CN218529773U - Transformable toy airplane - Google Patents
Transformable toy airplane Download PDFInfo
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- CN218529773U CN218529773U CN202222661483.2U CN202222661483U CN218529773U CN 218529773 U CN218529773 U CN 218529773U CN 202222661483 U CN202222661483 U CN 202222661483U CN 218529773 U CN218529773 U CN 218529773U
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- 230000000712 assembly Effects 0.000 claims description 3
- 238000000429 assembly Methods 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 6
- 230000008569 process Effects 0.000 description 6
- 238000003780 insertion Methods 0.000 description 4
- 230000037431 insertion Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
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Abstract
The utility model discloses a deformation toy aircraft relates to children's toys technical field, include: an aircraft body; the impeller is fixedly connected with the output end of a driving motor distributed in the main body of the airplane; the blades are arranged in a plurality of groups, and each group of blades is arranged on the end face of the impeller in a circumferential array; further comprising: the first roller is arranged at the bottom side of the airplane body in a triangular shape; the wings are relatively and rotatably arranged on two sides of the airplane body; the second gyro wheel, the second gyro wheel is laid at the wing end, through the orientation upset wing towards aircraft main part bottom for the wing is by being out of shape for the straightness state that hangs down with aircraft main part parallel state, because the wing has certain length, makes for the aircraft main part promoted to the take the altitude, and the distance grow between aircraft main part and the ground to comparatively complicated road surface, for example the surface has the road surface of water or grit, in the course of driving, can not cause the influence to the aircraft main part, and object for appreciation nature is higher.
Description
Technical Field
The utility model relates to a children's toys technical field, concretely relates to toy aircraft warp.
Background
Nowadays, children toys with different styles and functions not only bring much fun to the life of children, but also have great significance for the early intelligence development of the children toys. The toy airplane is taken as a type of toy which is hot, and is deeply loved and touted by children;
however, most of these toys adopt a single modeling structure, so that the toys only have the functions of a swing part and have no dynamic deformation process, so that the toys are not strong in interestingness and durability, the practical ability of children cannot be cultivated, and children easily lose the interest in playing.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a deformation toy aircraft solves following technical problem:
most of these toys adopt single molding structure, make its function that only has the goods of furniture for display rather than for use, do not have the process of dynamic deformation, lead to its interest and durability not strong yet, also can't cultivate children's hands-on ability, and child loses the interest of playing very easily.
The purpose of the utility model can be realized by the following technical proposal:
a transformable toy aircraft comprising:
an aircraft body;
the impeller is fixedly connected with the output end of a driving motor distributed in the main body of the airplane;
the blades are arranged in a plurality of groups, and the blades of each group are arranged on the end face of the impeller in a circumferential array;
further comprising:
the first roller is arranged at the bottom side of the airplane main body in a triangular shape;
the wings are relatively rotatably arranged on two sides of the airplane main body;
and the second idler wheels are arranged at the tail ends of the wings.
Preferably, a balance plate is arranged on one side of the wing and is fixedly connected with a positioning rod which is arranged in the wing in a sliding manner;
wherein, the balance plate end is correspondingly provided with a third roller for supporting.
Preferably, the end part of the positioning rod is also provided with a positioning hole;
wherein, the corresponding slip cloth is equipped with the inserted bar that is used for with the locating hole grafting on the wing, and the inserted bar tip is equipped with the handle, still is equipped with expanding spring on the inserted bar.
Preferably, the blades are provided in five groups.
Preferably, a plurality of groups of tail assemblies are arranged at the tail end of the tail of the airplane body in a circumferential array.
Preferably, a cabin assembly is arranged on the aircraft body.
The utility model has the advantages that:
(1) When the wings on the two sides are in a normal unfolding mode, the aircraft main body is supported through the first rollers, the aircraft can run on a relatively gentle road surface, when the wings on the two sides are folded, the wings are turned towards the bottom of the aircraft main body, so that the wings are deformed from a parallel state with the aircraft main body into a vertical state, and then the aircraft main body is supported through the second rollers, and as the wings have a certain length, the aircraft main body is lifted to a certain height, the distance between the aircraft main body and the ground is increased, and for a complex road surface, such as a road surface with water or gravel on the surface, the aircraft main body is not influenced in the running process, and the playability is higher;
(2) When the wing is overturned, the wing drives the balance plate to synchronously rotate through the positioning rod, so that the third idler wheel at the bottom of the balance plate simultaneously supports the aircraft main body, the distance between the third idler wheel and the second idler wheel is increased by arranging the telescopic balance plate, and the running stability of the toy aircraft after deformation is improved.
Drawings
The present invention will be further described with reference to the accompanying drawings.
FIG. 1 is a schematic perspective view of a transformable toy aircraft according to the present invention;
FIG. 2 is a schematic perspective view of a transformable toy aircraft according to the present invention;
FIG. 3 is a third schematic perspective view of a transformable toy aircraft according to the present invention;
fig. 4 is a schematic structural view of the positioning rod of the transformable toy airplane.
In the figure: 1. an aircraft body; 2. a drive motor; 3. a second roller; 4. inserting a rod; 101. a nacelle assembly; 102. a tail assembly; 103. an airfoil; 201. an impeller; 202. a blade; 301. positioning a rod; 302. a third roller; 303. a balance plate; 401. a tension spring; 402. a handle; 403. positioning holes; 5. a first roller.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-2, the present invention relates to a transformable toy aircraft, which includes an aircraft body 1, wings 103 are disposed on two sides of the aircraft body 1, and the wings 103 are rotatably connected to the aircraft body 1, it should be noted that the wings 103 and the aircraft body 1 can be rotatably connected by hinges, etc., and are not limited in this embodiment, so that the wings 103 can be folded;
the aircraft body 1 is provided with an impeller 201, the impeller 201 is fixedly connected with the output end of a driving motor 2 arranged in the aircraft body 1, and blades 202 are arranged on the outer end surface of the impeller 201 in a circumferential array; in an embodiment, the output end of the driving motor 2 drives the impeller 201 to rotate, and the impeller 201 drives the blades 202 to rotate in the rotating process, so as to implement the operation of the toy airplane, specifically, the blades 202 are provided with a plurality of groups, which can be set into three, four or five groups, and the like, and meanwhile, the toy airplane is not limited to the driving motor 2 in this embodiment, and corresponding driving equipment can be selected according to actual conditions, so that the impeller 201 can be driven to rotate;
the bottom of the airplane body 1 is provided with a plurality of groups of first rollers 5 for the toy airplane to run on a normal road, and specifically, the first rollers 5 are distributed with three groups and arranged at the bottom of the airplane body 1 in a triangular shape;
the tail end of the wing 103 is provided with the second roller 3, so that when the wing 103 is folded, the second roller 3 is in contact with the ground for supporting, specifically, the toy aircraft has two play modes, when the wings 103 on two sides are in a normal unfolding mode, the aircraft main body 1 is supported through the first roller 5, the toy aircraft can run on a relatively gentle road surface, when the wings 103 on two sides are folded, the wings 103 are turned towards the bottom of the aircraft main body 1, so that the wings 103 are deformed from a parallel state with the aircraft main body 1 to a vertical 90-degree state, and further the aircraft main body 1 is supported through the second roller 3, because the wings 103 have a certain length, the aircraft main body 1 is lifted to a certain height, the distance between the aircraft main body 1 and the ground is increased, for a complex road surface, such as a road surface with water or gravels, the aircraft main body 1 cannot be affected during running, and the playability is higher.
Referring to fig. 3, in some embodiments, a balance plate 303 is disposed on one side of the wing 103, and the balance plate 303 is fixedly connected to a positioning rod 301 slidably disposed in the wing 103;
wherein, the end part of the balance plate 303 is correspondingly provided with a third roller 302 for supporting; when the wings 103 are turned over, the wings 103 drive the balance plate 303 to synchronously rotate through the positioning rod 301, so that the third idler wheel 302 at the bottom of the balance plate 303 simultaneously supports the aircraft main body 1, in the embodiment, the distance between the third idler wheel 302 and the second idler wheel 3 is increased by arranging the telescopic balance plate 303, and the running stability of the toy aircraft after deformation is further improved;
referring to fig. 4, further, a positioning hole 403 is further disposed at an end of the positioning rod 301, wherein an insertion rod 4 for inserting into the positioning hole 403 is disposed on the wing 103 in a sliding manner, a handle 402 is disposed at an end of the insertion rod 4, and a telescopic spring 401 is further disposed on the insertion rod 4; specifically, when the position between the balance plate 303 and the wing 103 is adjusted, the balance plate 303 is pulled to drive the positioning rod 301 to slide between the wings 103, and when the farthest distance is reached, the insertion rod 4 is driven to be inserted into the positioning hole 403 under the action of the elastic force of the telescopic spring 401, so that the balance plate 303 is fixed;
in addition, a plurality of groups of tail wing assemblies 102 are arranged at the tail end of the tail part of the airplane body 1 in a circumferential array, so that the airplane body 1 plays a balancing role in the driving process;
furthermore, the aircraft body 1 is provided with a cabin assembly 101, in the embodiment, the cabin assembly 101 can be configured in an animal shape, so that the playability of the toy aircraft is improved, and the toy aircraft is more vivid.
The utility model discloses a theory of operation: when the wings 103 on two sides are in a normal unfolding mode, the aircraft body 1 is supported through the first rollers 5, the aircraft can run on a relatively gentle road surface, when the wings 103 on two sides are folded, the wings 103 are turned towards the bottom of the aircraft body 1, so that the wings 103 are deformed into a vertical 90-degree state from a parallel state with the aircraft body 1, and further the aircraft body 1 is supported through the second rollers 3, because the wings 103 have a certain length, the aircraft body 1 is lifted to a certain height, the distance between the aircraft body 1 and the ground is increased, for a relatively complex road surface, such as a road surface with water or gravel on the surface, and in a running process, the influence on the aircraft body 1 cannot be caused.
In the description of the present invention, it should be understood that the terms "upper", "lower", "left", "right", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of the description, but do not indicate or imply that the device or element referred to must have a specific orientation and a specific orientation configuration and operation, and thus, should not be construed as limiting the present invention. Furthermore, "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate member, or they may be connected through two or more elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Although an embodiment of the present invention has been described in detail, the description is only for the purpose of illustrating the preferred embodiments of the present invention and should not be taken as limiting the scope of the present invention. All the equivalent changes and improvements made according to the application scope of the present invention should still fall within the patent coverage of the present invention.
Claims (6)
1. A transformable toy aircraft, comprising:
an aircraft body (1);
the impeller (201), the said impeller (201) is fixed with the output end of the driving motor (2) laid in the body (1) of the plane;
the impeller comprises a plurality of groups of blades (202), wherein the blades (202) of each group are arranged on the end surface of the impeller (201) in a circumferential array;
further comprising:
the first roller (5) is arranged at the bottom side of the airplane main body (1) in a triangular shape;
the wings (103), the wings (103) are relatively rotatably arranged on two sides of the airplane main body (1);
the second roller (3), second roller (3) is arranged at the tail end of wing (103).
2. A transformable toy aircraft according to claim 1, characterized in that a balancing plate (303) is provided on one side of the wing (103), the balancing plate (303) being fixedly connected to a positioning rod (301) slidably disposed in the wing (103);
wherein, the end of the balance plate (303) is correspondingly provided with a third roller (302) for supporting.
3. A transformable toy aircraft according to claim 2, characterized in that the positioning rod (301) is also provided with positioning holes (403) at its ends;
wherein, the wing (103) is correspondingly provided with an inserted bar (4) in a sliding way for being inserted into the positioning hole (403), the end part of the inserted bar (4) is provided with a handle (402), and the inserted bar (4) is also provided with a telescopic spring (401).
4. A transformable toy aircraft according to any one of claims 1-3, characterised in that the blades (202) are provided in five groups.
5. A transformable toy aircraft as claimed in claim 4, characterized in that the tail ends of the aircraft body (1) are provided with groups of tail assemblies (102) in a circumferential array.
6. A transformable toy aircraft according to claim 1, characterized in that the aircraft body (1) is provided with a cabin module (101).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202222661483.2U CN218529773U (en) | 2022-10-10 | 2022-10-10 | Transformable toy airplane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202222661483.2U CN218529773U (en) | 2022-10-10 | 2022-10-10 | Transformable toy airplane |
Publications (1)
Publication Number | Publication Date |
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CN218529773U true CN218529773U (en) | 2023-02-28 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202222661483.2U Active CN218529773U (en) | 2022-10-10 | 2022-10-10 | Transformable toy airplane |
Country Status (1)
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CN (1) | CN218529773U (en) |
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2022
- 2022-10-10 CN CN202222661483.2U patent/CN218529773U/en active Active
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