Detachable wing structure of model airplane toy

By setting up a disassembly frame and plug-in structure in the model aircraft toy, the problem of inconvenience in disassembly and assembly of the wings is solved, stable connection and simple operation are achieved, and disassembly efficiency and aesthetic appearance are improved.

CN223248748UActive Publication Date: 2025-08-22SHANTOU HAIQU TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202521531006.1
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-07-22
Publication Date
2025-08-22
Estimated Expiration
2035-07-22

AI Technical Summary

Technical Problem

The disassembly and assembly of the toy wings of existing model aircraft aircraft is more troublesome, it is inconvenient to disassemble, and there are many auxiliary tools to use.

Method used

A detachable frame is arranged in the fuselage, and the wing and the detachable frame are connected through a plug-in structure, including a chamber, plug block, slot and cutting strip, to realize the detachable connection of the wing and hide the conductive wires through the through hole structure.

Benefits of technology

It realizes stable and firm connection of the wings, and is easy to disassemble and assembly, without additional tools, improves disassembly convenience and has a more beautiful appearance.

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Abstract

The utility model provides a detachable wing structure of a model airplane toy, which is characterized in that a detachable frame is fixed in an airplane body, the detachable frame is internally divided into two cavities, the inner wall of each cavity is raised at intervals from inside to outside to form a first insertion block and a second insertion block, and meanwhile, an insertion section of a wing is detachably connected into the cavities in a matched manner; a first inserting groove matched with the first inserting block in shape and a second inserting groove matched with the second inserting block in shape are formed in the inserting section in a concave mode, meanwhile, an inserting strip embedded in the wing is further connected into the first inserting groove in an extending mode, and the inserting strip is inserted and fixed into a first inserting hole of the first inserting block in a detachable mode. According to the detachable wing structure, a triple insertion structure consisting of the cavity, the insertion section, the insertion block, the insertion slot, the insertion strip and the first insertion hole is arranged between the detachable frame and the wing, so that the wing can be relatively stably and firmly connected to the fuselage, and meanwhile, the detachable wing structure has the advantages of simplicity, convenience and rapidness in disassembly and assembly operation.
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Description

Technical Field

[0001] The utility model relates to the technical field of model toys, in particular to a detachable wing structure of a model airplane toy. Background Art

[0002] Model airplanes are generally made of foam materials. To facilitate transportation and storage, most model airplanes are designed to be detachable. In the relevant public document with publication number CN208641746U and titled "A Detachable Fixed-Wing Model Airplane," screws are used to connect the pressure plate, wings, and bottom plate together, achieving a secure connection between the wings and the fuselage. The hatch can be opened by latches and movable latches at the front and rear ends, facilitating disassembly and internal maintenance. At the same time, a portion of the hatch presses on the wings, tightening and fixing the wings again. It can be seen that the wings in the related art are generally installed and fixed by screws and other locking parts, which is relatively cumbersome to operate and requires a large number of auxiliary tools. It is also inconvenient for users to disassemble when they want to replace parts. Therefore, we need to propose a detachable wing structure for model airplane toys to solve the above-mentioned problems. Utility Model Content

[0003] The purpose of the utility model is to provide a detachable wing structure for a model airplane toy, so as to solve the problem mentioned in the above background technology that the wing is difficult to assemble and disassemble in the prior art.

[0004] In order to achieve the above-mentioned purpose, the utility model provides a detachable wing structure of a model airplane toy, comprising a fuselage and wings detachably connected to the fuselage, a detachable frame fixedly connected to the fuselage, the detachable frame comprising an outer frame fixed in the fuselage and an inner frame fixed in the outer frame, the two sides of the outer frame are through-set and a first through hole connected to the inner cavity of the fuselage is opened at the bottom, the inner frame is separated and provided with two chambers corresponding to the two sides of the outer frame, the two chambers are connected to the first through hole respectively through a second through hole, the inner wall of each chamber is raised from the inside to the outside to form a first plug-in block and a second plug-in block, the The first plug block is provided with a first plug hole connected to the outside world, and the second plug block is provided with a second plug hole connected to the outside world and the second through hole; the wing includes an integrally formed insertion section and a wing section, the insertion section is detachably adapted to be inserted into the cavity, the insertion section is recessed with a first slot matching the shape of the first plug block and a second slot matching the shape of the second plug block, the wing section is recessed with a first groove and a second groove, the first groove is embedded with an insertion strip, the insertion strip extends into the first slot and can be removably inserted and fixed in the first plug hole, the second groove is connected to the second slot and can be connected to the second plug hole.

[0005] As a preferred solution, the height of the first inserting block is greater than the height of the second inserting block, and the height of the second inserting block is less than the depth of the second groove.

[0006] As a preferred solution, a third through hole is further provided in the inner frame. The third through hole is opened on the side wall between the two chambers opposite to the second insertion hole, and the third through hole is connected to the second through hole.

[0007] As a preferred solution, the inner frame includes a first frame and a second frame, each of the first frame and the second frame is provided with a chamber, and each side where the first frame and the second frame are connected is provided with at least one fixing part, each of the fixing parts includes a connecting column and a clearance groove arranged adjacent to each other in the vertical direction, and the connecting column of the first frame is placed in the clearance groove connected to the second frame, so that the connecting columns of the first frame and the second frame are placed on the same axis and can be fixed in the outer frame by screws.

[0008] As a preferred embodiment, a first positioning column is protruded from the side wall of the first frame toward the second frame, and a second positioning column is correspondingly provided on the side wall of the second frame for accommodating the first positioning column. The second positioning column protrudes from the cavity of the second frame and can be inserted and fixed in the insertion section in a removable manner.

[0009] As a preferred solution, fixing columns are respectively provided on both sides of the outer wall of the outer frame at positions directly opposite to the connecting columns, and countersunk holes for receiving the screws are provided in the fixing columns located on the same side of the outer frame.

[0010] As a preferred solution, an adhesion plate is further provided on the outer frame. The adhesion plate is planar and arranged around the outer periphery of the outer frame. A positioning plate is vertically arranged on the adhesion plate, and at least part of the positioning plate extends out of the fuselage.

[0011] As a preferred solution, the inner cavity of the fuselage is connected to the outside world through an inner cavity opening, and a hatch cover is adapted to be connected to the inner cavity opening. The positioning plate is exposed on one side of the inner cavity opening, and the positioning plate is connected to the hatch cover in a contacting manner. A card slot is recessed on the other side of the inner cavity opening and is detachably connected to the hatch cover.

[0012] As a preferred solution, one end of the hatch cover is provided with a card block that can be detachably plugged into the card slot, and the other end of the hatch cover is provided with an elastic U-shaped buckle, and the movable end of the elastic U-shaped buckle is provided with a limiting foot that can be abutted and connected with the positioning plate, and the movable end of the elastic U-shaped buckle can be movably extended from the hatch cover.

[0013] As a preferred embodiment, the wing section is further provided with a rudder plate and a fixing groove, the rudder plate is swingably connected to the wing section, a servo is fixedly installed in the fixing groove, the swing arm of the servo is connected to the swing rod of the rudder plate through a connecting rod, and the conductive wire of the servo can be placed in the second groove.

[0014] Therefore, according to the technical means of the present invention, the present invention can achieve at least one of the following beneficial effects: the detachable wing structure of the model airplane toy provided by the present invention is achieved by fixing a detachable frame inside the fuselage, so that two chambers are separated in the detachable frame, and the inner wall of each chamber is raised from the inside to the outside to form a first plug-in block and a second plug-in block, and at the same time, the insertion section of the wing is detachably adapted and connected to the chamber, and a first slot matching the shape of the first plug-in block and a second slot matching the shape of the second plug-in block are recessed in the insertion section, and at the same time, an insertion strip embedded in the wing is extended into the first slot, and the insertion strip can be removably inserted into the first socket fixed to the first plug-in block. In summary, the detachable wing structure provided by the present invention comprises a triple plug-in structure between the detachable frame and the wing, comprising a cavity and an insertion section, an insert block and a slot, and an insert strip and a first insertion hole. This allows the wing to be relatively stably and securely connected to the fuselage. Furthermore, the detachable wing structure provided by the present invention features a channel structure comprising a first through-hole, a second through-hole, a second insertion hole, and a second groove, disposed between the detachable frame and the wing, for connecting the wing to the interior cavity of the fuselage to facilitate concealing the conductive wires, thereby enhancing the appearance of the model aircraft toy. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 The figure is a schematic diagram of a model airplane toy according to one embodiment of the present invention.

[0016] Figure 2 for Figure 1 Schematic diagram of the exploded view of a Chinese model airplane toy.

[0017] Figure 3 for Figure 2 Exploded diagram of the disassembly frame.

[0018] Figure 4 for Figure 2 Schematic diagram of the mid-wing.

[0019] Figure 5 for Figure 1 Schematic diagram of the cross-section of a Chinese model aircraft toy in the left and right directions.

[0020] Figure 6 for Figure 1Schematic diagram of the cross-section of a model aircraft toy in the front and rear directions.

[0021] In the figure: 100 - fuselage; 110 - inner cavity; 111 - card slot; 120 - detachable frame; 121 - outer frame; 1211 - first through hole; 1212 - fixing column; 1213 - countersunk hole; 1214 - bonding plate; 1215 - positioning plate; 122 - inner frame; 1221 - first frame; 1222 - second frame; 1223 - connecting column; 1224 - clearance groove; 1225 - first positioning column; 1226 - second positioning column; 1230 - chamber; 1231 - second through hole; 1232 - first plug-in block; 1233 - second Second plug block; 1234-first plug hole; 1235-second plug hole; 1236-third through hole; 200-wing; 210-insertion section; 211-first slot; 212-second slot; 213-third slot; 214-fourth slot; 220-wing section; 221-rudder plate; 2211-rocker; 222-fixing slot; 223-first groove; 224-second groove; 230-servo; 231-rocker arm; 240-insertion strip; 300-hatch cover; 310-block; 320-elastic U-shaped buckle; 321-limiting foot. DETAILED DESCRIPTION

[0022] The preferred embodiments of the present invention will be further described in detail below with reference to the accompanying drawings.

[0023] The following describes in detail embodiments of the present invention, examples of which are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are intended to explain the present invention, and should not be construed as limiting the present invention.

[0024] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "clockwise", "counterclockwise" and the like to indicate directions or positional relationships based on the directions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific direction, be constructed and operated in a specific direction, and therefore should not be understood as a limitation on the present invention.

[0025] Furthermore, the terms "first," "second," etc., are used for descriptive purposes only and should not be understood to indicate or imply relative importance or to implicitly specify the quantity of the technical features indicated. Thus, a feature designated "first," "second," etc. may explicitly or implicitly include one or more of the features.

[0026] In this utility model, unless otherwise specified or limited, the terms "installed," "connected," "connect," "fixed," etc. should be understood in a broad sense. For example, they can refer to fixed connection, detachable connection, or integral connection; mechanical connection or electrical connection; direct connection or indirect connection through an intermediate medium; and internal communication between two components. Those skilled in the art will understand the specific meanings of the above terms in this utility model based on specific circumstances.

[0027] In the present invention, unless otherwise expressly specified or limited, a first feature being "above" or "below" a second feature may include the first and second features being in direct contact, or may include the first and second features being in contact not directly but through another feature between them. Moreover, a first feature being "above," "above," and "above" a second feature may include the first feature being directly above or obliquely above the second feature, or may simply mean that the first feature is higher in level than the second feature. A first feature being "below," "below," and "below" a second feature may include the first feature being directly below or obliquely below the second feature, or may simply mean that the first feature is lower in level than the second feature.

[0028] Please refer to Figures 1 to 6 This embodiment provides a detachable wing structure of a model airplane toy, including a fuselage 100 and wings 200 detachably connected to the fuselage 100. The fuselage 100 is provided with an inner cavity 110 for fixing and installing a control circuit structure such as a battery and a circuit board. The inner cavity 110 is connected to the outside through an inner cavity opening. A hatch 300 is detachably adapted to be connected to the inner cavity opening. The inner cavity 110 can be opened or closed by connecting or detaching the hatch 300 to the inner cavity opening, so as to facilitate the disassembly and subsequent maintenance of the control circuit structure.

[0029] A detachable frame 120 is fixedly attached to the fuselage 100 adjacent to the inner cavity opening. It is understood that a positioning plate for the detachable frame 120 is exposed on one side of the inner cavity opening. This positioning plate is connected to the hatch 300 in a manner that allows one end of the hatch 300 to be detachably connected to the inner cavity opening. A recessed slot 111 is provided on the other side of the inner cavity opening. This slot 111 is detachably plugged into and fixed to the hatch 300, allowing the other end of the hatch 300 to be similarly detachably connected to the inner cavity opening.

[0030] The detachable frame 120 includes an outer frame 121 fixed to the fuselage 100 and an inner frame 122 fixed to the outer frame 121. The outer frame 121 has two through-holes and a bottom with a first through-hole 1211 communicating with the inner cavity 110. The first through-hole 1211 allows the conductive wires of the control circuit structure to pass through and enter the detachable frame 120. It will be understood that fixing posts 1212 are respectively provided on both sides of the outer wall of the outer frame 121 at positions directly opposite the connecting posts of the inner frame 122. The fixing posts 1212 on the same side of the outer frame 121 have countersunk holes for receiving screws, which can be used to securely connect the inner frame 122 to the outer frame 121. The outer frame 121 is also provided with an adhesive plate 1214, which is planar and annularly arranged around the outer periphery of the outer frame 121. Adhesion plate 1214 is adhesively fixed to the interior of the fuselage 100, ensuring a more secure and stable connection between the fuselage 100 and the detachable frame 120. A positioning plate 1215 is perpendicularly mounted on the adhesive plate 1214, at least partially extending outside the fuselage 100. Specifically, a portion of positioning plate 1215 is exposed on one side of the inner cavity opening. Positioning plate 1215 is designed to engage with the elastic U-shaped buckle of the hatch cover 300, thereby preventing it from tilting upward away from the inner cavity opening.

[0031] In this embodiment, the inner frame 122 includes a first frame 1221 and a second frame 1222, each of which includes a chamber 1230. In other words, the inner frame 122 is provided with two chambers 1230 on either side of the outer frame 121. The two chambers 1230 are connected to the first through-hole 1211 via a second through-hole 1231, allowing the conductive wires of the control circuit structure to pass through the second through-hole 1231 and enter the two chambers 1230. It is understood that at least one fixing portion is provided on each side where the first frame 1221 and the second frame 1222 meet, each of which includes a connecting column 1223 and a clearance groove 1224 arranged adjacent to each other in the vertical direction. The connecting column 1223 of the first frame 1221 is placed in the clearance groove 1224 connected to the second frame 1222, so that the connecting columns 1223 of the first frame 1221 and the second frame 1222 and the fixing columns 1212 on both sides of the outer frame 121 can be placed on the same axis and fixed together by the screws, thereby enabling the first frame 1221 and the second frame 1222 to be fixed in an adjacent arrangement within the outer frame 121. It should be noted that splitting the inner frame 122 into a combination of the first frame 1221 and the second frame 1222 can help simplify the production process and save production costs. In other embodiments of the present invention, the inner frame 122 can be formed as a single piece. In this case, only the connecting column 1223 is provided in the inner frame 122 relative to the fixing column 1212.

[0032] In this embodiment, a first positioning post 1225 protrudes from the sidewall of the first frame 1221 toward the second frame 1222. A corresponding second positioning post 1226 is provided on the sidewall of the second frame 1222 to accommodate the first positioning post 1225, facilitating quick positioning and connection between the first frame 1221 and the second frame 1222. The second positioning post 1226 protrudes from the cavity 1230 of the second frame 1222 and can be removably inserted into the insertion section fixed to the wing 200, further enhancing the stability and securement of the connection of the wing 200 within the cavity 1230. In other embodiments of the present invention, the first and second frames 1221, 1222 may not be provided with the first and second positioning posts 1225, 1226.

[0033] As can be understood, the inner wall of each chamber 1230 is raised from the inside outward to form a first insert block 1232 and a second insert block 1233. The first insert block 1232 is provided with a first insertion hole 1234 for communication with the outside world, while the second insert block 1233 is provided with a second insertion hole 1235 for communication with the outside world and the second through hole 1231. In this embodiment, the height of the first insert block 1232 is greater than that of the second insert block 1233, which is less than the depth of the second groove in the wing 200. Furthermore, the inner frame 122 also includes a third through hole 1236, which is located on the sidewall between the two chambers 1230, opposite the second insertion hole 1235 and communicating with the second through hole 1231. It should be noted that the unequal heights of the first and second insert blocks 1232, 1233 facilitate the user's ability to correctly insert and secure the wing 200 into the corresponding chamber 1230. The unequal heights of the second insert 1233 and the second groove, as well as the provision of the third through hole 1236, allow the conductive wires of the control circuit structure to be arranged in a relatively reasonable and orderly manner, facilitating subsequent maintenance operations. In other embodiments of the present invention, the first insert 1232 and the second insert 1233 can be arranged at the same height, and the second insert 1233 can also be arranged at the same height as the second groove. In this case, the sidewall between the two chambers 1230 may optionally be provided with the third through hole 1236.

[0034] There are two wings 200, each comprising an integrally formed insertion section 210 and wing section 220. The insertion section 210 is removably adapted to be inserted into the cavity 1230. A first slot 211 matching the shape of the first insert block 1232 and a second slot 212 matching the shape of the second insert block 1233 are recessed within the insertion section 210. It will be appreciated that, because the arrangement of the connecting posts 1223 results in a correspondingly shaped protrusion within each cavity 1230, a third slot 213 matching the shape of the protrusion is also recessed within the insertion section 210. Furthermore, because the second positioning post 1226 protrudes into one of the cavities 1230, a fourth slot 214 matching the shape of the second positioning post 1226 is also recessed within the insertion section 210 of one of the wings 200.

[0035] As will be understood, the wing section 220 is provided with a rudder plate 221 and a fixing slot 222. The rudder plate 221 is pivotally connected to the wing section 220. A servo 230 is fixedly mounted within the fixing slot 222. The swing arm 231 of the servo 230 is linked to the rocker 2211 of the rudder plate 221 via a connecting rod. This arrangement enables the servo 230 to swing the rocker 2211 by swinging the swing arm 231, causing the rudder plate 221 to swing on the wing section 220. By adjusting the angle of the rudder plate 221, the flow state of the airflow on either side of the wing 200 is differentiated, thereby enabling the model aircraft to be steered in a desired direction. Wing section 220 is further provided with a first groove 223 and a second groove 224. An insert 240 is embedded in first groove 223. Insert 240 extends into first slot 211 and is removably inserted and fixed into first receptacle 1234. Second groove 224 communicates with second slot 212 and is connected to second receptacle 1235. In other words, when insertion section 210 of wing 200 is inserted into corresponding cavity 1230, first insert 1232 is inserted into first slot 211, insert 240 is inserted into first receptacle 1234, second insert 1233 is inserted into second slot 212, and second groove 224 is connected to second receptacle 1235. At the same time, the second groove 224 is connected to the fixing groove 222, so that the conductive wire of the servo 230 can be received in the second groove 224 and can enter the inner cavity 110 through the second plug hole 1235, the second through hole 1231 and the first through hole 1211 in sequence, thereby realizing the electrical connection between the servo 230 and the control circuit structure.

[0036] It should be noted that in other embodiments of the present invention, a light-emitting diode can also be fixedly installed in the fixing groove 222. At this time, the conductive wire of the light-emitting diode can also be placed in the second groove 224 and can pass through the third through hole 1236, the second through hole 1231 and the first through hole 1211 in sequence into the inner cavity 110, thereby realizing the electrical connection between the light-emitting diode and the control circuit structure.

[0037] One end of the hatch cover 300 is provided with a latch block 310 that is detachably engaged with the latch slot 111. The other end of the hatch cover 300 is provided with an elastic U-shaped buckle 320. The movable end of the elastic U-shaped buckle 320 is provided with a retaining foot 321 that engages and contacts the positioning plate 1215. The movable end of the elastic U-shaped buckle 320 can movably extend from the hatch cover 300. As will be appreciated, due to the elasticity of the elastic U-shaped buckle 320, the elastic force of the elastic U-shaped buckle 320 allows it to remain in the position where the retaining foot 321 engages and contacts the positioning plate 1215, thereby securing one end of the hatch cover 300 to the inner cavity opening. To open the hatch cover 300, the elastic U-shaped buckle 320 is pushed to move the retaining foot 321, separating it from the positioning plate 1215. The end of the hatch cover 300 is then pulled to separate from the inner cavity opening.

[0038] In summary, the detachable wing structure provided in this embodiment comprises a multi-connection structure between the detachable frame 120 and the wing 200, comprising a cavity 1230 and an insertion section 210, an insert block and slot, a positioning post and slot, an insert strip 240, and a first insertion hole 1234. This structure enables a relatively stable and secure connection of the wing 200 to the fuselage 100. Furthermore, this multi-connection structure offers the advantages of simple, convenient, and quick assembly and disassembly, eliminating the need for additional tools when installing or removing the wing 200, thereby enhancing the ease of installation and removal of the wing 200. Furthermore, the detachable wing structure further comprises a channel structure between the detachable frame 120 and the wing 200, comprising a first through hole 1211, a second through hole 1231, a third through hole 1236, a second insertion hole 1235, and a second groove 224. This channel structure connects the wing 200 to the inner cavity 110, facilitating the concealment of conductive wires and enhancing the aesthetics of the model aircraft toy.

[0039] For clarity, certain features of the present invention described in the context of separate embodiments may be combined in a single embodiment. Furthermore, various features of the present invention described in the context of a single embodiment may also be used individually or in any suitable subcombination.

Claims

1. A detachable wing structure of a model airplane toy, comprising a fuselage and wings detachably connected to the fuselage, characterized in that: A detachable frame is fixedly connected to the fuselage, comprising an outer frame fixed to the fuselage and an inner frame fixed to the outer frame. The outer frame is provided with two through-holes on both sides and a first through-hole at its bottom that communicates with the inner cavity of the fuselage. The inner frame is provided with two chambers on either side of the outer frame. The two chambers are connected to the first through-hole via second through-holes. The inner wall of each chamber is raised from the inside to the outside to form a first plug-in block and a second plug-in block. The first plug-in block is provided with a first plug-in hole that communicates with the outside world, and the second plug-in block is provided with a second plug-in hole that communicates with the outside world and the second through-hole. The wing comprises an integrally formed insertion section and a wing section. The insertion section is detachably adapted to be inserted into the chamber. The insertion section is provided with a first slot that matches the shape of the first plug-in block and a second slot that matches the shape of the second plug-in block. The wing section is provided with a first groove and a second groove. The first groove is provided with an insert bar that extends into the first slot and is removably inserted and fixed in the first hole. The second groove is connected to the second slot and can be connected to the second hole.

2. The detachable wing structure of the model airplane toy according to claim 1, characterized in that: The height of the first inserting block is greater than the height of the second inserting block, and the height of the second inserting block is less than the depth of the second groove.

3. The detachable wing structure of the model airplane toy according to claim 2, characterized in that: A third through hole is further provided in the inner frame. The third through hole is opened on the side wall between the two chambers, facing the second insertion hole. The third through hole is communicated with the second through hole.

4. The detachable wing structure of the model airplane toy according to claim 1, characterized in that: The inner frame includes a first frame and a second frame, each of which has a chamber, and each side where the first frame and the second frame are connected is provided with at least one fixing part, each of which includes a connecting column and a clearance groove arranged adjacent to each other in the vertical direction, and the connecting column of the first frame is placed in the clearance groove connected to the second frame, so that the connecting columns of the first frame and the second frame are placed on the same axis and can be fixed in the outer frame by screws.

5. The detachable wing structure of the model airplane toy according to claim 4, characterized in that: A first positioning column protrudes from the side wall of the first frame toward the second frame, and a second positioning column is correspondingly provided on the side wall of the second frame to accommodate the first positioning column. The second positioning column protrudes from the cavity of the second frame and can be inserted and fixed in the insertion section in a removable manner.

6. The detachable wing structure of the model airplane toy according to claim 4, characterized in that: Fixed columns are respectively provided on both sides of the outer wall of the outer frame at positions directly opposite to the connecting columns, and countersunk holes for receiving the screws are provided in the fixed columns located on the same side of the outer frame.

7. The detachable wing structure of the model airplane toy according to claim 1, characterized in that: The outer frame is further provided with an adhesion plate, which is planar and arranged around the outer periphery of the outer frame. A positioning plate is vertically arranged on the adhesion plate, and at least part of the positioning plate extends out of the fuselage.

8. The detachable wing structure of the model airplane toy according to claim 7, characterized in that: The inner cavity of the fuselage is connected to the outside world through the inner cavity opening, and a hatch cover is adapted to be connected to the inner cavity opening. The positioning plate is exposed on one side of the inner cavity opening, and the positioning plate is connected to the hatch cover in a contacting manner. A card slot is recessed on the other side of the inner cavity opening and is detachably plugged into the hatch cover.

9. The detachable wing structure of the model airplane toy according to claim 8, characterized in that: One end of the hatch cover is provided with a card block that can be detachably plugged into the card slot, and the other end of the hatch cover is provided with an elastic U-shaped buckle. The movable end of the elastic U-shaped buckle is provided with a limiting foot that can be abutted and connected with the positioning plate, and the movable end of the elastic U-shaped buckle can be movably extended from the hatch cover.

10. The detachable wing structure of the model airplane toy according to claim 1, characterized in that: The wing section is also provided with a rudder plate and a fixing groove. The rudder plate is swingably connected to the wing section. A steering gear is fixedly installed in the fixing groove. The swing arm of the steering gear is connected to the swing rod of the rudder plate through a connecting rod. The conductive wire of the steering gear can be placed in the second groove.

Citation Information

Patent Citations

  • Detachable stationary vane model aeroplane and model ship aircraft

    CN208641746U