CN207274972U - A kind of mini four-axle aircraft - Google Patents
A kind of mini four-axle aircraft Download PDFInfo
- Publication number
- CN207274972U CN207274972U CN201721252135.2U CN201721252135U CN207274972U CN 207274972 U CN207274972 U CN 207274972U CN 201721252135 U CN201721252135 U CN 201721252135U CN 207274972 U CN207274972 U CN 207274972U
- Authority
- CN
- China
- Prior art keywords
- fuselage
- motor
- mini
- axle aircraft
- flight wing
- 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
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of mini four-axle aircraft, the flight wing being connected including fuselage and with fuselage, its structural feature are that flight wing is flexibly connected with fuselage, flight wing inwardly fastens, flight wing is equipped with motor and accommodates column, and motor accommodates in column and is equipped with motor, and motor is connected with screw blade, motor accommodates and is connected with retaining frame on column, control panel is equipped with the fuselage, control panel controls the rotation of motor, and control panel is wirelessly connected with remote controler;The beneficial effects of the utility model are:Design is reasonable, and simple in structure, build is smaller, and flight wing can fold, and reduces occupied space, convenient collection, avoids the damage to screw blade.
Description
Technical field
The utility model belongs to flying toy field, and in particular to be a kind of mini four-axle aircraft.
Background technology
Four-axle aircraft is also known as quadrotor, four-rotor helicopter, referred to as four axis, quadrotor.This four-axle aircraft
It is a kind of multi-rotor aerocraft.Four propellers of four-axle aircraft are all the simple mechanisms of motor direct-connected, criss-cross layout
Aircraft is allowed to obtain the power of main body turning by varying motor speed, so that itself posture is adjusted, because its intrinsic complexity
Property, large-scale four-axle aircraft is had no precedent, and existing aircraft is more troublesome in collection and transport, be easy to cause wind
The damage of leaf.
Utility model content
In order to solve the above technical problems, a kind of build of the utility model offer is less, easily collect, will not be to spiral
Blade causes the mini four-axle aircraft of damage.
To achieve the above object, the technical solution adopted in the utility model is a kind of mini four-axle aircraft, including machine
Body and the flight wing being connected with fuselage, its structural feature are that flight wing is flexibly connected with fuselage, and flight wing inwardly fastens, flight
Wing is equipped with motor receiving column, and motor accommodates and motor is equipped with column, and motor is connected with screw blade, and motor accommodates activity on column and connects
Retaining frame is connected to, control panel is equipped with the fuselage, control panel controls the rotation of motor, and control panel is wirelessly connected with remote controler.
As further improvement of the utility model, remote controler is equipped with control button and buckle, and buckle adaptation is connected with
Handset bracket, remote controler is interior to be equipped with electric power storage transformer.
As further improvement of the utility model, fuselage is equipped with LED light, and LED light is connected with control panel.
As further improvement of the utility model, flight wing is four, and four flight wings are set around fuselage array.
As further improvement of the utility model, fuselage is equipped with camera, and camera is wirelessly connected with mobile phone.
As further improvement of the utility model, fuselage is built-in with storage battery, and storage battery becomes with the electric power storage in remote controler
Depressor connects.
As further improvement of the utility model, fuselage is equipped with gyroscope.
The beneficial effects of the utility model are:Design is reasonable, and simple in structure, build is smaller, and flight wing can fold,
Reduce occupied space, convenient collection, avoids the damage to screw blade.
Brief description of the drawings
Fig. 1 is the airframe structure schematic diagram of the utility model;
Fig. 2 is the remote controller structure schematic diagram of the utility model;
Wherein, 1- fuselages, 2- flight wings, 3- motors accommodate column, 4- screw blades, 5- retaining frames, 6- control buttons, 7- cards
Button, 8-LED lamps.
Embodiment
Explanation is further explained to the utility model below in conjunction with the accompanying drawings, but does not limit the protection model of the utility model
Enclose.
As shown in Figure 1 to Figure 2, a kind of mini four-axle aircraft, including fuselage 1 and the flight wing 2 that is connected with fuselage 1,
Flight wing 2 is flexibly connected with fuselage 1, and flight wing 2 inwardly fastens, and flight wing 2 is equipped with motor and accommodates column 3, and motor is accommodated in column 3
Equipped with motor, motor is connected with screw blade 4, and motor accommodates and retaining frame 5 is connected with column 3, and control is equipped with the fuselage 1
Making sheet, control panel control the rotation of motor, and control panel is wirelessly connected with remote controler;The remote controler is equipped with control button 6
With buckle 7, the adaptation of buckle 7 is connected with handset bracket, electric power storage transformer is equipped with remote controler;The fuselage 1 is equipped with LED light
8, LED light 8 is connected with control panel;The flight wing 2 is four, and four flight wings 2 are set around 1 array of fuselage;Described
Fuselage 1 is equipped with camera, and camera is wirelessly connected with mobile phone;The fuselage 1 is built-in with storage battery, storage battery and remote controler
Interior electric power storage transformer connection;The fuselage 1 is equipped with gyroscope;The utility model employs gyroscope technology and 2.4G frequencies
Section.
The technological core of the utility model can realize folding for flight wing, its control panel, circuit structure, gyroscope technology
It is no difference with existing aircraft with 2.4G frequency ranges, can be by being commercially available, therefore, it is can realize.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and
And in the case of the spirit or essential attributes without departing substantially from the utility model, it can realize that this practicality is new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this practicality is new
The scope of type is indicated by the appended claims rather than the foregoing description, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are embraced therein, and any reference numeral in claim should not be considered as limitation
Involved claim.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical solution, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (7)
1. a kind of mini four-axle aircraft, including fuselage and the flight wing that is connected with fuselage, it is characterised in that:The flight
Wing is flexibly connected with fuselage, and flight wing inwardly fastens, and flight wing is equipped with motor and accommodates column, and motor accommodates in column and is equipped with motor,
Motor is connected with screw blade, and motor accommodates and retaining frame is connected with column, and control panel, control panel control are equipped with the fuselage
The rotation of motor processed, control panel are wirelessly connected with remote controler.
A kind of 2. mini four-axle aircraft according to claim 1, it is characterised in that:The remote controler is equipped with control
Button and buckle processed, buckle adaptation are connected with handset bracket, electric power storage transformer are equipped with remote controler.
A kind of 3. mini four-axle aircraft according to claim 1, it is characterised in that:The fuselage is equipped with LED
Lamp, LED light are connected with control panel.
A kind of 4. mini four-axle aircraft according to claim 1, it is characterised in that:The flight wing is four,
Four flight wings are set around fuselage array.
A kind of 5. mini four-axle aircraft according to claim 1, it is characterised in that:The fuselage is equipped with shooting
Head, camera are wirelessly connected with mobile phone.
A kind of 6. mini four-axle aircraft according to claim 1, it is characterised in that:The fuselage is built-in with electric power storage
Pond, storage battery are connected with the electric power storage transformer in remote controler.
A kind of 7. mini four-axle aircraft according to claim 1, it is characterised in that:The fuselage is equipped with gyro
Instrument.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721252135.2U CN207274972U (en) | 2017-09-27 | 2017-09-27 | A kind of mini four-axle aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721252135.2U CN207274972U (en) | 2017-09-27 | 2017-09-27 | A kind of mini four-axle aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
CN207274972U true CN207274972U (en) | 2018-04-27 |
Family
ID=61988085
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201721252135.2U Expired - Fee Related CN207274972U (en) | 2017-09-27 | 2017-09-27 | A kind of mini four-axle aircraft |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN207274972U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115138081A (en) * | 2022-08-01 | 2022-10-04 | 董群法 | Children toy |
-
2017
- 2017-09-27 CN CN201721252135.2U patent/CN207274972U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN115138081A (en) * | 2022-08-01 | 2022-10-04 | 董群法 | Children toy |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2017016096A1 (en) | Novel vertical take-off and landing aircraft and control method therefor | |
CN204355275U (en) | There is the aircraft of safe propulsion system | |
CN207274972U (en) | A kind of mini four-axle aircraft | |
CN107364572A (en) | Fixed-wing vector unmanned plane | |
CN108820229A (en) | Hybrid power unmanned plane based on computer mode control | |
CN105711830B (en) | A kind of two axial vector balancing flap tiltrotor aircrafts | |
CN103112587A (en) | Aircraft | |
CN2759542Y (en) | Electromotive toy helicopter | |
CN205524954U (en) | Four -rotor aircraft | |
CN104111615A (en) | Miniature four-rotor aircraft based on mixed signal processor (MSP) 430F5310 single chip microcomputer | |
CN207045728U (en) | Fixed-wing vector unmanned plane | |
CN207221332U (en) | A kind of spherical four-axle aircraft | |
CN208963310U (en) | It is a kind of can VTOL vert the fixed-wing unmanned plane of quadrotor | |
CN209553496U (en) | A kind of four axis aircrafts | |
CN206900647U (en) | A kind of more rotors of combined type are tethered at UAS | |
CN206900643U (en) | A kind of agricultural spraying unmanned plane | |
CN108116675A (en) | It can VTOL and the long continuation of the journey electric airplane device of hovering | |
CN206664920U (en) | A kind of telescopic energy-saving unmanned plane of support | |
CN208198817U (en) | A kind of twin-engined quadrotor drones | |
CN209809519U (en) | Fingertip gyroscope type unmanned plane | |
CN202315309U (en) | Model plane | |
CN203355289U (en) | Triaxial flying device | |
CN207507007U (en) | A kind of rectangular four-axle aircraft | |
CN209700935U (en) | A kind of antiwind unmanned plane | |
CN203753395U (en) | Large-wingspan electric glider |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180427 Termination date: 20180927 |
|
CF01 | Termination of patent right due to non-payment of annual fee |