CN206552259U - A kind of with protecting cover four-axle aircraft - Google Patents
A kind of with protecting cover four-axle aircraft Download PDFInfo
- Publication number
- CN206552259U CN206552259U CN201720158378.3U CN201720158378U CN206552259U CN 206552259 U CN206552259 U CN 206552259U CN 201720158378 U CN201720158378 U CN 201720158378U CN 206552259 U CN206552259 U CN 206552259U
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- CN
- China
- Prior art keywords
- cover
- low protection
- protection cover
- protective cover
- motor
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Abstract
The utility model provides a kind of with protecting cover four-axle aircraft, the centre position of low protection cover is equipped with installing frame, two side positions of installing frame are fixed with motor placing tube, main body is assemblied in the inside of installing frame, the inside of motor placing tube is provided with motor, lower fixed cylinder is installed on the upside of low protection cover, the axis of lower fixed cylinder is arranged perpendicular to the plane where low protection cover, the upper end of low protection cover is provided with protective cover, strengthening rib strip is distributed with upper protective cover, protection to blade is realized with low protection cover by the upper protective cover of addition, the design solves conventional aircraft the problem of easily blade is broken during flight, and the design of upper fixed column and lower fixed cylinder is then easy to be attached upper protective cover and low protection cover, realize that on the one hand connection can ensure the intensity of connection by eight upper fixed columns, still further aspect can disperse suffered impulsive force when colliding, the design of other motor placing tube is then easy to change motor.
Description
Technical field
The utility model is a kind of with protecting cover four-axle aircraft, belongs to aircraft devices field.
Background technology
In the prior art, aircraft press application field, can be divided into it is military with it is civilian.Military aspect, aircraft is divided into scouting
Machine and target drone.Civilian aspect, aircraft+sector application is that aircraft has really just been needed；At present taking photo by plane, agricultural, plant protection, oneself
Bat, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, video display
The application in romance etc. field is shot, manufactured, the purposes of aircraft in itself has greatly been expanded, developed country is also actively extending
Sector application and development vehicle technology, with the progress in epoch, aircraft is also begun to as toy by called optical imaging, still
There is the problem of blade is easily damaged in traditional aircraft, this just brings unnecessary trouble to player's play activity, so
A kind of new equipment is needed to carry out final result above mentioned problem.
Utility model content
In view of the deficienciess of the prior art, the utility model purpose is to provide a kind of with protecting cover four-axle aircraft,
To solve the problems mentioned in the above background technology, the utility model is easy to use, is easy to operation, and stability is good, and reliability is high.
To achieve these goals, the utility model is to realize by the following technical solutions：It is a kind of with protecting cover
Four-axle aircraft, including upper protective cover, upper fixed column, lower fixed cylinder, low protection cover, installing frame, motor placing tube, reinforcement
Bar, main body, motor and blade, the centre position of the low protection cover are equipped with installing frame, two side positions of the installing frame
Motor placing tube is fixed with, the main body is assemblied in the inside of installing frame, and the inside of the motor placing tube is provided with motor, institute
State motor to be installed together with blade, lower fixed cylinder is installed on the upside of low protection cover, the axis of the lower fixed cylinder is vertical
It is arranged in the plane where low protection cover, the upper end of the low protection cover is provided with protective cover, the upper protective cover
Strengthening rib strip is distributed with, the lower end of the upper protective cover is provided with fixed column, and fixed post is assemblied in lower fixed cylinder
Together, the edge of the upper protective cover and low protection cover passes through chamfered.
Further, the specification that the motor placing tube is provided with four and four motor placing tubes is identical.
Further, the specification that the lower fixed cylinder is provided with eight and eight lower fixed cylinders is identical.
Further, it is distributed in the specification phase that the upper fixed column on the downside of protective cover is provided with eight and eight upper fixed columns
Together.
Further, the lower position of the low protection cover is equipped with rubber blanket.
Further, battery is distributed with the inside of the main body.
The beneficial effects of the utility model：A kind of with protecting cover four-axle aircraft of the present utility model, by addition
Protective cover realizes the protection to blade with low protection cover, and the design solves conventional aircraft during flight easily by leaf
The problem of piece is broken, the strengthening rib strip being additionally disposed on protective cover serves the purpose for strengthening upper protective cover bulk strength, prevents
The situation for only causing protective cover to damage when being collided with other articles occurs, and the design of upper fixed column and lower fixed cylinder is then just
It is attached in upper protective cover and low protection cover, realizes that on the one hand connection can ensure the strong of connection by eight upper fixed columns
Degree, still further aspect can disperse when colliding suffered by impulsive force, the design of motor placing tube in addition is then easy to pair
Motor is changed, and the utility model is easy to use, is easy to operation, and stability is good, and reliability is high.
Brief description of the drawings
By reading the detailed description made with reference to the following drawings to non-limiting example, other spies of the present utility model
Levy, objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural representation of with protecting cover four-axle aircraft of the utility model；
Fig. 2 is the structural representation of low protection cover in a kind of with protecting cover four-axle aircraft of the utility model；
In figure：Fixed cylinder, 4- low protection covers, 5- installing frames, 6- motors are placed under the upper protective covers of 1-, the upper fixed columns of 2-, 3-
Cylinder, 7- strengthening rib strips, 8- main bodys, 9- motors, 10- blades.
Embodiment
To be easy to understand technological means, creation characteristic, reached purpose and effect of the utility model realization, below
With reference to embodiment, the utility model is expanded on further.
Fig. 1 and Fig. 2 are referred to, the utility model provides a kind of technical scheme：A kind of with protecting cover four-axle aircraft, bag
Include protective cover 1, upper fixed column 2, lower fixed cylinder 3, low protection cover 4, installing frame 5, motor placing tube 6, strengthening rib strip 7, main body
8th, motor 9 and blade 10, the centre position of low protection cover 4 are equipped with installing frame 5, and two side positions of installing frame 5 are fixed with electricity
Machine placing tube 6, main body 8 is assemblied in the inside of installing frame 5, and the inside of motor placing tube 6 is provided with motor 9, motor 9 and blade 10
It is installed together, the upside of low protection cover 4 is provided with lower fixed cylinder 3, and the axis of lower fixed cylinder 3 is perpendicular to the institute of low protection cover 4
Plane be arranged, the upper end of low protection cover 4, which is provided with protective cover 1, upper protective cover 1, is distributed with strengthening rib strip 7, on
The lower end of protective cover 1 is provided with fixed column 2, and upper fixed column 2 is assembled together with lower fixed cylinder 3, upper protective cover 1 and lower protection
The edge of cover 4 passes through chamfered, realizes the protection to blade 10 with low protection cover 4 by the upper protective cover 1 of addition, the design
Conventional aircraft is solved the problem of easily blade 10 is broken during flight, the reinforcement on protective cover 1 is additionally disposed in
Rib 7 serves the purpose for strengthening the upper bulk strength of protective cover 1, prevents from causing protective cover 1 to damage when colliding with other articles
Bad situation occurs.
The specification that motor placing tube 6 is provided with four and four motor placing tubes 6 is identical, and lower fixed cylinder 3 is provided with eight
And the specification of eight lower fixed cylinders 3 is identical, the upper fixed column 2 for being distributed in the downside of protective cover 1 is provided with eight and eight above admittedly
The specification of fixed column 2 is identical, and the design of upper fixed column 2 and lower fixed cylinder 3 is then easy to connect upper protective cover 1 and low protection cover 4
Connect, realize that on the one hand connection can ensure the intensity of connection by eight upper fixed columns 2, still further aspect can collide
When disperse suffered impulsive force, the design of motor placing tube 6 in addition is then easy to change motor 9, under low protection cover 4
Side position is equipped with rubber blanket, and battery is distributed with the inside of main body 8.
Embodiment：In progress in use, staff first is checked the utility model, check whether and deposit
In defect, it can not just carry out using if there is defect, now need to notify maintenance personal to be repaired, if do not deposited
It can be carried out using if problem, in use, carrying out charging operations, charging complete to the battery inside main body 8 first
Blade 10 is fixed on to the upper end of motor 9 afterwards, then by the lower fixation in the upper fixed column 2 on upper protective cover 1 and low protection cover 4
Cylinder 3 is assembled together, and then realizes fixed purpose, now, you can flight operation is carried out, if this practicality during this
New to be collided with ground or other objects, upper protective cover 1 and low protection cover 4 serve the effect of protection, and then can be with
The effective situation for preventing blade 10 from damaging occurs, and upper protective cover 1 and the edge of low protection cover 4 use the design of chamfering can be with addition
Effectively play a part of disperses impact forces, prevent user's collision rift from causing the injured situation of user to occur in addition.
General principle of the present utility model and principal character and advantage of the present utility model has been shown and described above, for
For those skilled in the art, it is clear that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, embodiment all should be regarded as exemplary, and be nonrestrictive, scope of the present utility model is by institute
Attached claim rather than described above are limited, it is intended that will fall in the implication and scope of the equivalency of claim
All changes are included in the utility model.Any reference in claim should not be considered as to the right involved by limitation
It is required that.
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 scheme, this narrating mode of specification is only that for clarity, those skilled in the art should
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It may be appreciated other embodiment.
Claims (6)
1. a kind of with protecting cover four-axle aircraft, including upper protective cover, upper fixed column, lower fixed cylinder, low protection cover, installation
Frame, motor placing tube, strengthening rib strip, main body, motor and blade, it is characterised in that：The centre position dress of the low protection cover
Equipped with installing frame, two side positions of the installing frame are fixed with motor placing tube, and the main body is assemblied in the inside of installing frame, institute
The inside for stating motor placing tube is provided with motor, and the motor is installed together with blade, is provided with down on the upside of low protection cover
Fixed cylinder, the axis of the lower fixed cylinder is arranged perpendicular to the plane where low protection cover, the low protection cover it is upper
End, which is provided with protective cover, the upper protective cover, is distributed with strengthening rib strip, and the lower end of the upper protective cover is provided with fixation
Post, fixed post is assembled together with lower fixed cylinder, and the edge of the upper protective cover and low protection cover passes through chamfered.
2. a kind of with protecting cover four-axle aircraft according to claim 1, it is characterised in that：The motor placing tube is set
The specification for being equipped with four and four motor placing tubes is identical.
3. a kind of with protecting cover four-axle aircraft according to claim 1, it is characterised in that：The lower fixed cylinder is set
There is the specification of eight and eight lower fixed cylinders identical.
4. a kind of with protecting cover four-axle aircraft according to claim 1, it is characterised in that：It is distributed under protective cover
The specification that the upper fixed column of side is provided with eight and eight upper fixed columns is identical.
5. a kind of with protecting cover four-axle aircraft according to claim 1, it is characterised in that：Under the low protection cover
Side position is equipped with rubber blanket.
6. a kind of with protecting cover four-axle aircraft according to claim 1, it is characterised in that：The interior part of the main body
It is furnished with battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720158378.3U CN206552259U (en) | 2017-02-21 | 2017-02-21 | A kind of with protecting cover four-axle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720158378.3U CN206552259U (en) | 2017-02-21 | 2017-02-21 | A kind of with protecting cover four-axle aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206552259U true CN206552259U (en) | 2017-10-13 |
Family
ID=60360554
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720158378.3U Expired - Fee Related CN206552259U (en) | 2017-02-21 | 2017-02-21 | A kind of with protecting cover four-axle aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206552259U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108058823A (en) * | 2018-01-26 | 2018-05-22 | 湖州职业技术学院 | A kind of unmanned plane rotor protective device |
-
2017
- 2017-02-21 CN CN201720158378.3U patent/CN206552259U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108058823A (en) * | 2018-01-26 | 2018-05-22 | 湖州职业技术学院 | A kind of unmanned plane rotor protective device |
| CN108058823B (en) * | 2018-01-26 | 2024-05-10 | 湖州职业技术学院 | Unmanned aerial vehicle rotor wing protection device |
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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 |
Granted publication date: 20171013 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |