CN206336424U - A kind of hidden folds unmanned plane - Google Patents
A kind of hidden folds unmanned plane Download PDFInfo
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- CN206336424U CN206336424U CN201621484596.8U CN201621484596U CN206336424U CN 206336424 U CN206336424 U CN 206336424U CN 201621484596 U CN201621484596 U CN 201621484596U CN 206336424 U CN206336424 U CN 206336424U
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- unmanned plane
- fuselage
- protective case
- rotor module
- hidden
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Abstract
Unmanned plane is folded the utility model discloses a kind of hidden, belongs to unmanned plane field.A kind of hidden of the present utility model folds unmanned plane, including fuselage and rotor module, drives rotor module to fly by rotor module；The rotor module includes protective case and the propeller in protective case, and the fuselage side wall is provided with cabin, and rotor module is connected by rotary shaft with fuselage, and can be rotated to around rotary shaft in cabin, is completely obscured propeller.The utility model substantially reduces the volume of unmanned plane by way of rotor module is placed in unmanned aerial vehicle body, is favorably improved the portability and disguise of unmanned plane, and with more preferable outward appearance.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, and unmanned plane is folded more specifically to a kind of hidden.
Background technology
UAV is that one kind is manipulated by radio robot or itself presetting apparatus referred to as " unmanned plane "
Unmanned vehicle, 1940s is come across earliest, used as the target drone of military training at that time.Nobody
Machine is widely used, low cost, and efficiency-cost ratio is good；Survival ability is strong, and mobility is good, easy to use, not only has in modern war
Extremely important effect, more holds out broad prospects in civil area.At present, unmanned plane has been widely used guard, city pipe
The field such as reason, agricultural, geology, meteorology, electric power, rescue and relief work, video capture.
In the prior art, the unmanned plane of some fixed-wings may only have a piece of rotor, and the unmanned plane of some helicopter classes can
There can be rotor more than two panels or two panels；From the mechanical property of rotor, every rotor causes surrounding by rotation
Air-flow produces change, so as to form lift, therefore, every rotor is required to the certain separate space of correspondence, to be formed for it
Lift creates conditions.In other words, in existing unmanned plane scheme, rotor occupies the sectional area of the unmanned plane overwhelming majority, returns nothing
Man-machine taking brings inconvenience.
With the development of future technology, unmanned plane is following will turn into everyone daily necessary article as mobile phone.
But the portability of unmanned plane type now and disguise are still waited to improve.Therefore, unmanned plane it is following such as how its portability and
Disguise appears in people at one's side, the technical problem as the current urgent need to resolve of those skilled in the art.
Chinese Patent Application No.：201510472369.7, the applying date：On August 4th, 2015, this application case discloses one kind
Folding unmanned plane, including unmanned plane main body and connected Rotary-Wing Department, the Rotary-Wing Department include having at least one respectively
The first rotor module and the second rotor module of individual rotor, first rotor module and second rotor module are respectively articulated with
In the both sides of the unmanned plane main body, so that both rotate around respective jointed shaft and overlap or deploy.The program enters rotor
Row modularized design, is initially formed two rotor modules that can be overlapped or deploy relatively, then passes through the upset of rotor module
Rotate and realize folding or deploy, to convert the state of unmanned plane, meet folding and the flight demand of unmanned plane, improve unmanned plane
Portability；Circuit and control module needed for unmanned plane etc. can be built in unmanned plane main body, each without being placed in
In individual rotor module.
The program can realize the folding of unmanned plane rotor, to be convenient for carrying, but can directly find out that it revolves in appearance
Wing structure, it is disguised poor, it should not use, need to be further improved in the occasion for needing to hide unmanned plane structure.
Utility model content
1. the utility model technical problem to be solved
The purpose of this utility model is to overcome the shortcomings of that folding unmanned plane is not portable, disguised poor in the prior art,
There is provided a kind of hidden fold unmanned plane, the utility model by way of rotor module is placed in unmanned aerial vehicle body,
The volume of unmanned plane is substantially reduced, the portability and disguise of unmanned plane is favorably improved, and with more preferable aesthetic property,
Abreast of the times aesthetic growth requirement.
2. technical scheme
To reach above-mentioned purpose, the technical scheme that the utility model is provided is：
A kind of hidden of the present utility model folds unmanned plane, including fuselage and rotor module, is driven by rotor module
Rotor module is flown；The rotor module includes protective case and the propeller in protective case, and the fuselage side wall is provided with
Cabin, rotor module is connected by rotary shaft with fuselage, and can be rotated to around rotary shaft in cabin, propeller is hidden completely
Cover.
Further improved as the utility model, described protective case is sector structure, in the two side of protective case
Junction opens up axis hole, and the rotary shaft is rotated with axis hole and is connected.
Further improved as the utility model, the protective case is protected around the rotating range of rotary shaft not less than fan-shaped
The angle of sheath two side.
Further improved as the utility model, the rotary shaft is driven by motor to be rotated.
Further improved as the utility model, the fuselage is provided with double-deck cabin, two cabins of mounted on top
Opening it is opposite.
Further improved as the utility model, the fuselage is rectangular structure, and with two cabins of layer
Opening is identical.
Further improved as the utility model, retaining mechanism is provided with the fuselage, when rotor module rotation
During to state of flight, protective case is locked positioning.
Further improved as the utility model, the retaining mechanism includes projection and the protective case being located on fuselage
On neck, locking positioning is realized by the raised cooperation with neck.
Further improved as the utility model, state, the side wall of protective case are rotated to cabin in rotor module
Overlapped with corresponding fuselage side wall.
3. beneficial effect
The technical scheme provided using the utility model, compared with prior art, is had the advantages that：
(1) a kind of hidden of the present utility model folds unmanned plane, when unmanned plane is in state of flight, rotor module expansion
Outside fuselage, normal working flight can be realized；When unmanned plane is in non-state of flight, rotor module can be drawn in completely
In in cabin, being easy to daily carrying, good concealment, and with more preferable aesthetic property, abreast of the times aesthetic growth requirement；
(2) a kind of hidden of the present utility model folds unmanned plane, and protective case is sector structure, in a non-operative state,
Its side wall preferably can coordinate with fuselage, from hiding internal structure in appearance；And the protection to propeller can be realized, it is real
It is preferable with effect；
(3) a kind of hidden of the present utility model folds unmanned plane, and fuselage is provided with double-deck cabin, two machines of mounted on top
The opening in cabin will not produce interference on the contrary, corresponding rotor is rotated to cabin from opposite direction；In addition, the cabin stacked
The space of propeller occupancy can be substantially reduced, overall volume is reduced, it is easy to carry；
(4) a kind of hidden of the present utility model folds unmanned plane, is rotated using motor driving protective case, it is possible to achieve remote
Process control, reasonable in design, principle is simple, is easy to promote the use of.
Brief description of the drawings
Fig. 1 is the decomposition texture schematic diagram that hidden of the present utility model folds unmanned plane；
Fig. 2 is the structural representation under hidden of the present utility model folding unmanned plane deployed condition；
Fig. 3 is the structural representation under hidden of the present utility model folding unmanned plane rounding state；
Fig. 4 is the internal structure schematic diagram that hidden of the present utility model folds unmanned plane.
Label declaration in schematic diagram：1st, fuselage；2nd, rotor module；201st, protective case；202nd, propeller；203rd, axis hole；
3rd, rotary shaft；4th, cabin.
Embodiment
To further appreciate that content of the present utility model, the utility model is described in detail in conjunction with the accompanying drawings and embodiments.
Embodiment 1
With reference to Fig. 1, a kind of hidden of the present embodiment folds unmanned plane, including fuselage 1 and rotor module 2, can pass through
Rotor module 2 drives rotor module 2 to fly.Specifically, rotor module 2 includes protective case 201 and the spiral shell in protective case 201
Oar 202 is revolved, protective case 201 is sector structure but is not limited to the structure, and axis hole is opened up in the two side junction of protective case 201
The center of 203, i.e. sector structure offers axis hole, rotary shaft 3 is installed in axis hole, for connecting fuselage.
The side wall of fuselage 1 is provided with cabin 4, and the cabin 4 is communicated to fuselage interior, and rotor module 2 passes through rotary shaft 3 and fuselage
1 connection, and can be rotated to around rotary shaft 3 in cabin 4, it is completely obscured propeller 202.
As shown in Fig. 2 under working flight state, rotor module 2 is rotated to outermost end around rotary shaft 3, and propeller 202 is complete
It is naked to be exposed at outside fuselage, normal flight operation can be carried out.
As shown in figure 3, in a non-operative state, rotor module 2 is rotated to cabin around rotary shaft 3, propeller 202 is complete
Be hidden in engine room inside, unmanned plane volume is substantially reduced, is convenient for carrying, and good concealment, from be difficult in appearance directly judgement
For unmanned plane, it can be used in some military scenarios.
Embodiment 2
A kind of hidden of the present embodiment folds unmanned plane, and its basic structure is same as Example 1, and its difference exists
In：Protective case 201 is not less than the angle of the fan-shaped two side of protective case 201 around the rotating range of rotary shaft 3 in the present embodiment, to protect
Demonstrate,proving propeller 202 can be completely exposed, does not influence working flight.
Further, it can also be rotated by motor-driven rotation axle 3, rotor module can directly be controlled by control system
2 expansion, realize remote control.
Embodiment 3
With reference to Fig. 4, a kind of hidden of the present embodiment folds unmanned plane, and its basic structure is same as Example 2, and it is different
Part is：The present embodiment middle fuselage 1 is provided with double-deck cabin 4, and the opening of two cabins 4 of mounted on top is opposite.Mounted on top
Two cabins opening on the contrary, corresponding rotor is rotated to cabin from opposite direction, interference will not be produced.In addition, on
Under the cabin that stacks can be substantially reduced the space of propeller occupancy, reduce overall volume, it is easy to carry.
For the four axle unmanned planes of the present embodiment, fuselage 1 can be rectangular structure, and two cabins 4 of same layer are opened
Mouth is identical.
What deserves to be explained is, the signified rectangular structure of the present embodiment is not entirely limited, however not excluded that fuselage roof or bottom
Portion or side wall are set to the situation of arc, it can be understood as class rectangular structure.In addition, according to the quantity of rotor, corresponding
Fuselage is set to hexagonal prism or other similar structures, within the protection domain of this programme.
Embodiment 4
A kind of hidden of the present embodiment folds unmanned plane, and its basic structure is same as Example 3, and its difference exists
In：In order to realize to rotor module 2 in the positioning of different conditions, spring damping can be set on the rotating shaft, also can be by same
Other modes are locked.The present embodiment is provided with retaining mechanism on the fuselage 1, when rotor module 2 is rotated to state of flight,
Protective case 201 is locked positioning, and retaining mechanism includes being located at the neck on projection and protective case 201 on fuselage 1, passes through projection
Locking positioning is realized in cooperation with neck.
The state to cabin 4 is rotated in rotor module 2, the side wall of protective case 201 is overlapped with the corresponding side wall of fuselage 1, tool
There is more preferable overall aesthetics, also location locking mechanism can be set under the state, prevent rotor module 2 automatic out of cabin
Produce.
Specifically, edge and engine room inside magnet can be added in rotor module in this example, when drawing in, rotor module
It can preferably be fixed in cabin, will not be loosened because of motion, can also add and close in tumbler and rotor module junction
Circuit being closed, detecting whether rotor module is deployed into correct position during for taking off.
The utility model focuses on providing a kind of mechanical structure of hidden unmanned plane, and the flight to unmanned plane controls system
System is not described excessively, can be in body upper or the internal corresponding control system space of setting, without specific when specifically used
Limitation.
Schematically the utility model and embodiments thereof are described above, the description does not have restricted, accompanying drawing
Shown in be also one of embodiment of the present utility model, actual structure is not limited thereto.So, if this area
Those of ordinary skill enlightened by it, do not departing from the case that the utility model creates objective, designed without creative
The frame mode similar to the technical scheme and embodiment, all should belong to protection domain of the present utility model.
Claims (9)
1. a kind of hidden folds unmanned plane, including fuselage (1) and rotor module (2), rotor mould is driven by rotor module (2)
Block (2) flies；It is characterized in that：The rotor module (2) includes protective case (201) and the spiral in protective case (201)
Oar (202), fuselage (1) side wall is provided with cabin (4), and rotor module (2) is connected by rotary shaft (3) with fuselage (1), and
It can be rotated to around rotary shaft (3) in cabin (4), be completely obscured propeller (202).
2. a kind of hidden according to claim 1 folds unmanned plane, it is characterised in that：Described protective case (201) is
Sector structure, axis hole (203) is opened up in the two side junction of protective case (201), and the rotary shaft (3) turns with axis hole (203)
Dynamic connection.
3. a kind of hidden according to claim 2 folds unmanned plane, it is characterised in that：The protective case (201) rotates
The rotating range of moving axis (3) is not less than the angle of fan-shaped protective case (201) two side.
4. a kind of hidden according to claim 2 folds unmanned plane, it is characterised in that：The rotary shaft (3) passes through electricity
Machine driving rotation.
5. unmanned plane is folded according to a kind of hidden according to any one of claims 1 to 4, it is characterised in that：The fuselage
(1) provided with double-deck cabin (4), the opening of two cabins (4) of mounted on top is opposite.
6. a kind of hidden according to claim 5 folds unmanned plane, it is characterised in that：The fuselage (1) is cuboid
Structure, and it is identical with the opening of two cabins (4) of layer.
7. a kind of hidden according to any one of claim 5 folds unmanned plane, it is characterised in that：The fuselage (1)
On be provided with retaining mechanism, when rotor module (2) rotation is to state of flight, protective case (201) is locked positioning.
8. a kind of hidden according to claim 7 folds unmanned plane, it is characterised in that：The retaining mechanism includes being located at
The neck in projection and protective case (201) on fuselage (1), locking positioning is realized by the raised cooperation with neck.
9. a kind of hidden according to claim 7 folds unmanned plane, it is characterised in that：In rotor module (2) rotation extremely
Cabin (4) interior state, the side wall of protective case (201) is overlapped with corresponding fuselage (1) side wall.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621484596.8U CN206336424U (en) | 2016-12-31 | 2016-12-31 | A kind of hidden folds unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621484596.8U CN206336424U (en) | 2016-12-31 | 2016-12-31 | A kind of hidden folds unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN206336424U true CN206336424U (en) | 2017-07-18 |
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ID=59304339
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621484596.8U Expired - Fee Related CN206336424U (en) | 2016-12-31 | 2016-12-31 | A kind of hidden folds unmanned plane |
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| Country | Link |
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| CN (1) | CN206336424U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107963206A (en) * | 2017-12-06 | 2018-04-27 | 佛山市神风航空科技有限公司 | A kind of strength aircraft |
| CN108945419A (en) * | 2018-07-20 | 2018-12-07 | 酷黑科技（北京）有限公司 | A kind of unmanned plane for being suitble to stack and unmanned plane extension and retraction system |
| CN109229368A (en) * | 2018-08-31 | 2019-01-18 | 中国科学院光电研究院 | Hidden autonomous flight miniature drone |
| CN109484633A (en) * | 2018-11-15 | 2019-03-19 | 中南大学 | Collapsible mobile unmanned plane |
| CN114056541A (en) * | 2021-11-02 | 2022-02-18 | 国网安徽省电力有限公司蚌埠供电公司 | Unmanned aerial vehicle with foldable wings |
-
2016
- 2016-12-31 CN CN201621484596.8U patent/CN206336424U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107963206A (en) * | 2017-12-06 | 2018-04-27 | 佛山市神风航空科技有限公司 | A kind of strength aircraft |
| CN108945419A (en) * | 2018-07-20 | 2018-12-07 | 酷黑科技（北京）有限公司 | A kind of unmanned plane for being suitble to stack and unmanned plane extension and retraction system |
| CN109229368A (en) * | 2018-08-31 | 2019-01-18 | 中国科学院光电研究院 | Hidden autonomous flight miniature drone |
| CN109229368B (en) * | 2018-08-31 | 2023-09-19 | 中国科学院光电研究院 | Concealed autonomous flight micro unmanned aerial vehicle |
| 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 |
| CN114056541A (en) * | 2021-11-02 | 2022-02-18 | 国网安徽省电力有限公司蚌埠供电公司 | Unmanned aerial vehicle with foldable wings |
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Legal Events
| Date | Code | Title | Description |
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| 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: 20170718 Termination date: 20201231 |