CN209033742U - A kind of easy assembling type aircraft - Google Patents
A kind of easy assembling type aircraft Download PDFInfo
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- CN209033742U CN209033742U CN201821725660.6U CN201821725660U CN209033742U CN 209033742 U CN209033742 U CN 209033742U CN 201821725660 U CN201821725660 U CN 201821725660U CN 209033742 U CN209033742 U CN 209033742U
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- shell
- dynamic equipment
- assembling type
- easy assembling
- type aircraft
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Abstract
A kind of easy assembling type aircraft, including fuselage and be connected to fuselage two sides left dynamic equipment and right dynamic equipment, left and right two dynamic equipment respectively includes shell, is set to the intracorporal magnet of shell, the driving motor being connected on shell and the propeller driven by driving motor, the magnet of two dynamic equipments is attracting to be fixedly connected on two dynamic equipments on fuselage, and structure is simple, convenient for disassembly and assembly.
Description
Technical field
The utility model relates to toy technique fields, more particularly to a kind of easy assembling type aircraft.
Background technique
Existing toy is varied, there is the toy product for children's design, also there is the toy for adult's design
Product.Wherein, toy airplane is in tool type toy by a kind of popular toy, but the dynamic equipment of existing toy airplane
It is integrated design with fuselage, structure is complicated, dismounting is inconvenient.
Summary of the invention
In view of this, providing the easy assembling type aircraft that a kind of structure is simple, easy to assembly.
A kind of easy assembling type aircraft, including fuselage and be connected to fuselage two sides left dynamic equipment and right dynamic equipment, institute
Left and right two dynamic equipment is stated to respectively include shell, be set to the intracorporal magnet of shell, the driving motor being connected on shell, Yi Jiyou
The propeller of driving motor driving, the magnet of two dynamic equipments is attracting to be fixedly connected on two dynamic equipments on fuselage.
Preferably, the magnet polarities of two dynamic equipment are opposite.
Preferably, the shell includes bottom case and the lid that connect with bottom case, one of the bottom case and lid shape
At have clasp, it is wherein another be formed with button hole, bottom case in being connected by the clasp fastener in corresponding button hole with lid.
Preferably, be provided with electric unit in the shell of one of described left and right two dynamic equipment, the electric unit with
The driving motor of left and right two dynamic equipment connects.
Preferably, the shell of left and right two dynamic equipment is connected by a hinge.
Preferably, the shell has integrally extended to form mounting portion for installing driving motor, the mounting portion is formed with
Around the wind cylinder type protective cover of propeller.
Compared to the prior art, the two dynamic equipment fissions design of the utility model easy assembling type aircraft, then by respectively interior
The strong magnetic pull of the strength magnet in portion is fixed on fuselage two sides, and structure is simple, convenient for disassembly and assembly.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of an embodiment of the utility model easy assembling type aircraft.
Fig. 2 is the structural schematic diagram that easy assembling type aircraft shown in Fig. 1 removes fuselage.
Fig. 3 is the explosive view of the right dynamic equipment of aircraft in Fig. 2.
Fig. 4 is another angular views of Fig. 2.
Fig. 5 is the explosive view of the left dynamic equipment of aircraft in Fig. 4.
Specific embodiment
The utility model is more fully retouched below with reference to relevant drawings for the ease of understanding the utility model,
It states.One or more embodiments of the utility model are illustratively given in attached drawing, so that disclosed in the utility model
The understanding of technical solution is more accurate, thorough.However, it should be understood that the utility model can be with many different forms
To realize, however it is not limited to embodiments described below.
Fig. 1 show a specific embodiment of the utility model easy assembling type aircraft, shown easy assembling type aircraft include fuselage 10,
And it is symmetrically disposed on the left and right dynamic equipment 20,30 of 10 two sides of fuselage.The seperated design of the left and right dynamic equipment 20,30,
Shape, structure are substantially the same.As shown in Figures 4 and 5, the left dynamic equipment 20 include shell 22, be set to it is strong in shell 22
Power magnet 24, the driving motor 26 being installed on shell 22 and the propeller 28 being connect with driving motor 26.Such as Fig. 2 and Fig. 3
Shown, the right dynamic equipment 30 includes shell 32, the strength magnet 34 being set in shell 32, the driving being installed on shell 32
Motor 36 and the propeller 38 being connect with driving motor 36.The left and right dynamic equipment 20,30 passes through strength magnet 24,34
Gravitation is fixed on the two sides of fuselage 10, preferably, the fuselage 10 is formed with the interconnecting piece 12 of thin wall shape, interconnecting piece 12 when assembling
It is inserted between shell 22,32.
The shell 22 of the left dynamic equipment 20 includes bottom case 220 and the lid 221 being connected with bottom case 220, and the two is common
Enclosure space is constituted, strength magnet 24 is accommodated.The bottom case 220 is tabular, and opposite sides side (is illustrated as two sides up and down
Side) it extends perpendicularly outward, it is respectively formed a clasp 222, the corresponding clasp 222 of the lid 221 is respectively formed with button hole 223, group
222 fastener of clasp forms shell 22 in fitting together bottom case 220 and lid 221 in corresponding button hole 223 when dress.It is described
Lid 221 integrally extends outward to form a mounting portion 225, for placing driving motor 26.The propeller 28 and driving motor
26 connections, and the high-speed rotation under its driving generate thrust and drive aircraft flight.Preferably, the mounting portion 225 is also formed with
Around the wind cylinder type protective cover 226 of the propeller 28, in assembling, protective cover 226 can collide aircraft to avoid propeller 28
Fuselage 10；In landing, protective cover 226 first lands aircraft, avoids driving motor 26, propeller 28 etc. and collision on the ground, causes
Damage.
Similar, the 32 of the right dynamic equipment include bottom case 320 and the lid 321 being connected with bottom case 320, wherein bottom case
320 be tabular, and upper and lower two sides, which extend perpendicularly outward, is respectively formed a clasp 323, and the lid 321 forms button hole 323
With 323 phase fastener of clasp, bottom case 320 and lid 321 are fitted together, enclosure space is constituted and accommodates strength magnet 34.Preferably
Ground, the polarity of the strength magnet 24,34 of the left and right dynamic equipment 20,30 on the contrary, the two close to when generate extremely strong magnetic attraction
Left and right dynamic equipment 20,30 is fixed on the two sides of the interconnecting piece 12 of fuselage 10 by power.The lid 321 integrally extends outward to form
One mounting portion 325, for placing driving motor 36.The propeller 38 is connect with driving motor 36, and is generated under its driving
Thrust drives aircraft flight.Preferably, the mounting portion 325 is also formed with the wind cylinder type protective cover around the propeller 38
326。
The setting backwards of shell 22,32 of the left dynamic equipment 20, right dynamic equipment 30, and connected by hinge 40, such as Fig. 3 institute
Show.Preferably, being wherein equipped with electric unit 50 in a shell 22 or 32, electric unit 50 shown in the present embodiment is set to right power
In the shell 22 of device 20, as shown in Figure 5.The electric unit 50 includes but is not limited to power supply, controller etc., by conducting wire and is driven
Dynamic motor 26,36 connects.When assembling, the interconnecting piece 12 of fuselage 10 is placed between shell 22,32 and is located on hinge 40, two
Dynamic equipment 20,30 is located at the arranged on left and right sides of interconnecting piece 12.Then by two housings 22,32 rotate towards each other until bottom case 220,
320 two sides respectively with interconnecting piece 12 are affixed.At this point, the strength magnet 24,34 in shell 220,320 is mutually close and generates powerful
Attraction, two dynamic equipments 20,30 are fixedly connected on interconnecting piece 12, while electric unit 50 connects with two dynamic equipments 20,30
Logical, aircraft can take off at any time.
Two dynamic equipments 20,30 of the utility model easy assembling type aircraft are seperated design, then pass through respectively internal strength
The strong magnetic pull of magnet 24,34 is fixed on 10 two sides of fuselage and powers on, and structure is simple, convenient for disassembly and assembly.It should be noted that
The utility model is not limited to above embodiment, creative spirit according to the present utility model, and those skilled in the art may be used also
To make other variations, these variations done according to the creative spirit of the utility model should all be included in the utility model institute
Within the scope of claimed.
Claims (6)
1. a kind of easy assembling type aircraft, including fuselage and it is connected to the left dynamic equipment and right dynamic equipment of fuselage two sides, it is special
Sign is: left and right two dynamic equipment respectively includes shell, is set to the intracorporal magnet of shell, the driving being connected on shell electricity
Machine and the propeller driven by driving motor, the magnet of two dynamic equipments is attracting to be fixedly connected on two dynamic equipments on fuselage.
2. easy assembling type aircraft as described in claim 1, which is characterized in that the magnet polarities of two dynamic equipment are opposite.
3. easy assembling type aircraft as described in claim 1, which is characterized in that the shell includes bottom case and connect with bottom case
Lid, one of the bottom case and lid be formed with clasp, it is wherein another be formed with button hole, the clasp fastener is in correspondence
Button hole in bottom case is connected with lid.
4. easy assembling type aircraft as described in claim 1, which is characterized in that the shell of one of described left and right two dynamic equipment
It is inside provided with electric unit, the electric unit is connect with the driving motor of left and right two dynamic equipment.
5. easy assembling type aircraft as described in claim 1, which is characterized in that the shell of left and right two dynamic equipment passes through hinge
Connection.
6. easy assembling type aircraft as described in claim 1, which is characterized in that the shell has integrally extended to form mounting portion and has been used for
Driving motor is installed, the mounting portion is formed with the wind cylinder type protective cover around propeller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821725660.6U CN209033742U (en) | 2018-10-24 | 2018-10-24 | A kind of easy assembling type aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821725660.6U CN209033742U (en) | 2018-10-24 | 2018-10-24 | A kind of easy assembling type aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209033742U true CN209033742U (en) | 2019-06-28 |
Family
ID=67038955
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821725660.6U Active CN209033742U (en) | 2018-10-24 | 2018-10-24 | A kind of easy assembling type aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209033742U (en) |
-
2018
- 2018-10-24 CN CN201821725660.6U patent/CN209033742U/en active Active
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