CN206068125U - Unmanned plane housing - Google Patents
Unmanned plane housing Download PDFInfo
- Publication number
- CN206068125U CN206068125U CN201621091759.6U CN201621091759U CN206068125U CN 206068125 U CN206068125 U CN 206068125U CN 201621091759 U CN201621091759 U CN 201621091759U CN 206068125 U CN206068125 U CN 206068125U
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- fuselage
- unmanned plane
- groove
- inner bottom
- bottom part
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Abstract
This utility model is related to unmanned air vehicle technique field, refers in particular to a kind of unmanned plane housing；This utility model includes the fuselage of carbon fiber, fuselage inner bottom part forms multiple bracket grooves, bracket groove is formed by the fin of two parallel carbon fibers, the one end open of bracket groove, other end closing, two fin protrudes from fuselage inner bottom part, one end of two fins is joined together to form blind end, and the inner top correspondence of fuselage forms multiple bracket grooves；Bracket groove and fuselage paste more stable, and control device is installed on horizontal support, due to horizontal support, longitudinal carrier, bracket groove fitting tight, so control device also ensure that stability, improve the total quality of unmanned plane product.
Description
Technical field
This utility model is related to unmanned air vehicle technique field, refers in particular to a kind of unmanned plane housing.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Can be divided into from technical standpoint definition：Unmanned fixed-wing aircraft, unmanned VTOL machine, unmanned airship, nobody
Helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..
Unmanned plane press application, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.The people
With aspect, unmanned plane combines sector application, is the real firm need of unmanned plane；At present taking photo by plane, agricultural, plant protection, auto heterodyne, express delivery transport
Defeated, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture
The application in romance etc. field, has greatly expanded the purposes of unmanned plane itself, and developed country is also in actively extension sector application
With development unmanned air vehicle technique.
Existing unmanned plane, its central interior mainly install control board and relevant apparatus, these interior arrangements
Mounting stability, can also affect the using effect of unmanned plane, and at present, general unmanned plane is mainly pasted in center inner bottom part and propped up
Frame, is then installed on control device on support, and this stability for pasting support is not strong, for a long time using unmanned plane, uses
Effect will be affected.
Therefore, the defect based on above-mentioned existing unmanned plane housing, needs to be improved existing unmanned plane housing.
The content of the invention
The purpose of this utility model is to provide a kind of unmanned plane housing, the unmanned plane housing for the deficiencies in the prior art
Solve existing for existing unmanned plane：The control device stability defect such as not enough.
For achieving the above object, this utility model is achieved through the following technical solutions：Unmanned plane housing, including carbon fibre
The fuselage of dimension, fuselage inner bottom part form multiple bracket grooves, and bracket groove is formed by the fin of two parallel carbon fibers, bracket groove
One end open, other end closing, two fins protrude from fuselage inner bottom part, and one end of two fins is joined together to form envelope
Closed end, the inner top correspondence of fuselage form multiple bracket grooves.
Inner bottom part circumferentially shape distribution of the bracket groove around fuselage.
Also there is in fuselage the longitudinal carrier of carbon fiber, longitudinal carrier is inserted in the support of corresponding inner top, inner bottom part
Between groove, longitudinal carrier has multiple vacancy portions in stair shape.
Also there is in fuselage horizontal support, horizontal support has lap buckle, and lap buckle is inserted in the vacancy portion of longitudinal carrier.
Horn inner bottom part has horn groove, and horn groove is formed by two fins, and horn groove is extended to by the inner bottom part of fuselage
The external tapping of horn, radial direction molding of the horn groove along fuselage.
The beneficial effects of the utility model are：Bracket groove pastes more stable with fuselage, and control device is installed on and laterally props up
On frame, due to horizontal support, longitudinal carrier, bracket groove fitting tight, so control device also ensure that stability, improve
The total quality of unmanned plane product.
Description of the drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is internal structure schematic diagram of the present utility model.
Close-up schematic views of the Fig. 3 for Fig. 2.
Specific embodiment
Below in conjunction with the accompanying drawings this utility model is further described.
Seeing Fig. 1 --- Fig. 3, this utility model unmanned plane housing include：Fuselage 1, upper lid 2, horn 3, bracket groove 4, horn
Groove 5.
Fuselage of the present utility model 1, upper lid 2, horn 3 all adopt carbon fiber to make, and total quality is very light.
1 inner bottom part of fuselage of the present utility model forms multiple bracket grooves 4, and bracket groove 4 is formed by two parallel fins,
The one end open of bracket groove 4, other end closing, two fins protrude from 1 inner bottom part of fuselage, and one end of two fins is connected to one
Rise and form blind end, the inner top of fuselage 1 forms multiple bracket grooves 4, the bracket groove 4 of inner top molding and the support of inner bottom part
Groove 4 is symmetrical.
Inner bottom part circumferentially shape distribution of the bracket groove of the present utility model 4 around fuselage 1.
Also there is in fuselage of the present utility model 1 longitudinal carrier, longitudinal carrier is inserted in corresponding inner top, inner bottom part
Between bracket groove 4, longitudinal carrier has multiple vacancy portions in stair shape.
Also there is in fuselage of the present utility model 1 horizontal support, horizontal support has lap buckle, and lap buckle is inserted in longitudinal direction
The vacancy portion of support.
Fin of the present utility model all adopts carbon fibre material to make.
Longitudinal carrier of the present utility model, horizontal support are flat board and directly are punched to be formed, and all adopt carbon fiber material
Material makes.
3 inner bottom part of horn of the present utility model has horn groove 5, and horn groove 5 is formed by two fins, and horn groove 5 is by machine
The inner bottom part of body 1 extends to the external tapping of horn 3, radial direction molding of the horn groove 5 along fuselage 1.
This utility model all adopts carbon fibre material, bracket groove 4 to paste more stable with fuselage, and control device is installed on laterally
On support, due to horizontal support, longitudinal carrier, bracket groove 4 fitting tight, so control device also ensure that stability,
Improve the total quality of unmanned plane product.
Bracket groove of the present utility model 4, horn groove 5 can also play the effect of similar reinforcement, strengthen the strong of fuselage 1
Degree.Further, since be not plane connection between horn 3 and fuselage 1, but curved surface connection, so horn groove 5 is nor flat
Planar.
Upper lid 1 is corresponding with the middle part of the inner bottom of fuselage 1, is plane, by the external tapping of multiple horns 3 in the middle part of the inner bottom of fuselage 1
Center connect to form a central plane, in addition in the middle part of the inner bottom of fuselage 1, the other parts of fuselage 1 and 3 Shi Cheng centers of horn
Plane symmetry, during production and processing, and it is respectively produced the two parts and is pasted and fixed on together again, so bracket groove 4
Processing is simultaneously uncomplicated.
This utility model simple structure, stability in the large are strong.
Certainly, the embodiment of the above, simply preferred embodiments of the present utility model, not limit this utility model
Practical range, therefore the equivalence changes done of all constructions according to described in this utility model claim, feature and principle or repair
Decorations, all should be included in this utility model claim.
Claims (5)
1. unmanned plane housing, it is characterised in that：Including the fuselage of carbon fiber, fuselage inner bottom part forms multiple bracket grooves, support
Groove is formed by the fin of two parallel carbon fibers, and the one end open of bracket groove, other end closing, two fins protrude from fuselage
Inner bottom part, one end of two fins are joined together to form blind end, and the inner top correspondence of fuselage forms multiple bracket grooves.
2. unmanned plane housing according to claim 1, it is characterised in that：Bracket groove around the inner bottom part of fuselage, circumferentially divide by shape
Cloth.
3. unmanned plane housing according to claim 1, it is characterised in that：Also there is in fuselage the longitudinal carrier of carbon fiber,
Longitudinal carrier is inserted between the bracket groove of corresponding inner top, inner bottom part, and longitudinal carrier has multiple vacancy portions in stair shape.
4. unmanned plane housing according to claim 3, it is characterised in that：Also there is in fuselage horizontal support, horizontal support
With lap buckle, lap buckle is inserted in the vacancy portion of longitudinal carrier.
5. unmanned plane housing according to claim 1, it is characterised in that：Horn inner bottom part has a horn groove, horn groove by
Two fin is formed, and horn groove is extended to the external tapping of horn, radial direction molding of the horn groove along fuselage by the inner bottom part of fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621091759.6U CN206068125U (en) | 2016-09-29 | 2016-09-29 | Unmanned plane housing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621091759.6U CN206068125U (en) | 2016-09-29 | 2016-09-29 | Unmanned plane housing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206068125U true CN206068125U (en) | 2017-04-05 |
Family
ID=58439307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621091759.6U Active CN206068125U (en) | 2016-09-29 | 2016-09-29 | Unmanned plane housing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206068125U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107936801A (en) * | 2017-12-20 | 2018-04-20 | 长沙盾甲新材料科技有限公司 | A kind of anti abrasive unmanned plane housing |
| CN111959743A (en) * | 2020-08-21 | 2020-11-20 | 南京航空航天大学 | Bionic unmanned aerial vehicle body bearing structure |
-
2016
- 2016-09-29 CN CN201621091759.6U patent/CN206068125U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107936801A (en) * | 2017-12-20 | 2018-04-20 | 长沙盾甲新材料科技有限公司 | A kind of anti abrasive unmanned plane housing |
| CN111959743A (en) * | 2020-08-21 | 2020-11-20 | 南京航空航天大学 | Bionic unmanned aerial vehicle body bearing structure |
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