CN207221332U - A kind of spherical four-axle aircraft - Google Patents
A kind of spherical four-axle aircraft Download PDFInfo
- Publication number
- CN207221332U CN207221332U CN201721252138.6U CN201721252138U CN207221332U CN 207221332 U CN207221332 U CN 207221332U CN 201721252138 U CN201721252138 U CN 201721252138U CN 207221332 U CN207221332 U CN 207221332U
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- motor
- spherical
- control panel
- fuselage
- axle aircraft
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Abstract
The utility model discloses a kind of spherical four-axle aircraft, including base and fuselage, its structural feature is that fuselage is equipped with the flight wing that can be closed or open upwards downwards, and flight wing is equipped with extension tongue, the end for extending tongue accommodates column equipped with the motor of plane downward vertically with extending tongue, motor accommodates and motor is equipped with column, and motor is connected with fan blade, and control panel is equipped with the fuselage, control panel can control the rotation of motor, and control panel is wirelessly connected with remote controler;The beneficial effects of the utility model are:Design is reasonable, simple in structure, can reduce collection space, and prevents that fan blade is damaged, increases service life.
Description
Technical field
The utility model belongs to flying toy field, and in particular to be a kind of spherical 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, the utility model provide it is a kind of can fold, reduce collection space, prevent wind
The spherical four-axle aircraft of leaf damage.
To achieve the above object, the technical solution adopted in the utility model is a kind of spherical four-axle aircraft, including base
And fuselage, its structural feature are, fuselage is equipped with the flight wing that can be closed or open upwards downwards, and flight wing is equipped with extension
Tongue, the end for extending tongue accommodate column equipped with the motor of plane downward vertically with extending tongue, and motor accommodates in column and is equipped with motor, electric
Machine is connected with fan blade, is equipped with control panel in the fuselage, control panel can control 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.
As further improvement of the utility model, base 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, flight wing is equipped with protection ring, and protection ring will extend tongue around setting.
As further improvement of the utility model, storage battery is equipped with base, storage battery and motor and control panel are linear
Connection.
The beneficial effects of the utility model are:Design is reasonable, simple in structure, can reduce collection space, and prevent wind
Leaf is damaged, increases service life.
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- bases, 2- fuselages, 3- flight wings, 4- extension tongues, 5- motors receiving column, 6- fan blades, 7- control buttons,
8- is buckled, 9- handset brackets, 10-LED lamps, 11- protection rings.
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 spherical four-axle aircraft, including base 1 and fuselage 2, the fuselage 2 are equipped with
The flight wing 3 that can be closed or open upwards downwards, flight wing 3 are equipped with extension tongue 4, and the end of extension tongue 4 is equipped with and extension
The motor of the plane of tongue 4 downward vertically accommodates column 5, and motor accommodates in column 5 and is equipped with motor, and motor is connected with fan blade 6, the machine
Control panel is equipped with body 2, control panel can control the rotation of motor, and control panel is wirelessly connected with remote controler;The remote controler
Control button 7 and buckle 8 are equipped with, the adaptation of buckle 8 is connected with handset bracket 9;The base 1 is equipped with LED light 10, LED
Lamp 10 is connected with control panel;The flight wing 3 is four, and four flight wings 3 are set around 2 array of fuselage;The flight
Wing 3 is equipped with protection ring 11, and protection ring 11 will extend tongue 4 around setting;Be equipped with storage battery in the base 1, storage battery and
Motor and control panel linearly connected.
The utility model can close flight wing 3 downwards in collection, and charge to storage battery, and when in use, can
Flight wing 3 is opened upwards, and can be set by control panel and realize that a key returns and the flight of upset, the utility model are adopted
With gyroscope technology and 2.4G frequency ranges.
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 (6)
1. a kind of spherical four-axle aircraft, including base and fuselage, it is characterised in that:The fuselage is equipped with and can close downwards
The flight wing for closing or opening upwards, flight wing are equipped with extension tongue, and the end for extending tongue lets droop equipped with the plane with extending tongue
Straight motor accommodates column, and motor accommodates and motor is equipped with column, and motor is connected with fan blade, and control panel is equipped with the fuselage, controls
Making sheet can control the rotation of motor, and control panel is wirelessly connected with remote controler.
A kind of 2. spherical four-axle aircraft according to claim 1, it is characterised in that:The remote controler is equipped with control
Button and buckle, buckle adaptation are connected with handset bracket.
A kind of 3. spherical four-axle aircraft according to claim 1, it is characterised in that:The base is equipped with LED light,
LED light is connected with control panel.
A kind of 4. spherical four-axle aircraft according to claim 1, it is characterised in that:The flight wing be four, four
A flight wing is set around fuselage array.
A kind of 5. spherical four-axle aircraft according to claim 1, it is characterised in that:The flight wing is equipped with protection
Ring, protection ring will extend tongue around setting.
A kind of 6. spherical four-axle aircraft according to claim 1, it is characterised in that:Electric power storage is equipped with the base
Pond, storage battery and motor and control panel linearly connected.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721252138.6U CN207221332U (en) | 2017-09-27 | 2017-09-27 | A kind of spherical four-axle aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721252138.6U CN207221332U (en) | 2017-09-27 | 2017-09-27 | A kind of spherical four-axle aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
CN207221332U true CN207221332U (en) | 2018-04-13 |
Family
ID=61864503
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201721252138.6U Expired - Fee Related CN207221332U (en) | 2017-09-27 | 2017-09-27 | A kind of spherical four-axle aircraft |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN207221332U (en) |
-
2017
- 2017-09-27 CN CN201721252138.6U patent/CN207221332U/en not_active Expired - Fee Related
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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: 20180413 Termination date: 20200927 |