting rods, multiple connecting rods are set up between push rod 21 and wing lever 22, to form at least one quadrilateral linkage, push rod 21 is movably installed in main body 1, drive unit 3 is installed in main body 1, and is driven to be connected with push rod 21, to make wing lever 22 and multiple connecting rods have the movable stroke of approaching or moving away from main body 1 in the left and right direction.
[0043] Main body 1 provides the installation base for drive unit 3 and unfolding assembly 2, unfolding assembly 2 is set up in the left and right direction of main body 1 one side, and unfolding assembly 2 is similar to the "skeleton" of wing, and push rod 21 is the "skeleton" closest to main body 1 in the left and right direction, and wing lever 22 is the "skeleton" farthest from main body 1 in the left and right direction. At least one quadrilateral linkage is built between push rod 21 and wing lever 22 by multiple connecting rods, since the two opposite connecting rods of quadrilateral linkage can be very close, so drive unit 3 drives push rod 21 to move, to adjust the position of wing lever 22, so that wing lever 22 and multiple connecting rods approach or move away from push rod 21 in the left and right direction, since push rod 21 is connected with drive unit 3, so push rod 21 approaches the position of main body 1, therefore, wing lever 22 approaches main body 1 in the left and right direction to a greater extent, realizes that wing is folded, and makes the volume of wing assembly 100 smaller, and the degree of dispersion is smaller.
[0044] In order to make "wing" have enough wingspan and be shaped in the bending degree, and avoid that structure is too complex, so two quadrilateral linkages are built between push rod 21 and wing lever 22.
[0045] Specifically, unfolding assembly 2 includes: first connecting rod 23, second connecting rod 24, third connecting rod 25, first connecting rod 23 one end is rotatably installed in main body 1, second connecting rod 24 is oppositely arranged with first connecting rod 23, third connecting rod 25 is rotatably connected with first connecting rod 23 and second connecting rod 24 respectively, wherein, one end of push rod 21 is rotatably connected with first connecting rod 23, and the other end is coaxially rotatably installed in drive unit 3 with one end of second connecting rod 24, and third connecting rod 25 is oppositely arranged with push rod 21. So push rod 21, first connecting rod 23, second connecting rod 24, third connecting rod 25 constitute first quadrilateral linkage.
[0046] The unfolding assembly 2 further comprises a fourth connecting rod 26, which is arranged opposite to the third connecting rod 25 and is rotatably connected with the first connecting rod 23 and the second connecting rod 24 respectively; the wing rod 22 is rotatably connected with the third connecting rod 25 and the fourth connecting rod 26 and is arranged opposite to the second connecting rod 24. The second four-edge connecting rod mechanism is formed by the second connecting rod 24, the third connecting rod 25, the fourth connecting rod 26 and the wing rod 22.
[0047] In the first four-edge connecting rod mechanism, when the push rod 21 moves, the third connecting rod 25 moves correspondingly; in the second four-edge connecting rod mechanism, when the third connecting rod 25 moves, the wing rod 22 moves correspondingly and can move close to or away from the main body 1 in the left-right direction. In addition, the first four-edge connecting rod mechanism and the second four-edge connecting rod mechanism can be arranged as parallelogram connecting rod mechanisms.
[0048] In order to make the unfolding assembly 2 have a longer wingspan when unfolded and a smaller volume when folded, the connection between the connecting rods in the unfolding assembly 2 needs to meet the following requirements: the distance between the intersection of the push rod 21 and the first connecting rod 23 and the intersection of the push rod 21 and the second connecting rod 24 is L ab ; the distance between the intersection of the third connecting rod 25 and the first connecting rod 23 and the intersection of the third connecting rod 25 and the second connecting rod 24 is L cd ; the distance between the intersection of the fourth connecting rod 26 and the first connecting rod 23 and the intersection of the fourth connecting rod 26 and the second connecting rod 24 is L ef ; the distance between the intersection of the first connecting rod 23 and the third connecting rod 25 and the intersection of the first connecting rod 23 and the fourth connecting rod 26 is L ce ; the distance between the intersection of the second connecting rod 24 and the third connecting rod 25 and the intersection of the second connecting rod 24 and the fourth connecting rod 26 is L df ; the distance between the intersection of the wing rod 22 and the third connecting rod 25 and the intersection of the wing rod 22 and the fourth connecting rod 26 is L gh ; wherein L ab >L cd , L ab >L ef , L ce >L gh , L df >L gh .
[0049] Most of the existing role-playing costumes use two electric push rods 21 to drive the unfolding or folding of two wings, which causes the problem of asynchronous unfolding or folding of the two wings.
[0050] The unfolding assembly 2 is provided with two groups, which are respectively arranged on the left and right sides of the main body 1; the driving unit 3 is respectively drivingly connected with the push rods 21 of the two groups of the unfolding assembly 2. Specifically, the driving unit 3 can be provided as an electric cylinder 31, which extends along the up-down direction, is fixedly installed on the main body 1, and has a connecting part 311 which moves along the up-down direction; one end of the push rod 21 away from the first connecting rod 23 is rotatably installed on the connecting part 311, and one end of the second connecting rod 24 close to the push rod 21 is rotatably installed on the connecting part 311. The connecting part 311 moves along the up-down direction to slide one end of the push rod 21, and the other end of the push rod 21 pushes the first connecting rod 23 to rotate, so that the quadrilateral connecting rod mechanism composed of the push rod 21, the first connecting rod 23, the second connecting rod 24 and the third connecting rod 25 is deformed, and then the quadrilateral connecting rod mechanism composed of the second connecting rod 24, the third connecting rod 25, the fourth connecting rod 26 and the wing rod 22 is deformed, so as to adjust the position of the wing rod 22. Since the two push rods 21 are simultaneously driven by one driving unit 3, the unfolding assemblies 2 on the two sides are simultaneously moved.
[0051] In order to make the connecting part 311 only slide along the up-down direction, and to support the electric cylinder 31 to prevent it from being deformed by external force, the main body 1 has a slide rail which extends along the up-down direction, and the connecting part 311 is slidingly connected with the slide rail. The slide rail can be arranged in a slide groove, and the connecting part 311 is clamped in the slide groove to slide along the up-down direction.
[0052] In order to make the wing look more full, the unfolding assembly 2 includes a plurality of supporting rods 27, one end of each of the supporting rods 27 is rotatably installed on the fourth connecting rod 26 and the third connecting rod 25, and the plurality of supporting rods 27 are arranged at intervals along the extension direction of the fourth connecting rod 26.
[0053] In order to further shape the "feathers" of the "wings", a cloth is further provided, which is fixedly connected with the main body 1, the first connecting rod 23, the fourth connecting rod 26, the wing rod 22 and the plurality of supporting rods 27. Among them, the supporting rod 27 naturally droops under the action of gravity. In the above embodiment, the cloth is further fixedly connected with the fourth connecting rod 26, the wing rod 22 and the plurality of supporting rods 27. The cloth is unfolded under the pulling of the wing rod 22, so as to pull the supporting rod 27 to rotate, making the wings more lifelike. When the unfolding assembly 2 is folded, the supporting rod 27 naturally droops to make the cloth also fold.
[0054] In order to facilitate the wearing of the wing assembly 100, the wing assembly 100 further includes a shoulder strap, and both ends of the shoulder strap are fixedly arranged on the main body 1.
[0055] The utility model discloses still provide an appearance modelling dress, this appearance modelling dress includes wing assembly 100, the specific structure of wing assembly 100 refers to the above -mentioned embodiment, because the appearance modelling dress of the utility model adopts all technical schemes of all above -mentioned embodiments, therefore at least has all beneficial effects brought by the technical scheme of above -mentioned embodiment, here no longer one by one elaboration. Among them, wing assembly 100 includes: main body 1, unfolding assembly 2 and drive unit 3, unfolding assembly 2 is set up in the left and right direction one side of main body 1, unfolding assembly 2 includes push rod 21, wing lever 22 and multiple connecting rods, multiple connecting rods are set up between push rod 21 and wing lever 22, to at least form one quadrilateral connecting rod mechanism, push rod 21 is movably installed in main body 1, drive unit 3 is installed in main body 1, and is driven to be connected with push rod 21, to make wing lever 22 have the active stroke in left and right direction close or away from main body 1.
[0056] The above-mentioned is only the exemplary implementation of the utility model, and does not limit the patent range of the utility model, and all equivalent structural transformations made by the utility model specification and the drawings contents, or direct / indirect application in other related technical fields are included in the patent protection range of the utility model.
Claims
1. A wing assembly, characterized in that, include: main body; An unfolding assembly is disposed on one side of the main body in the left-right direction. The unfolding assembly includes a push rod, a wing rod, and multiple connecting rods. The multiple connecting rods are disposed between the push rod and the wing rod to form at least one quadrilateral linkage mechanism. A drive unit is mounted on the main body and driven by the push rod, so that the wing rod and the plurality of connecting rods have a travel distance that moves toward or away from the main body in the left and right directions.
2. The wing assembly as claimed in claim 1, characterized in that, The unfolding component includes: The first connecting rod is rotatably mounted to the main body at one end; The second link is positioned opposite to the first link; The third link is rotatably connected to both the first link and the second link; The push rod has one end rotatably connected to the first connecting rod, and the other end is coaxially rotatably mounted on the drive unit with one end of the second connecting rod. The first connecting rod, the second connecting rod, the third connecting rod and the push rod constitute a first quadrilateral linkage mechanism. The fourth link is disposed opposite to the third link and is rotatably connected to the first link and the second link respectively; The wing rod is rotatably connected to the third link and the fourth link respectively, and is arranged opposite to the second link. The second link, the third link, the fourth link and the wing rod constitute a second quadrilateral linkage mechanism.
3. The wing assembly as described in claim 2, characterized in that, The distance between the intersection of the push rod and the first connecting rod and the intersection of the push rod and the second connecting rod is L. ab ; The distance between the intersection of the third link and the first link and the intersection of the third link and the second link is L. cd ; The distance between the intersection of the fourth link and the first link and the intersection of the fourth link and the second link is L. ef ; The distance between the intersection of the first link and the third link and the intersection of the first link and the fourth link is L. ce ; The distance L between the intersection of the second link and the third link and the intersection of the second link and the fourth link. df ; The distance L between the intersection of the wing rod and the third link and the intersection of the wing rod and the fourth link. gh ; Among them, L ab > L cd , L ab > L ef , L ce > L gh , L df > L gh .
4. The wing assembly as claimed in claim 2, characterized in that, The unfolding components are provided in two sets, respectively located on both sides of the main body in the left and right directions; the driving unit is respectively connected to the push rods of the two sets of unfolding components.
5. The wing assembly as claimed in claim 4, characterized in that, The driving unit includes: An electric cylinder extends in the vertical direction and is fixedly installed on the main body, and has a connecting part that moves in the vertical direction; The ends of the two push rods away from the first connecting rod are rotatably mounted on the connecting part, and the end of the second connecting rod near the push rod is rotatably mounted on the connecting part.
6. The wing assembly as claimed in claim 5, characterized in that, The main body has a slide rail extending in the vertical direction, and the connecting part is slidably connected to the slide rail.
7. The wing assembly as claimed in claim 2, characterized in that, The deployment assembly includes multiple support rods, a third connecting rod, and a fourth connecting rod, which are used to rotatably mount one end of each support rod. The multiple support rods are spaced apart along the extension direction of the fourth connecting rod.
8. The wing assembly as claimed in claim 7, characterized in that, The wing assembly also includes a cover, which is fixedly connected to the main body, the first connecting rod, the fourth connecting rod, the wing rod, and the plurality of the support rods.
9. The wing assembly as claimed in claim 1, characterized in that, The wing assembly also includes shoulder straps disposed on the body.
10. A garment with a distinctive appearance, characterized in that: Includes the wing assembly as described in any one of claims 1 to 9.