CN106828929A - A kind of unmanned plane wind speed and humidity measurement device - Google Patents
A kind of unmanned plane wind speed and humidity measurement device Download PDFInfo
- Publication number
- CN106828929A CN106828929A CN201710033054.1A CN201710033054A CN106828929A CN 106828929 A CN106828929 A CN 106828929A CN 201710033054 A CN201710033054 A CN 201710033054A CN 106828929 A CN106828929 A CN 106828929A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- wind speed
- measuring apparatus
- measurement device
- humidity measurement
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000005259 measurement Methods 0.000 title claims abstract description 18
- 238000001514 detection method Methods 0.000 claims abstract description 14
- 239000000523 sample Substances 0.000 claims abstract description 12
- 230000005484 gravity Effects 0.000 claims abstract description 4
- 239000000463 material Substances 0.000 claims description 3
- 230000008054 signal transmission Effects 0.000 claims description 3
- 238000012544 monitoring process Methods 0.000 abstract description 3
- 230000001174 ascending effect Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001568 sexual effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D21/00—Measuring or testing not otherwise provided for
- G01D21/02—Measuring two or more variables by means not covered by a single other subclass
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)
Abstract
The present invention discloses a kind of unmanned plane wind speed and humidity measurement device, unmanned plane selects multi-rotor unmanned aerial vehicle, connecting rod is installed above unmanned plane body gravity axis, the connecting rod upper end is installed by detection probe, the detection probe is electrically connected air speed measuring apparatus, the air speed measuring apparatus are installed on unmanned plane organism bottom, measuring instrument of the air speed measuring apparatus from accurate measurement wind speed, air quantity and humiture, the connecting rod is using logical core bar, inside it is installed with electric wire, described electric wire one end is connected in detection probe, and the other end is connected to air speed measuring apparatus；Invention is compared with prior art, security of the unmanned aerial vehicle in flight operation can be ensured, in prairie bad environments region, have the influence of special miniclimate, powerful ascending air can influence the flight of unmanned aerial vehicle or be damaged unmanned plane, and the present invention can warn to ensure the safety of remote sensing monitoring unmanned aerial vehicle.
Description
Technical field
The present invention relates to environment measuring field, specifically a kind of unmanned plane wind speed and humidity measurement device.
Background technology
On Mongolian prairie, influence of the wind-force to live and work is especially important, and wind-force test be environmental monitoring and
The important technology index of Wind Power Utilization, prior art is typically employed in ground setting tester and discharges the modes such as balloon-sonde and receives
Collection information data, the method for existing detection wind-force is the fixed detection of ground somewhere or a certain eminence, prairie mostly at present
Area is vast, and some regions people are also to enter into, and many many sexual intercourses of regional high mountain, and miniclimate type is complicated and changeable,
Situations such as in order to detect its environment, propose a kind of unmanned plane wind speed and humidity measurement device.
The content of the invention
The invention aims to solve defect of the prior art, there is provided a kind of unmanned plane wind speed and humidity measurement
Device solves the above problems.
To achieve these goals, technical scheme is as follows：A kind of unmanned plane wind speed and humidity measurement device,
Unmanned plane selects multi-rotor unmanned aerial vehicle, it is characterised in that connecting rod, the connecting rod are installed above unmanned plane body gravity axis
Detection probe is installed in upper end, and the detection probe is electrically connected air speed measuring apparatus, and the air speed measuring apparatus are installed on unmanned plane body bottom
Portion.
Further improve, measuring instrument of the air speed measuring apparatus from accurate measurement wind speed, air quantity and humiture.
Further improve, the control module in the unmanned plane body adds one piece of bluetooth radio module, for wind speed
The signal transmission of measuring instrument.
Further improve, the connecting rod is inside installed with electric wire using logical core bar, and described electric wire one end is connected in detection probe,
The other end is connected to air speed measuring apparatus.
Further improve, the unmanned motor spindle sets mounting box, and the air speed measuring apparatus are installed in mounting box, described
Mounting box plastic material.
The present invention compared with prior art, can ensure security of the unmanned aerial vehicle in flight operation, in prairie environment
Severe region, has the influence of special miniclimate, and powerful ascending air can influence the flight of unmanned aerial vehicle or make unmanned plane
It is damaged, the present invention can warn to ensure the safety of remote sensing monitoring unmanned aerial vehicle.
Brief description of the drawings
Fig. 1 is the structural representation of a kind of unmanned plane wind speed of the invention and humidity measurement device.
Specific embodiment
Embodiments of the invention are elaborated below, the present embodiment is carried out under premised on technical solution of the present invention
Implement, give detailed implementation method and specific operating process, but protection scope of the present invention is not limited to following implementations
Example.
As shown in figure 1, a kind of unmanned plane wind speed of the present embodiment and humidity measurement device, unmanned plane from many rotors without
Man-machine, it is characterised in that connecting rod 2 is installed above the gravity axis of unmanned plane body 1, detection probe is installed in the upper end of the connecting rod 2
3, the detection probe 3 is electrically connected air speed measuring apparatus 4, and the air speed measuring apparatus 4 are installed on the bottom of unmanned plane body 1, it is described nobody
Control module in machine body 1 adds one piece of bluetooth radio module, for the signal transmission with air speed measuring apparatus 4, the connection
Bar 2 is inside installed with electric wire using logical core bar, and described electric wire one end is connected in detection probe 3, and the other end is connected to air speed measuring apparatus 4, institute
Measuring wind speed is stated, 4 select the measuring instrument of accurate measurement wind speed, air quantity and humiture, and the interior bluetooth that is provided with of the air speed measuring apparatus 4 is led to
Letter module, the communication with the control module of unmanned plane, the unmanned motor spindle sets mounting box, and the air speed measuring apparatus are installed on
In mounting box, the mounting box plastic material.
Presently preferred embodiments of the present invention is the foregoing is only, is not intended to limit the invention, it is all in essence of the invention
Any modification, equivalent and improvement made within god and principle etc., should be included within the scope of the present invention.
Claims (5)
1. a kind of unmanned plane wind speed and humidity measurement device, unmanned plane select multi-rotor unmanned aerial vehicle, it is characterised in that at nobody
Connecting rod is installed in machine body gravity axis top, and detection probe is installed in the connecting rod upper end, and the detection probe is electrically connected wind speed survey
Amount instrument, the air speed measuring apparatus are installed on unmanned plane organism bottom.
2. a kind of unmanned plane wind speed according to claim 1 and humidity measurement device, it is characterised in that：The wind speed is surveyed
Measuring instrument of the amount instrument from accurate measurement wind speed, air quantity and humiture.
3. a kind of unmanned plane wind speed according to claim 1 and humidity measurement device, it is characterised in that：The unmanned plane
Control module in body adds one piece of bluetooth radio module, for the signal transmission with air speed measuring apparatus.
4. according to a kind of unmanned plane wind speed described in claim 1 and humidity measurement device, it is characterised in that：The connecting rod is adopted
Logical core bar is used, electric wire is inside installed with, described electric wire one end is connected in detection probe, and the other end is connected to air speed measuring apparatus.
5. a kind of unmanned plane wind speed according to claim 1 and humidity measurement device, it is characterised in that：The unmanned plane
Bottom sets mounting box, and the air speed measuring apparatus are installed in mounting box, the mounting box plastic material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710033054.1A CN106828929A (en) | 2017-01-18 | 2017-01-18 | A kind of unmanned plane wind speed and humidity measurement device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710033054.1A CN106828929A (en) | 2017-01-18 | 2017-01-18 | A kind of unmanned plane wind speed and humidity measurement device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106828929A true CN106828929A (en) | 2017-06-13 |
Family
ID=59123712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710033054.1A Pending CN106828929A (en) | 2017-01-18 | 2017-01-18 | A kind of unmanned plane wind speed and humidity measurement device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106828929A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107291103A (en) * | 2017-08-07 | 2017-10-24 | 联想(北京)有限公司 | A kind of control method and electronic equipment |
| CN111595742A (en) * | 2020-05-26 | 2020-08-28 | 北京未来智能科技有限公司 | Unmanned aerial vehicle gas detection system and detection method thereof |
| CN114104292A (en) * | 2022-01-24 | 2022-03-01 | 西安杰出科技有限公司 | Multi-rotor unmanned aerial vehicle for alarming |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103558653A (en) * | 2013-11-23 | 2014-02-05 | 李炳燃 | Weather detection airplane based on platform with multiple rotor wings |
| US20160023776A1 (en) * | 2014-07-23 | 2016-01-28 | Honeywell International Inc. | Systems and methods for airspeed estimation using actuation signals |
| CN205044963U (en) * | 2015-09-14 | 2016-02-24 | 天津捷金金属制品有限公司 | Novel unmanned aerial vehicle of wind power generation field usefulness |
| CN105891908A (en) * | 2016-04-19 | 2016-08-24 | 华南农业大学 | Airborne weather station apparatus for unmanned plane, and application method thereof |
| CN105882968A (en) * | 2016-06-24 | 2016-08-24 | 中国农业科学院农田灌溉研究所 | Field spatial data acquisition device |
| CN106199215A (en) * | 2016-07-06 | 2016-12-07 | 青岛四合信息科技有限公司 | A kind of unmanned plane electromagnetic environment test devices and methods therefor |
-
2017
- 2017-01-18 CN CN201710033054.1A patent/CN106828929A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103558653A (en) * | 2013-11-23 | 2014-02-05 | 李炳燃 | Weather detection airplane based on platform with multiple rotor wings |
| US20160023776A1 (en) * | 2014-07-23 | 2016-01-28 | Honeywell International Inc. | Systems and methods for airspeed estimation using actuation signals |
| CN205044963U (en) * | 2015-09-14 | 2016-02-24 | 天津捷金金属制品有限公司 | Novel unmanned aerial vehicle of wind power generation field usefulness |
| CN105891908A (en) * | 2016-04-19 | 2016-08-24 | 华南农业大学 | Airborne weather station apparatus for unmanned plane, and application method thereof |
| CN105882968A (en) * | 2016-06-24 | 2016-08-24 | 中国农业科学院农田灌溉研究所 | Field spatial data acquisition device |
| CN106199215A (en) * | 2016-07-06 | 2016-12-07 | 青岛四合信息科技有限公司 | A kind of unmanned plane electromagnetic environment test devices and methods therefor |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107291103A (en) * | 2017-08-07 | 2017-10-24 | 联想(北京)有限公司 | A kind of control method and electronic equipment |
| CN111595742A (en) * | 2020-05-26 | 2020-08-28 | 北京未来智能科技有限公司 | Unmanned aerial vehicle gas detection system and detection method thereof |
| CN114104292A (en) * | 2022-01-24 | 2022-03-01 | 西安杰出科技有限公司 | Multi-rotor unmanned aerial vehicle for alarming |
| CN114104292B (en) * | 2022-01-24 | 2022-04-22 | 西安杰出科技有限公司 | Multi-rotor unmanned aerial vehicle for alarming |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105676843B (en) | New energy automobile benchmarking analysis and evaluation system and method thereof | |
| CN106828929A (en) | A kind of unmanned plane wind speed and humidity measurement device | |
| CN106759215B (en) | A kind of multifunction digital seismic wave hole pressure touching methods test macro | |
| CN205450295U (en) | Machine carries nuclear radiation ring border and detects and sampling device | |
| CN202815124U (en) | Insulator detecting device by using multi-rotor unmanned aerial vehicle | |
| CN102879692A (en) | Method and device for detecting insulator through multi-rotor unmanned aerial vehicle | |
| CN203595737U (en) | Universal meter with wireless communication function | |
| CN203365535U (en) | Vehicle current collection system and car having same | |
| CN106441929A (en) | Electromobile electric accessory performance testing and collecting system and collecting method | |
| CN103675680B (en) | A kind of locomotive motor optical-electricity encoder detector and detection method | |
| CN104835326A (en) | Vehicle detector based on anisotropy magnetic resistance sensor array | |
| CN206431113U (en) | A kind of novel air EMS | |
| CN114111905A (en) | High slope construction scaffold safety monitoring system | |
| CN105067833A (en) | Automobile engine rotating speed detection apparatus based on power controller | |
| CN112067056A (en) | Contact net detection device, method and device and computer readable storage medium | |
| CN205719881U (en) | Portable PM2.5 concentration detection apparatus | |
| CN103439367B (en) | Composite insulator string live detection equipment | |
| CN103983403A (en) | Apparatus and method for measuring operating performance and parameters of motor propeller system | |
| CN205921353U (en) | Cable joint with temperature measuring function | |
| CN108051026A (en) | Humiture transducer | |
| CN204346459U (en) | The wafer test system of micro-mechanical gyroscope | |
| CN205450178U (en) | Transmission line fault locating on -line monitoring device | |
| CN103064037A (en) | Burglar alarm device based on magnetic field sensor | |
| CN106774017A (en) | A kind of Unmanned Aerial Vehicle Data acquisition system | |
| CN203422425U (en) | Composite insulator chain electrification detection device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170613 |
|
| RJ01 | Rejection of invention patent application after publication |