CN219815270U - Toy aircraft with fight function - Google Patents
Toy aircraft with fight function Download PDFInfo
- Publication number
- CN219815270U CN219815270U CN202320963205.4U CN202320963205U CN219815270U CN 219815270 U CN219815270 U CN 219815270U CN 202320963205 U CN202320963205 U CN 202320963205U CN 219815270 U CN219815270 U CN 219815270U
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- machine body
- wing group
- fight
- aircraft
- battery
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- 230000001681 protective effect Effects 0.000 claims description 13
- 238000000034 method Methods 0.000 abstract description 4
- 230000008054 signal transmission Effects 0.000 abstract description 2
- 230000001174 ascending effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
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Abstract
The utility model discloses a toy aircraft with a fight function, which mainly comprises an aircraft body and rotary wings thereof, wherein the aircraft body is obliquely arranged, an upper rotary wing group and a lower rotary wing group which are parallel to each other are arranged at the upper end and the lower end of the aircraft body, the upper rotary wing group and the lower rotary wing group respectively consist of two pairs of rotary wings which are symmetrically arranged by taking the aircraft body as a central axis, a signal transmitter and a signal receiver are respectively arranged at the two ends of the aircraft body, and the signal transmitter or/and the signal receiver are in rotary connection with the aircraft body. A battery assembly groove and a modularized battery are arranged below the machine body, a clamping groove is arranged in the battery assembly groove, and a clamping strip matched with the clamping groove is arranged on the modularized battery. The utility model adopts a specific inclined machine body, combines the air guide cover to realize air flight and wheelless ground-attached sliding, and additionally adopts signal transmission to realize land, air and other fight modes, so that the playing method is diversified and the interest is stronger.
Description
Technical Field
The utility model belongs to the technical field of toy aircrafts, in particular to a toy aircrafts with a fight function.
Background
The existing toy aircrafts are various, most of the toy aircrafts are derived based on four-axis aircrafts, and all the aircrafts are operated at the motor rotating speeds of rotors at different positions, so that the aircrafts can fly vertically, advance, retreat, turn left or right, and the like. At present, the existing four-axis aircraft is symmetrical and smooth in shape, is particularly suitable for stable flight or suspension in the air, is not suitable for sliding on the ground, and most toys at present pursue an interactive fight function, and if the toys cannot slide on the ground freely, the possibility of land-air fight is further avoided.
Disclosure of Invention
In order to overcome the technical problems, the utility model provides the toy aircraft with the fight function, which can slide in a wheel-free manner by a specific machine body model, further realize the switching of land-air modes and fight, and has more playing methods and strong interactivity.
In order to solve the technical problems, the utility model adopts the following technical scheme:
the utility model provides a toy aircraft with fight function, mainly includes organism and rotor, the organism slope sets up, and both ends are provided with the rotor group that goes up of being parallel to each other and lower rotor group about the organism, go up rotor group and lower rotor group and constitute by two pairs of rotors that use the organism to set up as the axis symmetry respectively, and the both ends of organism are equipped with signal transmitter and signal receiver respectively, and signal transmitter or/and signal receiver and organism form to rotate to be connected.
The battery assembly groove and the modularized battery are arranged below the machine body, the clamping groove is arranged in the battery assembly groove, and the clamping strip matched with the clamping groove is arranged on the modularized battery.
The rotor wing is composed of a protective frame, a propeller and a motor, wherein the protective frame is annularly arranged on the periphery of the propeller, and the motor is positioned below the propeller.
And a guide cover is arranged below the protective frame and extends downwards and vertically along the edge of the protective frame.
The guide cover is arranged on one side of the upper end of the protection frame, which faces the machine body.
The beneficial effects of the utility model are as follows: the special inclined machine body can realize air flight and wheelless ground-attached sliding by combining the air guide cover, can realize various fight modes such as land-land, land-air, air-air and the like by configuring signal transmission, can make the machine body make actions such as swinging, rotating and the like when receiving a striking signal through programming arrangement, and has higher playability and interestingness. In addition, the machine body is provided with the buckle type modularized battery, so that the disassembly and assembly are simple and quick, and the cruising ability is high.
Description of the drawings:
FIG. 1 is a schematic view of the structure of the present utility model in flight;
FIG. 2 is a schematic view of the structure of the ground-engaging slide state in the present utility model;
FIG. 3 is a schematic view of the bottom structure of the present utility model;
FIG. 4 is a schematic diagram of the modular battery assembly of the present utility model;
fig. 5 is a schematic view of the structure of a modularized battery according to the present utility model.
In each drawing, a machine body 1, an upper rotor group 3, a lower rotor group 4, a guide cover 5, a modularized battery 6, a signal transmitter 11, a signal receiver 12, a battery assembly groove 13, a protective frame 21, a propeller 22, a motor 23, a clamping strip 61 and a clamping groove 131 are arranged.
The specific embodiment is as follows:
specific embodiments of the present utility model will be further described below with reference to the accompanying drawings.
As shown in figure 1, the toy aircraft with the fight function comprises an engine body 1 and a rotor wing thereof, and the rotor wing is composed of a protective frame 21, a propeller 22 and a motor 23, wherein the protective frame 21 is annularly arranged on the periphery of the propeller 22, and a plurality of rotor wings can control the rotating speed to push the engine body 1 to finish actions such as ascending, advancing, retreating, left turning, right turning and the like.
Specifically, the machine body 1 is obliquely arranged, the machine body 1 is preferably an oblique shuttle-shaped machine body, the upper end and the lower end of the machine body 1 are provided with an upper rotor wing group 3 and a lower rotor wing group 4 which are parallel to each other, the machine body 1 takes one end which is inclined upwards as the advancing direction, the protective frames 21 in each rotor wing group are all provided with the air guide covers 5, the air guide covers 5 vertically extend downwards along the edges of the protective frames 21, and the air guide covers 5 are arranged on one side of the upper end of the machine body 1, so that when the machine body 1 is placed on the ground, the air guide covers of all the rotor wings support the ground to erect the machine body 1, and when all the rotor wings rotate, wind flows can blow towards one downward inclined end (namely, the rear part when the machine body is prone) of the machine body 1, and the machine body 1 can be pushed to slide forwards.
The upper rotor wing group 3 and the lower rotor wing group 4 are respectively formed by two pairs of rotor wings which are symmetrically arranged by taking the machine body 1 as a central axis, when the upper rotor wing group 3 and the lower rotor wing group 4 adopt the same rotating speed, the machine body 1 can vertically ascend, the machine body 1 keeps a specific inclination angle at the moment, and the upper rotor wing group 3 and the lower rotor wing group 4 are in a horizontal state. After reaching a certain height, if the aircraft needs to advance, retreat or turn, the rotating speed of the motor in different rotors can be directly controlled, and the aircraft has many applications in the prior art in the aerial operation of the aircraft, and the description is omitted here.
When the machine body 1 slides on the ground, as shown in fig. 2, the motor rotation speed of the upper rotor wing set 3 should be lower than that of the lower rotor wing set, so that the machine body 1 can keep the prone form to slide on the ground. In the sliding process, the rotary wing motors on two sides of the upper rotary wing group 3 can be controlled to form a rotary speed difference, and if the rotary speed of the left rotary wing is lower than that of the right rotary wing in the left rotary controllable process, the left rotary can be completed.
The two ends of the machine body 1 are respectively provided with a signal emitter 11 and a signal receiver 12, the signal emitter 11 and the signal receiver 12 can adopt an infrared emitter and a receiver, the signal emitter and the signal receiver 12 are connected with a control circuit in the machine body 1, a person skilled in the art can set the control circuit through a program, when the signal receiver 12 receives an external signal, the control circuit enables the machine body 1 to perform actions such as swinging, rotating and the like by adjusting the rotating speed difference of each rotor wing.
In order to enable the two bodies to generate and receive signals at any angle, the signal transmitter 11 or/and the signal receiver 12 are rotatably connected with the body 1, that is, the signal transmitter 11 or the signal receiver 12 can be rotatably connected with the body 1, or the signal transmitter 11 and the signal receiver 12 can be rotatably connected with the body 1. The signal emitter 11 is preferably connected with the machine body 1 in an axial manner, so that the emission angle of the signal emitter 11 can be manually adjusted according to the requirement before a war, and the signal emitter 11 or the signal receiver 12 can be driven by a motor to rotate, so that automatic adjustment is realized, and the real-time fight function of the two machine bodies in the air and the air, the ground and the ground can be met.
As shown in fig. 3 to 5, a battery assembly groove 13 and a modularized battery 6 are arranged below the machine body, two sides of the battery assembly groove 13 are provided with slide ways for the modularized battery 6 to slide and insert, a clamping groove 131 is arranged in the battery assembly groove 13, a clamping strip 61 matched with the clamping groove 131 is arranged on the modularized battery 6, when the modularized battery 6 slides from one end of the battery assembly groove 13 to the other end, the modularized battery 6 is contacted with a power supply end of a control circuit in the machine body 1, the clamping strip 61 enters the clamping groove 131 to be fixed, and the modularized battery 6 can be removed by reverse pushing, so that the battery replacement is fast and convenient.
While the above-described preferred embodiments according to the present utility model have been shown and described, various changes and modifications can be made by one skilled in the art without departing from the spirit of the utility model. The technical scope of the present utility model is not limited to the description, but must be determined according to the scope of claims.
Claims (5)
1. Toy aircraft with fight function mainly includes organism and rotor, its characterized in that: the machine body is obliquely arranged, an upper rotor wing group and a lower rotor wing group which are parallel to each other are arranged at the upper end and the lower end of the machine body, the upper rotor wing group and the lower rotor wing group are respectively composed of two pairs of rotor wings which are symmetrically arranged by taking the machine body as a central axis, a signal transmitter and a signal receiver are respectively arranged at the two ends of the machine body, and the signal transmitter or/and the signal receiver are rotationally connected with the machine body.
2. A toy aircraft with a fight function according to claim 1, characterized in that: the battery assembly groove and the modularized battery are arranged below the machine body, the clamping groove is arranged in the battery assembly groove, and the clamping strip matched with the clamping groove is arranged on the modularized battery.
3. A toy aircraft with fight function according to claim 1 or 2, characterized in that: the rotor consists of a protective frame, a propeller and a motor, wherein the protective frame is annularly arranged on the periphery of the propeller, and the motor is positioned below the propeller.
4. A toy aircraft with a fight function according to claim 3, characterized in that: a guide cover is arranged below the protective frame and extends downwards and vertically along the edge of the protective frame.
5. A toy aircraft with a fight function according to claim 4, wherein: the air guide sleeve is arranged on one side of the upper end of the machine body, which faces the protection frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320963205.4U CN219815270U (en) | 2023-04-18 | 2023-04-18 | Toy aircraft with fight function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320963205.4U CN219815270U (en) | 2023-04-18 | 2023-04-18 | Toy aircraft with fight function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219815270U true CN219815270U (en) | 2023-10-13 |
Family
ID=88245141
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320963205.4U Active CN219815270U (en) | 2023-04-18 | 2023-04-18 | Toy aircraft with fight function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219815270U (en) |
-
2023
- 2023-04-18 CN CN202320963205.4U patent/CN219815270U/en active Active
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