CN216725768U - Transformable airplane toy - Google Patents
Transformable airplane toy Download PDFInfo
- Publication number
- CN216725768U CN216725768U CN202122940464.9U CN202122940464U CN216725768U CN 216725768 U CN216725768 U CN 216725768U CN 202122940464 U CN202122940464 U CN 202122940464U CN 216725768 U CN216725768 U CN 216725768U
- Authority
- CN
- China
- Prior art keywords
- head
- fuselage
- wing
- rotating
- sides
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Images
Landscapes
- Toys (AREA)
Abstract
本实用新型涉及一种变形飞机玩具，包括依次连接的机头部、前机身部、后机身部和机尾部；所述机头部包括左右对称的左机头和右机头，左机头和右机头的一端分别可转动地设置在前机身部；所述后机身部与前机身部之间可伸缩地连接，所述前机身部的顶部可滑动地设有机翼部，所述机尾部与所述后机身部之间可转动地连接。本实用新型所述的变形飞机玩具，其设计巧妙，可变形为机器人的玩具造型，并且在变形的过程中能够培养儿童的动手能力，具有很高的趣味性和娱乐性。
The utility model relates to a deformed aircraft toy, which comprises a head part, a front body part, a rear body part and a tail part which are connected in sequence; One ends of the head and the right nose are respectively rotatably arranged on the front fuselage part; the rear fuselage part and the front fuselage part are telescopically connected, and the top of the front fuselage part is slidably provided with wings part, the tail part and the rear fuselage part are rotatably connected. The deformed airplane toy of the utility model has an ingenious design, can be deformed into a toy shape of a robot, can cultivate children's hands-on ability in the process of deformation, and is highly interesting and entertaining.
Description
Technical Field
The utility model relates to a toy technical field especially relates to a deformation aircraft toy.
Background
The development of the children toy industry is promoted by the technological progress, and nowadays, various 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. Toy airplanes, as a popular type of toy, are very popular and sought after by children.
Toy aircraft on the market at present adopts single molding structure mostly, makes its function that only has the goods of furniture for display rather than for use, does not have dynamic deformation's process, leads 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.
SUMMERY OF THE UTILITY MODEL
Based on this, the utility model aims at overcoming prior art's not enough, providing a deformation aircraft toy, its design benefit, the flexible toy molding for the robot to can cultivate children's manipulative ability at the in-process that warp, have very high interest and recreational.
In order to realize the purpose, the utility model discloses a technical scheme be:
a deformable airplane toy comprises a nose part, a front fuselage part, a rear fuselage part and a tail part which are connected in sequence; the machine head part comprises a left machine head and a right machine head which are bilaterally symmetrical, and one ends of the left machine head and the right machine head are respectively and rotatably arranged on the front machine body part; the rear fuselage portion is telescopically connected with the front fuselage portion, the top of the front fuselage portion is slidably provided with a wing portion, and the tail portion is rotatably connected with the rear fuselage portion.
As an implementation mode, a robot head is arranged at the front end of the front body part, first rotating members are respectively and rotatably arranged on two sides of the front end of the front body part, head rotating members are respectively arranged at the rear ends of the left head and the right head, and the left head and the right head are respectively and movably connected with the first rotating members on two sides of the front body part through respective head rotating members.
As an embodiment, the first rotating members on both sides of the front fuselage portion can rotate towards both sides of the front fuselage portion respectively, and the ends of the two first rotating members are provided with first elastic convex columns; the machine head rotating parts of the left machine head and the right machine head can rotate towards the outer sides of the left machine head and the right machine head respectively, the tail ends of the two machine head rotating parts are provided with first sleeves respectively, and the two machine head rotating parts are movably sleeved on the first elastic protruding columns of the two first rotating parts through the respective first sleeves respectively.
As an embodiment, two sides of the front body part are respectively provided with a robot hand part in a rotatable way, and the two robot hand parts are arranged symmetrically; each robot hand part comprises a shoulder armor part and a scroll-shaped arm part, and the shoulder armor part and the arm part are rotatably connected; the both sides of preceding fuselage portion are equipped with the second respectively and rotate the piece, and the epaulette portion of two robots hands portion is connected with two second rotation pieces of preceding fuselage portion respectively.
In one embodiment, the shoulder armor part and the arm part are rotatably connected through an arm joint; the arm portion is equipped with fist portion, fist portion rotationally sets up and keeps away from the epaulet portion at the arm portion and gets one end, and is equipped with the weapon mounting hole on the fist portion.
As an implementation mode, the wing part comprises a sliding base plate and wing plates rotatably arranged on two sides of the sliding base plate, the sliding base plate is slidably arranged on the top of the front body part, and the top of the sliding base plate is detachably inserted with a radar turntable.
As an implementation mode, the sliding base plate comprises a front sliding plate and a rear sliding plate which are connected in a front-rear overturning manner, the top of the rear sliding plate is provided with an insertion column, the bottom of the radar turntable is provided with a first insertion hole which is inserted in a matching manner with the insertion column, and the top of the front sliding plate is provided with a second insertion hole which is inserted in a matching manner with the insertion column; wing rotating grooves are respectively formed in two sides of the front sliding plate, wing plates are respectively provided with wing rotating shafts, the two wing parts are respectively rotatably arranged in the wing rotating grooves of the front sliding plate through the respective wing rotating shafts, and the bottoms of the two wing parts are respectively detachably inserted with turbine parts.
As an embodiment, the rear body section includes a rotating base and two machine leg sections rotatably disposed on the rotating base, a front end of the rotating base is rotatably disposed at a rear end of the front body section, and the two machine leg sections are relatively rotatable, respectively.
As an embodiment, the rear body part further comprises a left body shell and a right body shell which are symmetrically arranged with each other, and the rear ends of the two machine leg parts are respectively telescopically arranged in the left body shell and the right body shell; the opposite sides of the left machine body shell and the right machine body shell are respectively provided with a leg inserting hole and a leg inserting piece which are matched and inserted, and the ends, far away from the two machine legs, of the left machine body shell and the right machine body shell are respectively provided with a sole supporting part in a turnable manner.
As an embodiment, the front top of the tail part is rotatably arranged on the rear top of the rear body part through a tail rotating part; the top of the tail part is vertically and upwards provided with a tail wing part, and two sides above the tail wing part are respectively detachably inserted with a transverse wing plate.
The transformable airplane toy of the utility model has the advantages that the transformable airplane toy is ingenious in design, can be used as an airplane toy to play, set and the like, can be transformed into a toy shape of a robot through transformation operation, and particularly can be transformed into a toy shape of the robot through operations such as matching rotation, splicing, splitting or stretching between the nose part, the front fuselage part, the rear fuselage part, the tail part and the wing part, so that the practical ability of children can be cultivated in the transformation process, and the transformable airplane toy has high interestingness and entertainment; additionally, the utility model discloses a deformation aircraft toy novel structure, appearance are pleasing to the eye, make the object for appreciation nature of toy obtain high promotion through the dynamic effect that warp, have fine market value.
For a better understanding and an implementation, the present invention is described in detail below with reference to the accompanying drawings.
Drawings
FIG. 1 is a schematic view of a transformable toy aircraft according to the present invention;
FIG. 2 is another schematic structural view of the transformable toy aircraft of the present invention;
FIG. 3 is a partially exploded perspective view of the transformable toy aircraft of the present invention;
FIG. 4 is a schematic view of the connection between the turbine member and the transverse wing plate of the transformable aircraft toy of the present invention;
FIG. 5 is a front view of the transformable toy aircraft according to the present invention;
FIG. 6 is a schematic view of the reverse structure of the transformable toy aircraft in the form of a robot according to the present invention;
fig. 7 is an exploded view of the robot configuration of the transformable toy aircraft according to the present invention.
Detailed Description
To further illustrate the embodiments, the present invention provides the accompanying drawings. The accompanying drawings, which are incorporated in and constitute a part of this disclosure, illustrate embodiments of the invention and, together with the description, serve to explain the principles of the embodiments. With these references, one of ordinary skill in the art will appreciate other possible implementations and advantages of the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "left", "right", "top", "bottom", "inner", "outer", "axial", "radial", "circumferential", and the like indicate orientations or positional relationships based on those shown in the drawings, and are merely for convenience of description and to simplify the description, and do not indicate or imply that the device or element so referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, are not to be considered limiting of the present invention.
Referring to fig. 1 to 7, fig. 1 is a schematic structural view of a transformable toy aircraft according to the present invention; FIG. 2 is another schematic structural view of the transformable toy aircraft of the present invention; FIG. 3 is a partially exploded perspective view of the transformable toy aircraft of the present invention; FIG. 4 is a schematic view of the connection between the turbine member and the transverse wing plate of the transformable aircraft toy of the present invention; FIG. 5 is a front view of the transformable toy aircraft according to the present invention; FIG. 6 is a schematic view of the reverse structure of the transformable toy aircraft in the form of a robot according to the present invention; fig. 7 is an exploded view of the robot configuration of the transformable toy aircraft according to the present invention.
The embodiment provides a transformable aircraft toy, which comprises a nose part 10, a front fuselage part 20, a rear fuselage part 30 and a tail part 40 which are connected in sequence; the nose part 10 comprises a left nose 11 and a right nose 12 which are symmetrical left and right, and one ends of the left nose 11 and the right nose 12 are respectively and rotatably arranged on a front body part 20; the rear fuselage section 30 is telescopically connected to the front fuselage section 20, the top of the front fuselage section 20 is slidably provided with a wing section 50, and the tail section 40 is rotatably connected to the rear fuselage section 30.
Optionally, the front end of the front body portion 20 is provided with a robot head 21, two sides of the front end of the front body portion 20 are respectively rotatably provided with a first rotating member 22, the rear ends of the left head 11 and the right head 12 are respectively provided with a head rotating member 23, and the left head 11 and the right head 12 are respectively movably connected with the first rotating members 22 at two sides of the front body portion 20 through the respective head rotating members 23.
Wherein, in this embodiment, the rear end of left aircraft nose 11 and right aircraft nose 12 is provided with the hemisphere cavity of symmetry and intercommunication each other respectively, and from this, when left aircraft nose 11 and right aircraft nose 12 interconnect, the accommodation space that holds robot head 21 is constituteed jointly to two hemisphere cavities for robot head 21 and the connection between left aircraft nose 11 and the right aircraft nose 12 are reasonable. When the left head 11 and the right head 12 are rotated toward both sides of the front body part 20, respectively, the robot head 21 is automatically visualized.
Further, the first rotating parts 22 at both sides of the front fuselage portion 20 of the present embodiment can rotate toward both sides of the front fuselage portion 20, and the ends of the two first rotating parts 22 are provided with first elastic protruding columns; the handpiece rotating pieces 23 of the left handpiece 11 and the right handpiece 12 can rotate towards the outer sides of the left handpiece 11 and the right handpiece 12 respectively, the tail ends of the two handpiece rotating pieces 23 are provided with first sleeves respectively, and the two handpiece rotating pieces 23 are movably sleeved on the first elastic convex columns of the two first rotating pieces 22 respectively through the respective first sleeves.
Optionally, two robot hand portions 24 are respectively rotatably disposed on two sides of the front body portion 20, and the two robot hand portions 24 are symmetrically disposed; each robot hand portion 24 includes a shoulder portion 25 and a arm portion 26 in a turbine shape, the shoulder portion 25 and the arm portion 26 being rotatably connected therebetween; second rotating members 27 are respectively provided on both sides of the front body section 20, and the shoulder portions 25 of the two robot hand portions 24 are respectively connected to the two second rotating members 27 of the front body section 20.
Further, the shoulder armor part 25 and the arm part 26 are rotatably connected through an arm joint 28; the arm part 26 is provided with a fist part which is rotatably arranged at one end of the arm part 26 far away from the shoulder armor part 25, and a weapon mounting hole is formed in the fist part.
Wherein, in the present embodiment, the shoulder portion 25 is rotatably connected to the outer end of the second rotating member 27; specifically, the end of the second rotating member 27 of the present embodiment is provided with a second elastic protruding pillar, the shoulder nail portion 25 is provided with a second sleeve engaged with the second elastic protruding pillar, and the shoulder nail portion 25 is movably sleeved on the second rotating member 27 through the second sleeve. Thus, the shoulder armor portion 25 of the present embodiment can be detached from the second rotating member 27 and can rotate 360 ° around the second rotating member 27, so that the flexibility of the shoulder armor portion 25 is greatly enhanced.
Optionally, the wing portion 50 includes a sliding base plate 52 and wing plates 53 rotatably disposed on two sides of the sliding base plate 52, the sliding base plate 52 is slidably disposed on the top of the front body portion 20, and a radar turntable 60 is detachably connected to the top of the sliding base plate 52.
Further, the sliding base plate 52 comprises a front sliding plate 54 and a rear sliding plate 55 which are connected in a front-rear overturning manner, the top of the rear sliding plate 55 is provided with an insertion column 56, the bottom of the radar turntable 60 is provided with a first insertion hole which is inserted in a matching manner with the insertion column 56, and the top of the front sliding plate 54 is provided with a second insertion hole 57 which is inserted in a matching manner with the insertion column 56; wing rotating grooves are respectively formed in two sides of the front sliding plate 54, wing plates 53 are respectively provided with wing rotating shafts, the two wing portions 50 are respectively rotatably arranged in the wing rotating grooves of the front sliding plate 54 through the respective wing rotating shafts, and turbine members 58 are respectively detachably inserted into the bottoms of the two wing portions 50.
In the present embodiment, in order to facilitate mounting the radar rotary disc 60 on one of the robot hands 24, a weapon mounting post is disposed on an outer side of the arm portion 26, and the weapon mounting post is fittingly inserted into the first insertion hole of the radar rotary disc 60, so that a user can mount the radar rotary disc 60 on the robot hand 24 as a shield weapon.
The outer ends of the two wing plates 53 are respectively and rotatably provided with a wing subplate 59, a rotating disc 51 is arranged between the wing subplates 59 and the wing plates 53, and the wing subplates 59 are movably sleeved on the rotating disc 51, so that the wing subplates 59 can rotate relative to the wing plates 53. In this embodiment, the bottom portions of the two wing plates 53 are respectively provided with a third insertion hole, and the two turbine members 58 are provided with an insertion block which is inserted into the third insertion hole in a matching manner, so that the turbine members 58 can be detachably inserted into the third insertion holes of the wing plates 53 through the insertion blocks.
In addition, in the present embodiment, a limit sliding slot is disposed at the top of the front fuselage portion 20, a wing slider is disposed at the bottom of the front sliding plate 54, and the wing slider is slidably disposed in the limit sliding slot of the front fuselage portion 20, so that the front sliding plate 54 can be slidably disposed at the top of the front fuselage portion 20 by the wing slider at the bottom thereof.
Optionally, the front body portion 20 is provided with an armor flap 29 at the bottom thereof in a turnable manner, one end of the armor flap 29 is rotatably disposed at the rear end of the bottom of the front body portion 20, the two sides of the armor flap 29 are respectively provided with a fourth jack, and the bottom of the front body portion 20 is provided with a flap insert block that is fittingly inserted into the fourth jack, so that when the armor flap 29 is turned over toward the front body portion 20, the flap insert block of the front body portion 20 can be fittingly inserted into the fourth jack.
Further, the front end of the rear fuselage section 30 of the present embodiment is rotatably connected to the rear end of the front fuselage section 20 through a universal joint structure, the top of the rear fuselage section 30 is provided with a limiting insertion block, and after the rear fuselage section 30 rotates 180 degrees relative to the front fuselage section 20, the armor flap 29 can rotate toward the rear fuselage section 30 and is inserted into the limiting insertion block of the rear fuselage section 30 through the fourth insertion hole thereof in a matching manner, so as to limit the rotation of the rear fuselage section 30.
Alternatively, the rear body section 30 includes a rotating base 31 and two machine legs 32 rotatably disposed on the rotating base 31, a front end of the rotating base 31 is rotatably disposed at a rear end of the front body section 20, and the two machine legs 32 are respectively rotatably disposed at a rear end of the rotating base 31.
Further, the rear body part 30 further includes a left body shell 33 and a right body shell 34 which are symmetrically arranged with each other, and rear ends of the two machine leg parts 32 are telescopically arranged in the left body shell 33 and the right body shell 34, respectively; the opposite sides of the left body shell 33 and the right body shell 34 are respectively provided with a leg plug-in hole and a leg plug-in unit which are matched and plugged, and the ends of the left body shell 33 and the right body shell 34 far away from the two machine legs 32 are respectively provided with a sole support part 35 in a turnable manner.
In the present embodiment, the front top of the tail portion 40 is rotatably disposed on the rear top of the rear fuselage portion 30 via a tail rotating member 43; the top of the tail part 40 is vertically and upwardly provided with a tail wing part 41, and two sides above the tail wing part 41 are respectively detachably inserted with a transverse wing plate 42.
In order to facilitate the storage design between the tail portion 40 and the sole support portions 35, in this embodiment, the front end of the tail portion 40 is provided with a receiving cavity, so that when the two sole support portions 35 are stored backwards, the two sole support portions can extend into the receiving cavity of the tail portion 40.
In addition, the wing plate 42 of the present embodiment is provided with wing insertion posts 44, and both sides of the upper end of the tail wing member 41 are respectively provided with wing insertion holes, so that the two wing plates 42 are respectively detachably inserted into the two wing insertion holes of the tail wing member 41 through the respective wing insertion posts 44. In order to further increase the playing method of the toy, the two turbine members 58 of the present embodiment are respectively provided with turbine insertion holes, and the two cross wing plates 42 are respectively provided with turbine insertion blocks which are in fit insertion with the turbine insertion holes, so that the cross wing plates 42 and the turbine members 58 can be in fit insertion with each other, and can be in fit insertion with the weapon mounting holes of the fist head through the cross wing insertion columns 44 of the two cross wings.
Compared with the prior art, the transformable aircraft toy of the utility model has ingenious design, can be used as an aircraft toy to play, decorate and the like, can be transformed into a toy shape of a robot through transformation operation, and specifically can be transformed into a toy shape of the robot through operations such as matching rotation, splicing, splitting or expansion and the like among the nose part 10, the front fuselage part 20, the rear fuselage part 30, the tail part 40 and the wing part 50, and can cultivate the practical and functional ability of children in the transformation process, thereby having high interest and entertainment; additionally, the utility model discloses a deformation aircraft toy novel structure, appearance are pleasing to the eye, make the object for appreciation nature of toy obtain high promotion through the dynamic effect that warp, have fine market value.
The above examples are merely illustrative of several embodiments of the present invention, and the description thereof is specific and detailed, but not intended to be construed as limiting the scope of the invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122940464.9U CN216725768U (en) | 2021-11-26 | 2021-11-26 | Transformable airplane toy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122940464.9U CN216725768U (en) | 2021-11-26 | 2021-11-26 | Transformable airplane toy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216725768U true CN216725768U (en) | 2022-06-14 |
Family
ID=81932081
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122940464.9U Expired - Fee Related CN216725768U (en) | 2021-11-26 | 2021-11-26 | Transformable airplane toy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216725768U (en) |
-
2021
- 2021-11-26 CN CN202122940464.9U patent/CN216725768U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP2529818B1 (en) | Interconnectable and transformable toy building element | |
| CN111167132B (en) | Deformation toy car | |
| CN102921174A (en) | Toy bricks | |
| CN216725768U (en) | Transformable airplane toy | |
| CN205796503U (en) | A kind of block toy assembly | |
| CN216725770U (en) | Transformable airplane toy | |
| CN212881017U (en) | A multi-unit combination toy with variable attitude | |
| CN219208964U (en) | Toy combination set | |
| CN217391577U (en) | Transformable airplane toy | |
| CN116407852B (en) | Cross-country vehicle deformation toy | |
| CN217661488U (en) | Aerospace deformation toy | |
| CN217391579U (en) | Transformable airplane toy | |
| CN217391578U (en) | Transformable airplane toy | |
| CN216824788U (en) | Transformable airplane toy | |
| CN116173520B (en) | A transforming airplane toy | |
| CN216725769U (en) | Transformable airplane toy | |
| CN217593809U (en) | Transformable toy car | |
| CN216725767U (en) | Transformable airplane toy | |
| CN216725771U (en) | Transformable helicopter toy | |
| CN214808399U (en) | Toy of space shuttle deformation robot | |
| CN211798783U (en) | A transforming toy car | |
| CN217661487U (en) | Aerospace deformation toy | |
| CN223350973U (en) | Folding and deformable structures and transformable toys | |
| CN217593801U (en) | Transformable robot toy | |
| CN217988349U (en) | A transforming robot toy |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220614 |