CN204660031U - A kind of special gas detecting device based on four-axle aircraft - Google Patents
A kind of special gas detecting device based on four-axle aircraft Download PDFInfo
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- CN204660031U CN204660031U CN201520280716.1U CN201520280716U CN204660031U CN 204660031 U CN204660031 U CN 204660031U CN 201520280716 U CN201520280716 U CN 201520280716U CN 204660031 U CN204660031 U CN 204660031U
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- detecting device
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Abstract
The utility model discloses a kind of special gas detecting device based on four-axle aircraft, comprise support, flight controller, electronic governor, brushless motor, lithium cell, signal projector, 2.4G wireless receiver, one n RF24L01 module, ground station, 2nd n RF24L01 module, upper computer, it is characterized in that, described lithium cell both sides are provided with described support, flight controller installed by described support, side, described flight controller top arranges described signal projector, described support extends to both sides and top is provided with described brushless motor, electronic governor has been installed in described support extended spot lower end, described support side is provided with described 2.4G wireless receiver, described support opposite side is provided with a described n RF24L01 module, this device does not need artificial carrying device to go to detect, and the dangerous place of being inconvenient to arrive such as high-altitude, hill path, crater can be detected, whole detecting device does not limit by external factors such as environment, landform, weather.
Description
Technical field
The utility model relates to a kind of gas-detecting device, is specifically related to a kind of special gas detecting device based on four-axle aircraft.
Background technology
Along with people are for the concern of environmental protection, increasing people payes attention to air environment, we live in atmosphere after all, the quality of whole air also determine our quality of life, but air cannot see change intuitively, trace change in air is also that naked eyes cannot distinguish, how to observe the change of air timely and effectively prevents the pollution of air from becoming the important topic of air conservation.
Traditional gas-detecting device is portable and hand-held mainly, the gaseous species that this kind of device mainly utilizes gas sensor to come to exist in testing environment at gas detect and concentration, traditional gas detecting instrument women weaver detects the place that people can arrive, by monitoring of environmental and think that factor interference ratio is larger, for the place that some more dangerous inconvenient people such as high-altitude, mountain valley, crater enter, traditional device has been difficult to detection.
Utility model content
The technical problems to be solved in the utility model overcomes existing defect, a kind of special gas detecting device based on four-axle aircraft is provided, flight instruments arranges special gas detecting device, the data obtained are presented on the read-out of ground control system, to solve the technical matters in background technology.
In order to solve the problems of the technologies described above, the utility model provides following technical scheme:
The utility model provides a kind of special gas detecting device based on four-axle aircraft, comprise support, flight controller, electronic governor, brushless motor, lithium cell, signal projector, 2.4G wireless receiver, a n RF24L01 module, ground station, the 2nd n RF24L01 module, upper computer; It is characterized in that, described lithium cell both sides are provided with described support, flight controller installed by described support, side, described flight controller top arranges described signal projector, described support extends to both sides and top is provided with described brushless motor, electronic governor has been installed in described support extended spot lower end, and described support side is provided with described 2.4G wireless receiver, and described support opposite side is provided with a described n RF24L01 module.
Further, described ground station is made up of described upper computer and described 2nd n RF24L01 module, and described 2nd n RF24L01 module composition is arranged on a block system plate, is connected with described upper computer by circuit.
Further, described electronic governor and described brushless motor have four, are arranged on respectively in four branches of support, and wing is arranged at described brushless motor top.
Further, described flight controller and described signal disposed thereon are emitted through circuit and a described n RF24L01 model calling.
Further, described lithium cell and described flight controller are parallel is crossingly arranged on described support upper and lower surface.
Compared with prior art, the beneficial effects of the utility model are: installed on board the aircraft by special gas detecting device, aircraft is controlled by ground, special gas detecting device transmits data and goes back to ground control center to complete whole operation, artificial carrying device is not needed to go to detect, the dangerous place of being inconvenient to arrive such as high-altitude, hill path, crater can be detected, whole detecting device does not limit by external factors such as environment, landform, weather.
Accompanying drawing explanation
Accompanying drawing is used to provide further understanding of the present utility model, and forms a part for specification sheets, is used from explanation the utility model, does not form restriction of the present utility model with embodiment one of the present utility model.In the accompanying drawings:
Fig. 1 is four-axle aircraft and the special gas Sensor section schematic perspective view of a kind of special gas detecting device based on four-axle aircraft described in the utility model embodiment;
Fig. 2 is ground station's schematic perspective view of a kind of special gas detecting device based on four-axle aircraft described in the utility model embodiment;
In figure: 1, support; 2, flight controller; 3, electronic governor; 4, brushless motor; 5, lithium cell; 6, signal projector; 7,2.4G wireless receiver; 8, a n RF24L01 module; 9, ground station; 10, the 2nd n RF24L01 module; 11, upper computer.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described, should be appreciated that preferred embodiment described herein is only for instruction and explanation of the utility model, and be not used in restriction the utility model.
As shown in Figure 1 to Figure 2, a kind of special gas detecting device based on four-axle aircraft of the utility model, comprises support 1, flight controller 2, electronic governor 3, brushless motor 4, lithium cell 5, signal projector 6,2.4G wireless receiver 7, a n RF24L01 module 8, ground station 9, the 2nd n RF24L01 module 10, upper computer 11; It is characterized in that, described lithium cell 5 both sides are provided with described support 1, flight controller 2 installed by described support 1, side, described flight controller 2 top arranges described signal and launches 6, described support 1 extends to both sides and top is provided with described brushless motor 4, electronic governor 3 has been installed in described support 1 extended spot lower end, and described support 1 side is provided with described 2.4G wireless receiver 7, and described support 1 opposite side is provided with a described n RF24L01 module 8.
Described ground station 9 is made up of with described 2nd n RF24L01 module 10 described upper computer 11, described 2nd n RF24L01 module 10 composition is arranged on a block system plate, be connected with described upper computer 11 by circuit, the special gas detecting device installed on board the aircraft, operation and the data processing of whole device is controlled with described ground station 9, not employment is carried gas-detecting device and is detected, be convenient to the place that detection manpower cannot arrive, not by the impact of landform, adaptive faculty is extremely strong, and control conveniently, monitoring data is accurate.
Described electronic governor 3 has four with described brushless motor 4, and be arranged on respectively on four axles of support 1, and wing is arranged at described brushless motor 4 top, drives wing by brushless motor 4, the wing on four axles does not limit by landform, can vertical lift.
Described flight controller 2 and described signal disposed thereon are launched 6 and are connected with a described nRF24L01 module 8 by circuit, described ground station 9 launch intruction controls described flight controller to described heart method receptor 7 and starts, flies, dissimilar gas sensor is installed on board the aircraft by port temporarily, and detect the data of air special gas, and processed by a described n RF24L01 module 8, be transmitted to described ground station 9 by described signal projector 6.
Described lithium cell 5 and described flight controller 2 are parallel is crossingly arranged on described support 1 upper and lower surface, and described lithium cell 5 is crossing with described flight controller 2 effectively can reduce the loss of electricity in transport process together, extends the work-hours of aircraft.
A kind of special gas detecting device based on four-axle aircraft of the utility model, four-axle aircraft, gas sensor, ground control system combine by this kind of device, define not by the special gas detecting device of landform, weather effect, in ground control situation, the special gas that aircraft can complete Special zone detects, and reduces the danger detecting in hazardous environment and bring to people.
The utility model is a kind of special gas detecting device based on four-axle aircraft, special gas detecting device is installed on board the aircraft, aircraft is controlled by ground, special gas detecting device transmits data and goes back to ground control center to complete whole operation, artificial carrying device is not needed to go to detect, the dangerous place of being inconvenient to arrive such as high-altitude, hill path, crater can be detected, whole detecting device does not limit by external factors such as environment, landform, weather.
Last it is noted that the foregoing is only preferred embodiment of the present utility model, be not limited to the utility model, although be described in detail the utility model with reference to previous embodiment, for a person skilled in the art, it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature.All within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (5)
1., based on a special gas detecting device for four-axle aircraft, comprise support (1), flight controller (2), electronic governor (3), brushless motor (4), lithium cell (5), signal projector (6), 2.4G wireless receiver (7), a n RF24L01 module (8), ground station (9), the 2nd n RF24L01 module (10), upper computer (11), it is characterized in that, described lithium cell (5) both sides are provided with described support (1), described support (1) is installed flight controller (2), described flight controller (2) side, top arranges described signal projector (6), described support (1) extends to both sides and top is provided with described brushless motor (4), electronic governor (3) has been installed in described support (1) extended spot lower end, described support (1) side is provided with described 2.4G wireless receiver (7), described support (1) opposite side is provided with a described n RF24L01 module (8).
2. a kind of special gas detecting device based on four-axle aircraft according to claim 1, it is characterized in that, described ground station (9) is made up of described upper computer (11) and described 2nd n RF24L01 module (10), described 2nd n RF24L01 module (10) composition is arranged on a block system plate, is connected with described upper computer (11) by circuit.
3. a kind of special gas detecting device based on four-axle aircraft according to claim 1, it is characterized in that, described electronic governor (3) and described brushless motor (4) have four, be arranged on respectively on four axles of support (1), and wing is arranged at described brushless motor (4) top.
4. a kind of special gas detecting device based on four-axle aircraft according to claim 1, it is characterized in that, described flight controller (2) is connected with a described n RF24L01 module (8) by circuit with described signal projector (6) disposed thereon.
5. a kind of special gas detecting device based on four-axle aircraft according to claim 1 or 4, it is characterized in that, described lithium cell (5) and described flight controller (2) are parallel is crossingly arranged on described support (1) upper and lower surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520280716.1U CN204660031U (en) | 2015-04-27 | 2015-04-27 | A kind of special gas detecting device based on four-axle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520280716.1U CN204660031U (en) | 2015-04-27 | 2015-04-27 | A kind of special gas detecting device based on four-axle aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204660031U true CN204660031U (en) | 2015-09-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520280716.1U Expired - Fee Related CN204660031U (en) | 2015-04-27 | 2015-04-27 | A kind of special gas detecting device based on four-axle aircraft |
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| CN (1) | CN204660031U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017084198A1 (en) * | 2015-11-21 | 2017-05-26 | 深圳市易特科信息技术有限公司 | Unmanned aerial vehicle for detecting environmental toxic gas |
-
2015
- 2015-04-27 CN CN201520280716.1U patent/CN204660031U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017084198A1 (en) * | 2015-11-21 | 2017-05-26 | 深圳市易特科信息技术有限公司 | Unmanned aerial vehicle for detecting environmental toxic gas |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150923 Termination date: 20160427 |