CN106114840B - A kind of well lid loss warning unmanned plane - Google Patents
A kind of well lid loss warning unmanned plane Download PDFInfo
- Publication number
- CN106114840B CN106114840B CN201610612193.5A CN201610612193A CN106114840B CN 106114840 B CN106114840 B CN 106114840B CN 201610612193 A CN201610612193 A CN 201610612193A CN 106114840 B CN106114840 B CN 106114840B
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- CN
- China
- Prior art keywords
- fixedly mounted
- pedestal
- hydraulic cylinders
- hydraulic cylinder
- motor
- 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.)
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 24
- 230000003287 optical effect Effects 0.000 claims abstract description 8
- 238000001914 filtration Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 1
- 208000037805 labour Diseases 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Monitoring And Testing Of Nuclear Reactors (AREA)
- Hydraulic Motors (AREA)
Abstract
The present invention provides a kind of well lid loss warning unmanned plane, including pedestal, 4 propellers, 4 motors, 4 motor racks, 4 first hydraulic cylinders, 4 optical axises, protection network, camera, power plant module, second hydraulic cylinders, it is characterised in that：4 motor racks are fixedly mounted on by the fixed seat of bottom on pedestal upper surface；4 motors are respectively and fixedly installed on 4 motor racks；4 propellers are fixedly mounted on 4 motor output shafts；4 first hydraulic cylinders are fixedly mounted on by top fixed frame on pedestal lower face, and 4 first hydraulic cylinders are equipped with axis hole；The second hydraulic cylinder is fixedly mounted on pedestal upper surface；The upper plate of the protection network is fixedly mounted on the ring flange of second hydraulic cylinder piston rod end；The present invention can quickly reach designated position, be suitble to sizes well head, can play a role in filtering, have a wide range of application.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of well lid loses warning unmanned plane.
Background technology
With climate change, serious flood, rainwater often jack up well lid frequent occurrence, and are not easy to find, right
The safety for going out administrative staff threatens, therefore is frequently necessary to people station and is reminded passerby on well side, and this mode is danger
A large amount of labours are needed again, therefore are badly in need of a kind of well lid loss warning unmanned plane.
Invention content
In view of the above-mentioned problems, the present invention provides a kind of well lid loss warning unmanned plane, designated position can be quickly reached, is fitted
It is wide with range.
Technical solution used in the present invention is：A kind of well lid loss warning unmanned plane, including pedestal, 4 propellers, 4
A motor, 4 motor racks, 4 first hydraulic cylinders, 4 optical axises, protection network, camera, power plant module, second hydraulic cylinders, it is special
Sign is：4 motor racks are fixedly mounted on by the fixed seat of bottom on pedestal upper surface；4 motors point
It is not fixedly mounted on 4 motor racks；4 propellers are fixedly mounted on 4 motor output shafts；Described 4
One hydraulic cylinder is fixedly mounted on by top fixed frame on pedestal lower face, and 4 first hydraulic cylinders are equipped with axis hole；Described 4
Root optical axis one end is fixedly mounted on 4 first hydraulic cylinder piston rod ends, and the other end is slidably mounted on axis hole；The camera shooting
Head is fixedly mounted on the holder of pedestal upper surface；The power plant module is fixedly mounted on pedestal upper surface；Described
Two hydraulic cylinders are fixedly mounted on pedestal upper surface；The upper plate of the protection network is fixedly mounted on second hydraulic cylinder piston rod
On the ring flange of end；
The protection network includes upper plate, 24 connecting rods, foundation rings, and described 24 connecting rod one end are evenly distributed on foundation ring
On upper surface, the other end is evenly distributed on upper plate lower face；
4 first hydraulic cylinders, second hydraulic cylinder are connected by oil pipe with power plant module；4 motors are taken the photograph
As head is connected by conducting wire with power plant module；
Further, the base center is machined with circular hole；It is processed into 4 first hydraulic cylinder piston rod ends
Boss.
Since present invention employs above-mentioned technical proposal, the present invention has the following advantages：
The present invention can quickly reach designated position, be suitble to sizes well head, can play a role in filtering, application range
Extensively.
Description of the drawings
Fig. 1 is the structural schematic diagram after the present invention is completed.
Fig. 2 is the structural schematic diagram that the present invention is completed rear another angle.
Fig. 3 is the structural schematic diagram of protection network of the present invention.
Drawing reference numeral：1- pedestals；2- propellers；3- motors；4- motor racks；5- first hydraulic cylinders；6- optical axises；7- is protected
Net；8- cameras；9- power plant modules；10- second hydraulic cylinders；701- upper plates；702- connecting rods；The foundation rings 703-.
Specific implementation mode
Below with reference to the embodiments and with reference to the accompanying drawing the technical solutions of the present invention will be further described.
As shown in Figure 1, Figure 2, Figure 3 shows, a kind of well lid loses warning unmanned plane, including 2,4, the propeller motor of pedestal 1,4
3,4 motor racks 4,4 first hydraulic cylinder 5,4 optical axis 6, protection network 7, camera 8, power plant module 9, second hydraulic cylinders 10,
It is characterized in that：4 motor racks 4 are fixedly mounted on by the fixed seat of bottom on 1 upper surface of pedestal；Described 4
Motor 3 is respectively and fixedly installed on 4 motor racks 4；4 propellers 2 are fixedly mounted on 43 output shafts of motor；Institute
4 first hydraulic cylinders 5 stated are fixedly mounted on by top fixed frame on 1 lower face of pedestal, and 4 first hydraulic cylinders 5 are equipped with
Axis hole；4 described 6 one end of optical axis are fixedly mounted on 45 piston rod ends of first hydraulic cylinder, and the other end is slidably mounted on axis
Kong Shang；The camera 8 is fixedly mounted on the holder of 1 upper surface of pedestal；The power plant module 9 is fixedly mounted on pedestal
On 1 upper surface；The second hydraulic cylinder 10 is fixedly mounted on 1 upper surface of pedestal；The upper plate 701 of the protection network 7
It is fixedly mounted on the ring flange of 10 piston rod end of second hydraulic cylinder；
The protection network 7 includes upper plate 701,24 connecting rods 702, foundation rings 703, described 24 702 one end of connecting rod
It is evenly distributed on 703 upper surface of foundation ring, the other end is evenly distributed on 701 lower face of upper plate；
4 first hydraulic cylinders 5, second hydraulic cylinder 10 are connected by oil pipe with power plant module 9；4 electricity
Machine 3, camera 8 are connected by conducting wire with power plant module 9；
Further, 1 center of pedestal is machined with circular hole；45 piston rod ends of first hydraulic cylinder processing
At boss.
The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, for the skill of this field
For art personnel, the invention may be variously modified and varied.All within the spirits and principles of the present invention, any made by repair
Change, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Operation principle of the present invention：Specific location is set first, is navigated by camera 8, and 43 bands of motor are passed through
Destination is flown in dynamic 4 propellers 2 rotation, and 4 first hydraulic cylinders 5 are stretched out, and unmanned plane is made to land, and the stretching of second hydraulic cylinder 10 makes
Protection network 7 is moved downward to edge and is contacted with well head, and 4 motors 3 stop operating.
Claims (1)
1. a kind of well lid loses warning unmanned plane, including pedestal（1）, 4 propellers（2）, 4 motors（3）, 4 motor racks
（4）, 4 first hydraulic cylinders（5）, 4 pieces optical axises（6）, protection network（7）, camera（8）, power plant module（9）, second hydraulic cylinder
（10）, it is characterised in that：4 motor racks（4）It is fixedly mounted on pedestal by the fixed seat of bottom（1）On upper surface；
4 motors（3）It is respectively and fixedly installed to 4 motor racks（4）On；4 propellers（2）It is fixedly mounted on 4
Motor（3）On output shaft；4 first hydraulic cylinders（5）It is fixedly mounted on pedestal by top fixed frame（1）Lower face
On, 4 first hydraulic cylinders（5）It is equipped with axis hole；4 optical axises（6）One end is fixedly mounted on 4 first hydraulic cylinders（5）
Piston rod end, the other end are slidably mounted on axis hole；The camera（8）It is fixedly mounted on pedestal（1）The branch of upper surface
On frame；The power plant module（9）It is fixedly mounted on pedestal（1）On upper surface；The second hydraulic cylinder（10）It is fixedly mounted
In pedestal（1）On upper surface；The protection network（7）Upper plate（701）It is fixedly mounted on second hydraulic cylinder（10）Piston rod
On the ring flange of end；The protection network（7）Including upper plate（701）, 24 pieces connecting rods（702）, foundation ring（703）, described
24 connecting rods（702）One end is evenly distributed on foundation ring（703）On upper surface, the other end is evenly distributed on upper plate（701）Lower end
On face；4 first hydraulic cylinders（5）, second hydraulic cylinder（10）Pass through oil pipe and power plant module（9）It is connected；Described 4
Motor（3）, camera（8）Pass through conducting wire and power plant module（9）It is connected；The pedestal（1）Center is machined with circular hole；Described
4 first hydraulic cylinders（5）It is processed into boss in piston rod end；Pass through camera（8）It navigates, is driven by 4 motors (3)
Destination is flown in 4 propeller (2) rotations, and 4 first hydraulic cylinders (5) are stretched out, and so that unmanned plane is landed, second hydraulic cylinder (10)
Stretching makes protection network (7) be moved downward to edge to contact with well head, and 4 motors (3) stop operating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610612193.5A CN106114840B (en) | 2016-07-31 | 2016-07-31 | A kind of well lid loss warning unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610612193.5A CN106114840B (en) | 2016-07-31 | 2016-07-31 | A kind of well lid loss warning unmanned plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106114840A CN106114840A (en) | 2016-11-16 |
| CN106114840B true CN106114840B (en) | 2018-11-13 |
Family
ID=57254895
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610612193.5A Active CN106114840B (en) | 2016-07-31 | 2016-07-31 | A kind of well lid loss warning unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106114840B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107524103B (en) * | 2017-08-30 | 2019-06-25 | 广州市翔通交通设施工程有限公司 | A kind of Intelligent road warning system and its method based on unmanned plane |
| CN107587526B (en) * | 2017-10-17 | 2019-11-01 | 灵武市海德鸿工业产品设计有限公司 | A kind of intelligent well cover system and its control method based on unmanned plane |
| CN109141367B (en) * | 2018-04-16 | 2019-06-14 | 深圳市金盾智能系统工程有限公司 | Well lid display system based on image recognition |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4188674A (en) * | 1978-06-15 | 1980-02-19 | Mardirosian Louis C | Contact lens saving devices |
| CN204399482U (en) * | 2014-12-26 | 2015-06-17 | 郑州中电新能源汽车有限公司 | The electronic unmanned fog machine of a kind of DCB Specimen close coupled type anticollision |
| CN204674822U (en) * | 2015-05-14 | 2015-09-30 | 深圳市大疆创新科技有限公司 | Alighting gear and use the unmanned vehicle of this alighting gear |
| CN204849843U (en) * | 2015-08-11 | 2015-12-09 | 陈伟 | Well lid of can be dropproof and reporting to police |
| CN205186515U (en) * | 2015-12-12 | 2016-04-27 | 黎倩 | Support height -adjustable's unmanned aerial vehicle |
-
2016
- 2016-07-31 CN CN201610612193.5A patent/CN106114840B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4188674A (en) * | 1978-06-15 | 1980-02-19 | Mardirosian Louis C | Contact lens saving devices |
| CN204399482U (en) * | 2014-12-26 | 2015-06-17 | 郑州中电新能源汽车有限公司 | The electronic unmanned fog machine of a kind of DCB Specimen close coupled type anticollision |
| CN204674822U (en) * | 2015-05-14 | 2015-09-30 | 深圳市大疆创新科技有限公司 | Alighting gear and use the unmanned vehicle of this alighting gear |
| CN204849843U (en) * | 2015-08-11 | 2015-12-09 | 陈伟 | Well lid of can be dropproof and reporting to police |
| CN205186515U (en) * | 2015-12-12 | 2016-04-27 | 黎倩 | Support height -adjustable's unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106114840A (en) | 2016-11-16 |
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|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20181008 Address after: 225200 district two, Zhenwu Town, Jiangdu District, Yangzhou, Jiangsu. Applicant after: Yangzhou Qing Yu environmental protection equipment Engineering Co., Ltd Address before: 054900 346 Yao Lou village, Luzhai Township, Linxi County, Xingtai, Hebei Applicant before: Ding Huanggang |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |