CN206871354U - Portable four-axle aircraft - Google Patents
Portable four-axle aircraft Download PDFInfo
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- CN206871354U CN206871354U CN201720740948.XU CN201720740948U CN206871354U CN 206871354 U CN206871354 U CN 206871354U CN 201720740948 U CN201720740948 U CN 201720740948U CN 206871354 U CN206871354 U CN 206871354U
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- accommodating groove
- axle aircraft
- aircraft
- support
- portable
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Abstract
The utility model discloses a kind of portable four-axle aircraft, include aircraft body, rotor and the support for installing rotor, two relative sides of the aircraft body correspond to be provided with accommodating groove respectively, described support one end is articulated with the both ends of the accommodating groove, and the support is located in accommodating groove toward the extreme position that accommodating groove direction rotates.The beneficial effect of this programme is：In off working state, by four holder pivots of four-axle aircraft in the accommodating groove of aircraft body side, four-axle aircraft need not be dismantled, the space hold with regard to four-axle aircraft can be greatly reduced, improve the portability and ease of use of four-axle aircraft.
Description
Technical field
Four-axle aircraft field is the utility model is related to, especially relates to a kind of portable four-axle aircraft.
Background technology
Four-axle aircraft (Quadrotor) is a kind of multi-rotor aerocraft, and also known as quadrotor, four rotors are gone straight up to
Machine, referred to as four axles, four rotors.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 changing motor speed, so as to adjust itself posture.Have benefited from microcomputer in recent years
The development of electric control technology, stable four-axle aircraft have obtained extensive concern, and application prospect is very considerable.
But the support of existing four-axle aircraft is fixedly installed on outside aircraft body, user is carrying the flight of four axles
The support of four different directions needs very big accommodation space when device, the problem of producing transportation inconvenience.
Utility model content
In order to solve the defects of above-mentioned prior art, the purpose of this utility model is to provide a kind of portable four axles flight
Device, the difficulty of user's transportation four-axle aircraft can be reduced.
To reach above-mentioned purpose, the technical solution of the utility model is：
A kind of portable four-axle aircraft, include aircraft body, rotor and the support for installing rotor, it is described to fly
Two relative sides of row device main body correspond to be provided with accommodating groove respectively, and described support one end is articulated with the both ends of the accommodating groove,
The support is located in accommodating groove toward the extreme position that accommodating groove direction rotates.
Further, in addition to it is used for the groove lid for covering the accommodating groove, it is left that the groove lid is articulated with corresponding accommodating groove
Right flank.
Further, the groove lid surface sets anti-skid bulge.
Further, the anti-skid bulge is arranged on the upper surface of the groove lid, and the anti-skid bulge includes a plurality of phase
The tread plate that neighbour be arranged in parallel.
Further, the anti-skid bulge is anti-slip rubber, and the anti-skid bulge is fixedly arranged on the surface of the groove lid.
Further, the storage slot length is more than the length of two supports, and the width of the accommodating groove is more than institute
State the width that support is mounted with the rotor.Further,
The beneficial effects of the utility model are：In off working state, by four holder pivots of four-axle aircraft in place
In in the accommodating groove of aircraft body side, without being dismantled to four-axle aircraft, with regard to four-axle aircraft can be greatly reduced
Space hold, improve the portability and ease of use of four-axle aircraft.
Brief description of the drawings
Fig. 1 is a kind of structural representation of portable four-axle aircraft collapsed state of the embodiment of the utility model one；
Fig. 2 is the view that the embodiment groove lid of the utility model one is opened；
Fig. 3 is a kind of structural representation of portable four-axle aircraft working condition of the embodiment of the utility model one.
Reference：
The groove lid of 10 aircraft body 20
The support of 21 anti-skid bulge 30
40 rack shafts
Embodiment
To illustrate thought and purpose of the present utility model, the utility model is done below in conjunction with the drawings and specific embodiments
Further instruction.
Reference picture 1- Fig. 3, a kind of portable four-axle aircraft, include aircraft body 10, rotor and revolved for installing
The support 30 of the wing, two relative sides of aircraft body 10 are corresponded to be provided with accommodating groove respectively, and the one end of support 30 is turned by support
Axle 40 is articulated with the both ends of accommodating groove, and support 30 is located in accommodating groove toward the extreme position that accommodating groove direction rotates.
Specifically, portable four-axle aircraft also includes being used for the groove lid 20 for covering accommodating groove, groove lid 20 is articulated with correspondingly
Accommodating groove left and right side.Groove lid 20 is used to close corresponding receipts accommodating groove, when support 30 and the rotor on support 30
When turning to the accommodation space in accommodating groove, or, support 30 and rotor rotational on support 30 are in running order
When, groove lid 20 closes, and forms closing space with accommodating groove, support 30 can be limited in accommodating groove.
Specifically, the two sides of groove lid 20 are provided with the rotary shaft of outwardly convex, the adjacent side in side where rotary shaft with
A certain distance between rotary shaft be present, chute is correspondingly provided with the side of accommodating groove, rotary shaft can be limited in sliding groove
The slip of system, when rotary shaft is in chute ad-hoc location, rotary shaft can be rotated in the position.
Specifically, the surface of groove lid 20 sets anti-skid bulge 21, anti-skid bulge 21 is arranged at the upper surface of groove lid 20, anti-skidding convex
21 tread plates for including a plurality of adjacent, parallel setting are played, user is acted in groove lid 20 when opening groove lid 20 by using power
Anti-skid bulge 21, then push out, drive groove lid 20 to be displaced outwardly by caused frictional force between anti-skid bulge 21
Certain distance, groove lid 20 is then rotated, the opening of groove lid 20 is can be achieved with, the closing of groove lid 20 can also be realized in turn.
Anti-skid bulge 21 is anti-slip rubber, and anti-skid bulge 21 is fixedly arranged on the surface of groove lid 20, the coefficient of friction of anti-slip rubber
It is higher, the friction for promoting the rotary shaft of groove lid 20 to be slided in chute enough can be produced in the case of same pressing force
Power.
The length that slot length is more than two supports 30 is stored, the width of accommodating groove is more than the width that support 30 is mounted with rotor
Degree, for store homonymy carry rotor two supports 30 when, will not because of storage slot length it is inadequate, it is mutual to there is support 30
The situation of interference.
This programme beneficial effect is：In off working state, four supports 30 of four-axle aircraft are rotate in place in winged
In the accommodating groove of the side of row device main body 10, without being dismantled to four-axle aircraft, with regard to four-axle aircraft can be greatly reduced
Space hold, improve the portability and ease of use of four-axle aircraft.
Preferred embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model,
Every equivalent structure made using the utility model specification and accompanying drawing content or equivalent flow conversion, or directly or indirectly fortune
Used in other related technical areas, similarly it is included in scope of patent protection of the present utility model.
Claims (6)
1. a kind of portable four-axle aircraft, include aircraft body, rotor and the support for installing rotor, its feature and exist
In two relative sides of the aircraft body correspond to be provided with accommodating groove respectively, and described support one end is articulated with the storage
The both ends of groove, the support are located in accommodating groove toward the extreme position that accommodating groove direction rotates.
2. portable four-axle aircraft as claimed in claim 1, it is characterised in that also include being used to cover the accommodating groove
Groove lid, the groove lid are articulated with corresponding accommodating groove left and right side.
3. portable four-axle aircraft as claimed in claim 2, it is characterised in that the groove lid surface sets anti-skid bulge.
4. portable four-axle aircraft as claimed in claim 3, it is characterised in that the anti-skid bulge is arranged on the groove lid
Upper surface, the anti-skid bulge include the tread plate of a plurality of adjacent, parallel setting.
5. the portable four-axle aircraft as described in claim 3 or 4, it is characterised in that the anti-skid bulge is anti-slip rubber,
The anti-skid bulge is fixedly arranged on the surface of the groove lid.
6. portable four-axle aircraft as claimed in claim 1, it is characterised in that the storage slot length is more than described in two
The length of support, the width of the accommodating groove are more than the width that the support is mounted with the rotor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720740948.XU CN206871354U (en) | 2017-06-23 | 2017-06-23 | Portable four-axle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720740948.XU CN206871354U (en) | 2017-06-23 | 2017-06-23 | Portable four-axle aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206871354U true CN206871354U (en) | 2018-01-12 |
Family
ID=61334281
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720740948.XU Active CN206871354U (en) | 2017-06-23 | 2017-06-23 | Portable four-axle aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206871354U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109484633A (en) * | 2018-11-15 | 2019-03-19 | 中南大学 | Collapsible mobile unmanned plane |
-
2017
- 2017-06-23 CN CN201720740948.XU patent/CN206871354U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109484633A (en) * | 2018-11-15 | 2019-03-19 | 中南大学 | Collapsible mobile unmanned plane |
| CN109484633B (en) * | 2018-11-15 | 2020-05-08 | 中南大学 | Collapsible portable unmanned aerial vehicle |
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