CN205971802U - Collapsible four shaft air vehicle - Google Patents
Collapsible four shaft air vehicle Download PDFInfo
- Publication number
- CN205971802U CN205971802U CN201620835189.0U CN201620835189U CN205971802U CN 205971802 U CN205971802 U CN 205971802U CN 201620835189 U CN201620835189 U CN 201620835189U CN 205971802 U CN205971802 U CN 205971802U
- Authority
- CN
- China
- Prior art keywords
- axle
- aircraft
- column spinner
- collapsible
- parallel lines
- 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
Abstract
The utility model relates to a collapsible four shaft air vehicle contains body and four axles, and body internally mounted has can dismantle storage battery, the body front end is provided with two preceding axle beds that are in same parallel lines, the body rear end is provided with two back axle beds that are in same parallel lines, the one end of axle is provided with the column spinner, the axle is connected with the body on installing in the front axle bed or back axle bed through the column spinner. The beneficial effects of the utility model are that, a collapsible four shaft air vehicle is provided, the wing is the state that staggers just can be folded, and folding the incorporation behind the body, the body is in balanced state with all wings, a similar helicopter, the appearance is pleasing to the eye, is different from other aircraft simultaneously, can reduce storage space, portable by a wide margin.
Description
Technical field
This utility model is related to foldable four-axle aircraft.
Background technology
Four-axle aircraft, also known as quadrotor, four-rotor helicopter, referred to as four axles, four rotors.Four-axle aircraft is
A kind of multi-rotor aerocraft.Four propellers of four-axle aircraft are all the simple mechanisms of motor direct-connected, and criss-cross layout permits
Permitted aircraft to pass through to change the power that motor speed obtains main body turning, thus adjusting itself attitude.
The form of four-axle aircraft on the market is all fixing at present, and four axles cannot be carried out folding, and is like this receiving
Can seem greatly very much inconvenient due to area occupied when Tibetan, meanwhile, existing four-axle aircraft intelligently keeps a kind of form, holds
It is also easy to produce visual fatigue.
Utility model content
This utility model provides a kind of foldable four-axle aircraft, to solve the above problems.
In order to solve above-mentioned technical problem, the technical solution adopted in the utility model is as follows：
A kind of foldable four-axle aircraft, containing body and four axles, body interior is provided with detachable savings battery, institute
State body front end and be provided with two front axle beds being in same parallel lines, described body rear end be provided with two be in same parallel
The rear axle bed of line, one end of described axle is provided with column spinner, described axle by column spinner be arranged on front axle bed or rear axle bed with
Body is connected.
Further, the other end of described axle is provided with the motor of propeller, and described motor is provided with display lamp.
Further, described body interior is provided with aircraft head, and described aircraft head lower surface is provided with shooting
Head.
Further, described body upper surface is provided with radiating gap.
Further, described body bottom portion is provided with support feet.
Similar to helicopter front end geometry, body is provided with before and after's axle bed to above-mentioned utility model body shape, in front and back axle bed
Position be not at same parallel lines, described column spinner can rotate freely after being arranged on axle bed, thus carrying moving axis to be revolved
Turn, when aircraft not flight, four axles can rotate simultaneously and can be simultaneously overlapping be placed in rear body, meanwhile, body bottom portion
It is provided with support feet, during folded state, look like a helicopter.
The other end of axle is provided with motor, motor carries propeller, is provided with red green display lamp, redness represents quiet simultaneously
Only state, green represents state of flight.
Body interior is provided with aircraft head, and described aircraft head lower surface is provided with photographic head, aircraft head
Make photographic head be in three-axis stabilization state, make that video camera shooting effect is more stable, picture becomes apparent from.
The beneficial effects of the utility model are to provide a kind of foldable four-axle aircraft, and wing is staggered like state and permissible
Fold, fold after being incorporated in body, body and all of wing are in poised state, a similar helicopter, good looking appearance, with
When be different from other aircraft, accommodation space can be greatly decreased, be easy to carry.
Brief description
Fig. 1 is this utility model structural representation；
Fig. 2 is this utility model rounding state structural representation.
Specific embodiment
As shown in Figure 1 and Figure 2, a kind of foldable four-axle aircraft, containing body 1 and four axles 2, is provided with inside body 1
Detachable savings battery, described body 1 front end is provided with two front axle beds 3 being in same parallel lines, and described body rear end sets
It is equipped with two rear axle beds 4 being in same parallel lines, one end of described axle 2 is provided with column spinner 21, described axle 2 passes through column spinner
21 are arranged on and are connected with body 1 on front axle bed 3 or rear axle bed 4, and the other end of described axle 2 is provided with the motor of propeller
22, on described motor, 22 are provided with display lamp, and described body 1 is internally provided with aircraft head 5, under described aircraft head 5
Surface is provided with photographic head, and described body 1 upper surface is provided with radiating gap, and described body 1 bottom is provided with support feet 6.
Claims (5)
1. a kind of foldable four-axle aircraft, containing body and four axles, body interior is provided with detachable savings battery, and it is special
Levy and be：Described body front end is provided with two front axle beds being in same parallel lines, and described body rear end is provided with two
In the rear axle bed of same parallel lines, one end of described axle is provided with column spinner, described axle by column spinner be arranged on front axle bed or
It is connected with body on axle bed afterwards.
2. aircraft according to claim 1 it is characterised in that：The other end of described axle is provided with the electricity of propeller
Machine, described motor is provided with display lamp.
3. aircraft according to claim 1 it is characterised in that：Described body interior is provided with aircraft head, described
Aircraft head lower surface is provided with photographic head.
4. aircraft according to claim 1 it is characterised in that：Described body upper surface is provided with radiating gap.
5. aircraft according to claim 1 it is characterised in that：Described body bottom portion is provided with support feet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620835189.0U CN205971802U (en) | 2016-08-04 | 2016-08-04 | Collapsible four shaft air vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620835189.0U CN205971802U (en) | 2016-08-04 | 2016-08-04 | Collapsible four shaft air vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205971802U true CN205971802U (en) | 2017-02-22 |
Family
ID=58028820
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620835189.0U Expired - Fee Related CN205971802U (en) | 2016-08-04 | 2016-08-04 | Collapsible four shaft air vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205971802U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110944856A (en) * | 2017-07-17 | 2020-03-31 | 意大利乔治亚罗设计公司 | Automobile capable of being converted into rotorcraft |
-
2016
- 2016-08-04 CN CN201620835189.0U patent/CN205971802U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110944856A (en) * | 2017-07-17 | 2020-03-31 | 意大利乔治亚罗设计公司 | Automobile capable of being converted into rotorcraft |
| CN110944856B (en) * | 2017-07-17 | 2023-07-18 | 意大利乔治亚罗设计公司 | Automobile convertible into rotorcraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170222 Termination date: 20190804 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |