CN203593159U - Multi-purpose unmanned aerial vehicle - Google Patents
Multi-purpose unmanned aerial vehicle Download PDFInfo
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- CN203593159U CN203593159U CN201320612794.8U CN201320612794U CN203593159U CN 203593159 U CN203593159 U CN 203593159U CN 201320612794 U CN201320612794 U CN 201320612794U CN 203593159 U CN203593159 U CN 203593159U
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- cabin
- unmanned plane
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- aerial vehicle
- unmanned aerial
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- 230000000712 assembly Effects 0.000 claims description 6
- 238000000429 assembly Methods 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims description 5
- 238000001514 detection method Methods 0.000 abstract 1
- 238000005516 engineering process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000002917 insecticide Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
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Abstract
The utility model discloses a multi-purpose unmanned aerial vehicle, and belongs to the field of aircrafts. The multi-purpose unmanned aerial vehicle comprises a vehicle body, and a first wing and a second wing that are arranged on the two sides of the vehicle body; the second wing is connected with the vehicle body through a strut arranged between the two sides of the vehicle body; a first cabin is arranged in the vehicle body, and is provided with an upward opening; a mounting platform used for mounting a detecting instrument is arranged in the first cabin. According to the utility model, the mounting platform used for mounting the detecting instrument is arranged in the first cabin of the unmanned aerial vehicle, and the upward opening is formed in the first cabin, so that the detecting instrument can extend out of the cabin through the opening to conduct normal detection. Therefore, the problem of poor stability due to the adoption of a nacelle is avoided, and the flight efficiency of the unmanned aerial vehicle is improved; no extra expenses are needed, so that the cost of the unmanned aerial vehicle is reduced.
Description
Technical field
The utility model relates to aircraft field, particularly a kind of multi-purpose unmanned aerial vehicle.
Background technology
Along with the development of unmanned plane technology, unmanned plane is widely used in geologic prospect, power circuit patrolling, sprays insecticide, forest inspection, nuclear leakage are surveyed and the field such as the disaster relief.Unmanned plane, in the time of operation, need to carry check implement, for example pick up camera and pesticide container.Existing unmanned plane generally adopts gondola to carry check implement, and gondola is arranged on wing below.
Realizing in process of the present utility model, contriver finds that prior art at least exists following problem: gondola mass ratio is larger, and in the time of unmanned plane operation, gondola center of gravity has significantly and moves, and affects the stability of unmanned plane navigation; And the price of gondola is also higher, increase the cost of unmanned plane.
Utility model content
In order to solve the problem of prior art, the utility model embodiment provides a kind of multi-purpose unmanned aerial vehicle.Described technical scheme is as follows:
The utility model embodiment provides a kind of multi-purpose unmanned aerial vehicle, described unmanned plane comprises: body, the first wing that is located at described body both sides and the second wing, described the second wing is connected with described body by the pole being located between described body both sides, in described body, be provided with the first cabin, described the first cabin is upwards provided with opening, and is provided with the erecting bed for installation and measuring instrument in described the first cabin.
Alternatively, described unmanned plane also comprises the 3rd wing, in described body, be also provided with the second cabin, one end of described the 3rd wing is slidably disposed in described the second cabin by slide assemblies, and the other end of described the 3rd wing stretches out outside described the second cabin and is positioned at below described the first wing.
Alternatively, described slide assemblies comprises motor, worm gear and worm screw, described motor is arranged on described the second cabin inwall, the mouth of described motor is connected with one end of described worm screw, the other end of described worm screw is fixed on described the second cabin inwall, the length direction of described worm screw is vertical with the length direction of described the first wing, and described worm gear is arranged on described worm screw, and is connected with one end of described the 3rd wing.
Alternatively, be also provided with the 3rd cabin on described body, described the first cabin is between described the 3rd cabin and described pole.
Alternatively, described unmanned plane also comprises driver train, and described driver train is arranged in described the 3rd cabin.
Alternatively, described unmanned plane also comprises screw propeller, and screw propeller is connected with the mouth of described driver train.
Alternatively, described the second wing is V-shaped.
Alternatively, described unmanned plane also comprises hatchcover, and described hatchcover removably covers on described opening.
Alternatively, described unmanned plane also comprises the alighting gear that is arranged on described organism bottom.
Alternatively, the quantity of described alighting gear is 3.
The beneficial effect that the technical scheme that the utility model embodiment provides is brought is: by the erecting bed of installation and measuring instrument is set in the first cabin of unmanned plane, the first cabin is upwards provided with opening, detecting instrument can lean out cabin by opening and normally detect, like this, avoid adopting the problem of the poor stability that gondola brings, improve the flight efficiency of unmanned plane, and do not needed extra spending, saved the cost of unmanned plane.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme in the utility model embodiment, below the accompanying drawing of required use during embodiment is described is briefly described, apparently, accompanying drawing in the following describes is only embodiment more of the present utility model, for those of ordinary skills, do not paying under the prerequisite of creative work, can also obtain according to these accompanying drawings other accompanying drawing.
Fig. 1 is the structural representation of a kind of multi-purpose unmanned aerial vehicle of providing of the utility model embodiment.
The specific embodiment
For making the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with accompanying drawing, the utility model embodiment is described in further detail.
Embodiment
Referring to Fig. 1-Fig. 3, the utility model embodiment provides a kind of multi-purpose unmanned aerial vehicle, and this unmanned plane comprises:
Alternatively, this unmanned plane also comprises the 3rd wing 6, in body 1, be also provided with the second cabin (scheming not shown), one end of the 3rd wing 6 is slidably disposed in the second cabin by slide assemblies (scheming not shown), and the other end of the 3rd wing 6 stretches out outside the second cabin and is positioned at below the first wing 2.
Alternatively, slide assemblies comprises motor, worm gear and worm screw.Motor is arranged on the second cabin inwall, and the mouth of motor is connected with one end of worm screw, and the other end of worm screw is fixed on the second cabin inwall.The length direction of worm screw is vertical with the length direction of the first wing 2.Worm gear is arranged on worm screw, and is connected with one end of the 3rd wing 6.
Wherein, the 3rd wing 6 can, under the driving of motor, draw in the second cabin (referring to Fig. 1).In the time of unmanned plane during flying, can, according to the demand of unmanned plane load quality and operation, the 3rd wing 6 be skidded off to (referring to Fig. 2) from the second cabin, adopt the 3rd wing 6, can change wing 1ift-drag ratio, make the unmanned plane can heavy-duty flight, can in the time of underloading, reduce again resistance, reduce energy consumption; Can guarantee that the large voyage of High speed and low resistance power cruises, can carry out again low speed high lift-drag ratio and leave a blank.
Alternatively, be also provided with the 3rd cabin on body 1, the first cabin is between the 3rd cabin and pole 4.
Alternatively, unmanned plane also comprises driver train 7 and the screw propeller 8 being connected with the mouth of driver train, and driver train 7 is arranged in the 3rd cabin.
Alternatively, this unmanned plane also comprises hatchcover (scheming not shown), and this hatchcover removably covers on opening.
Alternatively, this unmanned plane also comprises the alighting gear 9 that is arranged on body 1 bottom.The quantity of alighting gear 9 can be 3.
Alternatively, the second wing 3 is V-shaped.
The utility model embodiment by arranging the erecting bed of installation and measuring instrument in the first cabin of unmanned plane, the first cabin is upwards provided with opening, detecting instrument can lean out cabin by opening and normally detect, like this, avoid adopting the problem of the poor stability that gondola brings, improve the flight efficiency of unmanned plane, and do not needed extra spending, saved the cost of unmanned plane.
The foregoing is only preferred embodiment of the present utility model, not in order to limit the utility model, all within spirit of the present utility model and principle, any modification of doing, be equal to replacement, improvement etc., within all should being included in protection domain of the present utility model.
Claims (10)
1. a multi-purpose unmanned aerial vehicle, it is characterized in that, described unmanned plane comprises: body, the first wing that is located at described body both sides and the second wing, described the second wing is connected with described body by the pole being located between described body both sides, in described body, be provided with the first cabin, described the first cabin is upwards provided with opening, and is provided with the erecting bed for installation and measuring instrument in described the first cabin.
2. unmanned plane according to claim 1, it is characterized in that, described unmanned plane also comprises the 3rd wing, in described body, be also provided with the second cabin, one end of described the 3rd wing is slidably disposed in described the second cabin by slide assemblies, and the other end of described the 3rd wing stretches out outside described the second cabin and is positioned at below described the first wing.
3. unmanned plane according to claim 2, it is characterized in that, described slide assemblies comprises motor, worm gear and worm screw, described motor is arranged on described the second cabin inwall, the mouth of described motor is connected with one end of described worm screw, and the other end of described worm screw is fixed on described the second cabin inwall, and the length direction of described worm screw is vertical with the length direction of described the first wing, described worm gear is arranged on described worm screw, and is connected with one end of described the 3rd wing.
4. unmanned plane according to claim 1, is characterized in that, is also provided with the 3rd cabin on described body, and described the first cabin is between described the 3rd cabin and described pole.
5. unmanned plane according to claim 4, is characterized in that, described unmanned plane also comprises driver train, and described driver train is arranged in described the 3rd cabin.
6. unmanned plane according to claim 5, is characterized in that, described unmanned plane also comprises screw propeller, and screw propeller is connected with the mouth of described driver train.
7. according to the unmanned plane described in claim 1-6 any one, it is characterized in that, described the second wing is V-shaped.
8. according to the unmanned plane described in claim 1-6 any one, it is characterized in that, described unmanned plane also comprises hatchcover, and described hatchcover removably covers on described opening.
9. according to the unmanned plane described in claim 1-6 any one, it is characterized in that, described unmanned plane also comprises the alighting gear that is arranged on described organism bottom.
10. unmanned plane according to claim 9, is characterized in that, the quantity of described alighting gear is 3.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320612794.8U CN203593159U (en) | 2013-09-29 | 2013-09-29 | Multi-purpose unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320612794.8U CN203593159U (en) | 2013-09-29 | 2013-09-29 | Multi-purpose unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203593159U true CN203593159U (en) | 2014-05-14 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320612794.8U Expired - Fee Related CN203593159U (en) | 2013-09-29 | 2013-09-29 | Multi-purpose unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN203593159U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104058087A (en) * | 2014-07-03 | 2014-09-24 | 天津曙光敬业科技有限公司 | Case opening and closing system of unmanned helicopter |
| CN108137149A (en) * | 2015-09-02 | 2018-06-08 | 杰托普特拉股份有限公司 | Injector and airfoil configuration |
-
2013
- 2013-09-29 CN CN201320612794.8U patent/CN203593159U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104058087A (en) * | 2014-07-03 | 2014-09-24 | 天津曙光敬业科技有限公司 | Case opening and closing system of unmanned helicopter |
| CN104058087B (en) * | 2014-07-03 | 2016-07-06 | 天津曙光敬业科技有限公司 | The casing open-close system of depopulated helicopter |
| CN108137149A (en) * | 2015-09-02 | 2018-06-08 | 杰托普特拉股份有限公司 | Injector and airfoil configuration |
| CN108137149B (en) * | 2015-09-02 | 2021-07-06 | 杰托普特拉股份有限公司 | Ejector and airfoil configuration |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: TAIYUAN POWER SUPPLY COMPANY, STATE GRID SHANXI EL Effective date: 20140811 Owner name: STATE GRID CORPORATION OF CHINA Free format text: FORMER OWNER: TAIYUAN POWER SUPPLY COMPANY, STATE GRID SHANXI ELECTRIC POWER COMPANY Effective date: 20140811 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 030012 TAIYUAN, SHAANXI PROVINCE TO: 100031 DONGCHENG, BEIJING |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20140811 Address after: 100031 West Chang'an Avenue, Beijing, No. 86 Patentee after: State Grid Corporation of China Patentee after: Taiyuan Power Supply Company, State Grid Shanxi Electric Power Company Address before: 030012 No. 89 North Road, Shanxi, Taiyuan Patentee before: Taiyuan Power Supply Company, State Grid Shanxi Electric Power Company |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140514 Termination date: 20140929 |
|
| EXPY | Termination of patent right or utility model |