CN212491546U - Reinforcement type toy unmanned aerial vehicle - Google Patents
Reinforcement type toy unmanned aerial vehicle Download PDFInfo
- Publication number
- CN212491546U CN212491546U CN202021272422.1U CN202021272422U CN212491546U CN 212491546 U CN212491546 U CN 212491546U CN 202021272422 U CN202021272422 U CN 202021272422U CN 212491546 U CN212491546 U CN 212491546U
- Authority
- CN
- China
- Prior art keywords
- propeller
- aerial vehicle
- unmanned aerial
- toy
- reinforcement
- 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.)
- Active
Links
Images
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a reinforcement type toy unmanned aerial vehicle, this reinforcement type toy unmanned aerial vehicle includes: the aircraft comprises a rack main body and a plurality of wing assemblies arranged on two sides of the rack main body, wherein each wing assembly comprises a machine arm connected with the rack main body, a propeller air guide sleeve arranged at one end of the machine arm far away from the rack main body and a propeller arranged in the propeller air guide sleeve, and a gap is reserved between the propeller air guide sleeves; wherein, reinforcement type toy unmanned aerial vehicle still includes a plurality of reinforcements, the reinforcement is followed extending direction's both ends respectively with adjacent two the screw kuppe meets. The utility model discloses technical scheme installs the screw in the screw kuppe, meets through reinforcement and each independent screw kuppe, makes each independent screw link to each other, forms the whole that a structure is firm, has improved the steadiness of reinforcement type toy unmanned aerial vehicle structure.
Description
Technical Field
The utility model relates to a flight class toy technical field, in particular to reinforcement type toy unmanned aerial vehicle.
Background
With the development of social economy and the continuous improvement of the living standard of people, the styles of children toys on the market are diversified, and the reinforced unmanned toy vehicle is deeply loved by children as a flying toy; mutually independent each other between each screw of reinforcement type toy unmanned aerial vehicle on the present market, the structural stability of this type of screw can be relatively weak, when receiving external colliding with, easy broken damage or directly break away from with the fuselage to lead to reinforcement type toy unmanned aerial vehicle's life to shorten greatly.
SUMMERY OF THE UTILITY MODEL
The utility model mainly aims at providing a reinforcement type toy unmanned aerial vehicle aims at improving the structure steadiness of screw.
In order to achieve the above object, the utility model provides a reinforcement type toy unmanned aerial vehicle, include: the aircraft comprises a rack main body and a plurality of wing assemblies arranged on two sides of the rack main body, wherein each wing assembly comprises a machine arm connected with the rack main body, a propeller air guide sleeve arranged at one end of the machine arm far away from the rack main body and a propeller arranged in the propeller air guide sleeve, and a gap is reserved between the propeller air guide sleeves; wherein the content of the first and second substances,
reinforcement type toy unmanned aerial vehicle still includes a plurality of reinforcements, the reinforcement is followed extending direction's both ends respectively with adjacent two the screw kuppe meets.
Optionally, at least two of the stiffeners are arranged between two adjacent propeller fairings.
Optionally, the reinforcement is provided in the form of a plate.
Optionally, the outer wall of the reinforcement member is fixedly provided with a reinforcing rib.
Optionally, the extending direction of the reinforcing rib is consistent with the extending direction of the reinforcing member.
Optionally, the reinforcement member is internally hollow.
Optionally, the propeller fairings are arranged in a ring shape, and extension lines of the reinforcing members are tangent to the two propeller fairings respectively.
Optionally, the stiffener is disposed at an end of the propeller pod remote from the frame body.
Optionally, the reinforced toy unmanned aerial vehicle is provided with two wing assemblies on two sides of the frame main body respectively, the wing assemblies on two sides are symmetrically arranged along the front and back direction of the frame main body, and the reinforced toy unmanned aerial vehicle comprises four reinforcing members which are arranged between the adjacent propeller fairings respectively.
Optionally, each of the arms is detachably connected to the rack body.
The utility model discloses technical scheme is through installing each screw respectively in corresponding independent screw kuppe to prevent that the screw from receiving external colliding with and causing the damage, further extension end through the reinforcement meets with two screw kuppes respectively, in order to connect each independent screw kuppe combination as a whole, so, the guarantee of each screw operation environment no longer is subject to single screw kuppe, effectively improves the steadiness of reinforcement type toy unmanned aerial vehicle structure.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
Fig. 1 is the structural schematic diagram of an embodiment of the reinforced toy unmanned aerial vehicle.
The reference numbers illustrate:
| reference numerals | Name (R) | Reference numerals | Name (R) |
| 1 | Frame |
2 | |
| 21 | |
22 | |
| 23 | Propeller air guide sleeve | 3 | Reinforcing |
| 31 | Reinforced rib |
The objects, features and advantages of the present invention will be further described with reference to the accompanying drawings.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying 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 in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.
It should be noted that, if directional indications (such as upper, lower, left, right, front and rear … …) are involved in the embodiment of the present invention, the directional indications are only used to explain the relative position relationship between the components, the motion situation, etc. in a specific posture (as shown in the drawings), and if the specific posture is changed, the directional indications are changed accordingly.
In addition, if there is a description relating to "first", "second", etc. in the embodiments of the present invention, the description of "first", "second", etc. is for descriptive purposes only and is 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 at least one such feature. In addition, the technical solutions in the embodiments may be combined with each other, but it must be based on the realization of those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the combination of the technical solutions should not be considered to exist, and is not within the protection scope of the present invention.
The utility model provides a reinforcement type toy unmanned aerial vehicle.
In the embodiment of the present invention, as shown in fig. 1, the reinforced toy unmanned aerial vehicle includes: the aircraft comprises a rack main body 1 and a plurality of wing assemblies 2 arranged on two sides of the rack main body 1, wherein each wing assembly 2 comprises a machine arm 21 connected with the rack main body 1, a propeller air guide sleeve 23 arranged at one end of the machine arm 21 far away from the rack main body 1 and a propeller 22 arranged in the propeller air guide sleeve 23, and a gap is reserved between the propeller air guide sleeves 23; wherein the content of the first and second substances,
reinforcement type toy unmanned aerial vehicle still includes a plurality of reinforcements 3, and reinforcement 3 meet with two adjacent screw kuppe 23 respectively along extending direction's both ends.
It can be understood that, besides the propeller fairings 23 and the propellers 22, the end of the horn 21 away from the frame body 1 is also provided with batteries and wires connected with the propellers 22 to drive the corresponding propellers 22 to take off rotationally; the rack body 1 is internally defined with an installation space for installing a control circuit board, specifically, in order to better reduce the weight of the reinforced toy unmanned aerial vehicle and avoid the battery from doing too much useless work to overcome the weight, the horn 21 is a hollow structural member, it should be noted that the design is not limited thereto, and in other embodiments, the horn 21 may also be a solid structure made of a light material, which is not limited thereto.
In this embodiment, the propeller fairwater 23 is disposed in a ring shape, and the wall of the propeller fairwater 23 extends in the vertical direction, so that the propeller fairwater 23 can provide a safe operation space for the propeller 22 besides guiding the airflow generated by the propeller 22, of course, the design is not limited thereto, and in other embodiments, the propeller fairwater 23 may be disposed in a rectangular shape or other closed shapes, which is not limited thereto; without loss of generality, the reinforcing member 3 is designed in a strip shape, and two extending ends of the reinforcing member are fixedly connected to the outer wall of the adjacent propeller air guide sleeve 23 respectively, so that the independent propeller air guide sleeves 23 are connected through the reinforcing member 3 to form a combined body, and the structural stability of the propeller air guide sleeves 23 is greatly improved.
Alternatively, each of the arms 21 is detachably attached to the housing main body 1. It can be understood that reinforcement type toy unmanned aerial vehicle's frame main part 1 and the integration of wing subassembly 2 can lead to the product volume too big, are unfavorable for the user to save and transport the product, and when wing subassembly 2 was impaired, also can't simply replace the repair, lead to the maintenance cost too high, and the combination can be dismantled between wing and frame main part 1, provides convenience for the storage of product, transportation and part replacement.
The utility model discloses technical scheme is through installing each screw 22 respectively in corresponding independent screw kuppe 23 to prevent that screw 22 from receiving external colliding with and causing the damage, further extension end through reinforcement 3 meets with two screw kuppe 23 respectively, in order to connect each independent screw kuppe 23 to combine into a whole, so, the guarantee of each screw 22 operation environment no longer is subject to single screw kuppe 23, effectively improves the steadiness of reinforcement type toy unmanned aerial vehicle structure.
Alternatively, the reinforcement 3 is provided in the form of a plate. It can be understood that under the same length, the structural characteristics of the plate shape enable the plate to have lighter mass compared with a cylinder or other shapes, so that the reinforced type toy unmanned aerial vehicle can be effectively prevented from doing excessive gravity useless work during takeoff; without loss of generality, the inside of the reinforcing member 3 is arranged in a hollow manner, so that the whole structure of the reinforcing member 3 is lighter.
Optionally, at least two stiffeners 3 are disposed between two adjacent propeller fairings 23. It can be understood that, by adopting the design, the connection between the two propeller fairings 23 is more firm, and the outer surface wall of the reinforcing piece 3 is fixedly provided with the reinforcing rib 31; it is easy to understand that the reinforcing rib is a reinforcing structure widely adopted in the prior art, and the reinforcing rib 31 is additionally arranged on the outer surface wall of the reinforcing member 3, so that the structural strength of the reinforcing member 3 can be effectively improved; specifically, the extending direction of strengthening the muscle 31 is unanimous with the extending direction of reinforcement 3, so set up, makes reinforcement 3 can bear more and is come from perpendicular self length direction's ascending power, has increased the anti ability of breaking of reinforcement 3.
Optionally, the propeller fairings 23 are arranged in a ring shape, and the extension lines of the stiffeners 3 are tangent to the two propeller fairings 23 respectively. In this embodiment, the propeller fairing 23 includes an outer protection ring and an inner mounting ring coaxially disposed and connected by a connecting arm, the inner mounting ring is used for being mounted and fixed on one end of the horn 21 far away from the frame body 1, and the outer protection ring is used for forming a space for the propeller 22 to safely operate; it can be understood that the connection line of the points between the circles is the longest distance of the common tangent line, and the extension line of the reinforcement 3 is tangent to the two outer protection rings, that is, the reinforcement 3 is disposed in the direction of the longest distance between the two outer protection rings, so that the reinforcement 3 can maximally stabilize the structure of the two propeller fairings 23. Specifically, the reinforcing member 3 is arranged at one end of the propeller air guide sleeve 23 far away from the frame main body 1. It is easy to understand, when daily use, the collision that frame main part 1 end and external environment were kept away from to screw kuppe 23 is the most frequent, and is impaired also comparatively serious, and screw kuppe 23 is located to reinforcement 3 keeps away from frame main part 1 end, makes the interest of reinforcement 3 can reach the maximize and handle.
Optionally, reinforced toy unmanned aerial vehicle is equipped with two wing subassemblies 2 respectively in frame main part 1 both sides, and the wing subassembly 2 of both sides is arranged to the symmetry around frame main part 1, and reinforced toy unmanned aerial vehicle is including locating four reinforcements 3 between adjacent screw kuppe 23 respectively. It can be understood that, when assembling the product, each horn 21 may be installed in the frame body 1, then the propeller fairings 23 and the propellers 22 are installed at the ends of the horns 21 far away from the frame body 1, and finally the four stiffeners 3 are sequentially connected with the outer walls of the propeller fairings 23, thereby completing the installation steps.
The above only is the preferred embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structure changes made by the contents of the specification and the drawings under the inventive concept of the present invention, or the direct/indirect application in other related technical fields are included in the patent protection scope of the present invention.
Claims (10)
1. A ruggedized toy drone, comprising: the aircraft comprises a rack main body and a plurality of wing assemblies arranged on two sides of the rack main body, wherein each wing assembly comprises a machine arm connected with the rack main body, a propeller air guide sleeve arranged at one end of the machine arm far away from the rack main body and a propeller arranged in the propeller air guide sleeve, and a gap is reserved between the propeller air guide sleeves; wherein the content of the first and second substances,
reinforcement type toy unmanned aerial vehicle still includes a plurality of reinforcements, the reinforcement is followed extending direction's both ends respectively with adjacent two the screw kuppe meets.
2. The ruggedized toy drone of claim 1, wherein at least two of the stiffeners are disposed between adjacent propeller fairings.
3. The ruggedized toy drone of claim 1, wherein the reinforcing member is disposed in a plate shape.
4. The reinforced toy drone of claim 3, wherein the outer surface wall of the reinforcing member is fixedly provided with reinforcing ribs.
5. The reinforced toy drone of claim 4, wherein the reinforcing ribs extend in a direction that coincides with the direction of extension of the reinforcing member.
6. The ruggedized toy drone of claim 3, wherein the reinforcement is hollow inside.
7. The ruggedized toy drone of claim 1, wherein the propeller fairings are arranged in a ring shape, and extension lines of the stiffeners are tangent to the two propeller fairings, respectively.
8. The ruggedized toy drone of claim 7, wherein the reinforcement is disposed at an end of the propeller pod distal from the frame body.
9. The reinforced toy unmanned aerial vehicle of claim 8, wherein the reinforced toy unmanned aerial vehicle is provided with two wing assemblies on two sides of the frame body, the wing assemblies on two sides are symmetrically arranged along the front and back direction of the frame body, and the reinforced toy unmanned aerial vehicle comprises four reinforcing members respectively arranged between the adjacent propeller fairings.
10. The ruggedized toy drone of any one of claims 1 to 9, wherein each of the arms is removably connected to the rack body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021272422.1U CN212491546U (en) | 2020-07-03 | 2020-07-03 | Reinforcement type toy unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021272422.1U CN212491546U (en) | 2020-07-03 | 2020-07-03 | Reinforcement type toy unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212491546U true CN212491546U (en) | 2021-02-09 |
Family
ID=74432951
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021272422.1U Active CN212491546U (en) | 2020-07-03 | 2020-07-03 | Reinforcement type toy unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212491546U (en) |
-
2020
- 2020-07-03 CN CN202021272422.1U patent/CN212491546U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101786499B (en) | Impact resistant aircraft leading edge structures and aircraft including the same | |
| CN104340352B (en) | The rear body section of aircraft | |
| CN105905274B (en) | The airframe structure of eight rotor wing unmanned aerial vehicles | |
| CN207346074U (en) | A kind of double shoe VTOL fixed-wing unmanned planes of normal arrangement | |
| US20170369159A1 (en) | Rotary wing aircraft with a fuselage and a non-retractable skid-type landing gear | |
| WO2021136397A1 (en) | Aerial vehicle | |
| CN106628116A (en) | Fixed wing unmanned aerial vehicle | |
| CN113371175A (en) | Fixed wing scouting and hitting integrated unmanned aerial vehicle model and design method thereof | |
| CN212491546U (en) | Reinforcement type toy unmanned aerial vehicle | |
| CN215944856U (en) | Fixed wing scouting and hitting integrated unmanned aerial vehicle model | |
| CN208530842U (en) | Composite rotor aircraft | |
| CN205574251U (en) | Organism is four rotor unmanned aerial vehicle of streamlined | |
| CN210942223U (en) | Duct formula unmanned aerial vehicle | |
| CN110371286A (en) | A kind of manned vehicle | |
| CN108341052A (en) | Composite rotor aircraft | |
| CN212491547U (en) | Light toy unmanned plane | |
| KR102092473B1 (en) | Toy airplane for education | |
| CN214138949U (en) | Novel VTOL fixed wing unmanned aerial vehicle | |
| CN209757494U (en) | Helicopter multifunctional auxiliary flight support and helicopter | |
| CN210618450U (en) | Airplane baseline device | |
| CN210912850U (en) | Unmanned vehicles's fuselage and unmanned vehicles who has it | |
| CN217598816U (en) | High-load unmanned aerial vehicle body | |
| CN208181399U (en) | A kind of general-purpose aircraft tail portion radome fairing | |
| CN214776513U (en) | Left wallboard of light continuous carbon fiber wing | |
| CN218198804U (en) | Unmanned aerial vehicle undercarriage |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |