CN110254717A - A kind of unmanned plane that internal and surface damage can be detected automatically - Google Patents
A kind of unmanned plane that internal and surface damage can be detected automatically Download PDFInfo
- Publication number
- CN110254717A CN110254717A CN201910582332.8A CN201910582332A CN110254717A CN 110254717 A CN110254717 A CN 110254717A CN 201910582332 A CN201910582332 A CN 201910582332A CN 110254717 A CN110254717 A CN 110254717A
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- unmanned plane
- fixed
- chamber
- main body
- fixed frame
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- 238000001931 thermography Methods 0.000 claims abstract description 19
- 238000004891 communication Methods 0.000 claims abstract description 10
- 238000013016 damping Methods 0.000 claims description 12
- 238000009434 installation Methods 0.000 claims 1
- 239000003208 petroleum Substances 0.000 description 8
- 238000010586 diagram Methods 0.000 description 5
- 238000001514 detection method Methods 0.000 description 4
- 230000003321 amplification Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/20—Constructional features
- B64C11/28—Collapsible or foldable blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
- B64D27/353—Arrangements for on-board electric energy production, distribution, recovery or storage using solar cells
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17D—PIPE-LINE SYSTEMS; PIPE-LINES
- F17D5/00—Protection or supervision of installations
-
- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses a kind of unmanned planes that can be detected automatically to internal and surface damage, including fixed frame, unmanned plane main body and propeller blade, solar panel is installed on the outside of the unmanned plane main body, and the bottom end of unmanned plane body interior is provided with chamber, one end of the chamber interior is equipped with battery, and central processing module is installed in the chamber of battery side, wireless communication module is installed in chamber below the central processing module, the inside of the fixed frame is fixed with thermal imaging camera, the both ends of the unmanned plane bottom part body are provided with undercarriage.The present invention is by being equipped with unmanned plane main body, solar panel, battery, fixed frame, first motor, ear, turning ball and thermal imaging camera, the two sides of fixed frame are mounted on first motor, first motor is connect by shaft with ball is turned, allow to adjust the shooting angle of thermal imaging camera, it is not easy to generate dead angle.
Description
Technical field
The present invention relates to technical field of petroleum extraction, specially one kind can automatically be detected internal and surface damage
Unmanned plane.
Background technique
It is well known that petroleum industry is the important component in global energy field, either military defense or civilian
The people's livelihood all be unable to do without petroleum resources, and since petroleum pipeline route is longer, most of route area is relatively remote, with a varied topography, according to
It is unable to satisfy demand by traditional artificial detection, so needing the inside of petroleum pipeline and surface damage to be carried out using unmanned plane
Detection, but the most structure of existing unmanned plane is simple, has a single function, it is specific that there are the following problems；
1, traditional unmanned plane photographic device for shooting is fixed on the rack mostly, is not easy to carry out the adjusting of angle,
It is easy to produce dead angle, causes shooting visual angle not accurate；
2, in landing, the motor of driving propeller blade rotation can stop operating traditional unmanned plane, and propeller blade may
In state directed downwardly, it is easy to be damaged when landing；
3, traditional unmanned plane does not have shock-absorbing function, is easy to cause photographic device rigid collision in landing, shortens and use
Service life.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned planes that can be detected automatically to internal and surface damage, to solve
Existing part unmanned plane mentioned above in the background art is not easy to be easy damage when adjusting shooting angle, propeller blade landing
Badly and do not have the problem of shock-absorbing function.
To achieve the above object, the invention provides the following technical scheme: one kind can automatically carry out internal and surface damage
The unmanned plane of detection, including fixed frame, unmanned plane main body and propeller blade are equipped with the sun on the outside of the unmanned plane main body
Energy solar panel, and the bottom end of unmanned plane body interior is provided with chamber, one end of the chamber interior is equipped with battery, and stores
Central processing module is installed in the chamber of battery side, wireless communication is installed in the chamber below the central processing module
Module, and GPS locator is installed in the chamber of wireless communication module side, the chamber indoor location of the GPS locator side
There is identification module, four corners of the unmanned plane main body are mounted on fixed link, and the top of fixed link is mounted on
The output end of two motors, second motor is fixed with hub body by shaft, and the two sides of hub body are provided with propeller blade,
Four corners of the unmanned plane bottom part body pass through damping and are fixed with buffer board, and the bottom end of buffer board is equipped with
Fixed frame, the inside of the fixed frame are fixed with thermal imaging camera, and the both ends of the unmanned plane bottom part body, which are provided with, rises and falls
Frame.
Preferably, the fixed frame is in reverse U-shaped structure, and the two sides inside fixed frame are provided with by turning ball
Ear, the ear are connect with thermal imaging camera.
Preferably, the two sides of the fixed frame are mounted on first motor, and the output end of first motor passes through shaft
It is connect with ball is turned.
Preferably, the damping includes support, movable block and reset spring, and the bottom end of damping is respectively and fixedly provided with
Support, and the longitudinal section of support is in " recessed " type structure, the inside of the support passes through reset spring and is fixed with movable block, and
The top of movable block is connect with the bottom end of unmanned plane main body.
Preferably, the two sides of the hub body are respectively and fixedly provided with fixed block, and the propeller blade is equal close to one end of fixed block
It is hinged with fixed block, and the top of fixed block is provided with curled portion.
Preferably, the bottom end between the fixed block and propeller blade is provided with spring leaf, and spring leaf is towards remote
It is recessed from the direction of propeller blade.
Compared with prior art, the beneficial effects of the present invention are:
(1) unmanned plane that can be detected automatically to internal and surface damage is by being equipped with unmanned plane main body, solar-electricity
Pond plate, fixed frame, first motor, ear, turns ball and thermal imaging camera at battery, and the two sides of fixed frame are mounted on first
Motor, first motor are connect by shaft with ball is turned, and allow to adjust the shooting angle of thermal imaging camera, it is not easy to be generated dead
Angle meets various shooting demands, while device rationally utilizes solar energy resources by being equipped with solar panel and battery
Electric power is provided for device, facilitates energy-saving and emission-reduction, protects environment；
(2) device is by being equipped with the second motor, hub body, propeller blade, fixed block and spring leaf, propeller blade rotation
When, spring leaf is contacted with hub body and propeller blade respectively, and spring leaf is urged to recessed state, and propeller blade stops turning
When dynamic, propeller blade can be damaged when preventing device from landing because the elastic force of spring leaf flips up；
(3) by being equipped with damping, support, reset spring and movable block, device lands to be generated device with ground face contact
Shaking force make unmanned plane main body be pressed down against movable block so that movable block squeeze support in reset spring, pass through reset
The screen resilience of spring absorbs the shaking force of a part, plays the role of vibration damper, the impact force that slowing device generates when landing,
So that device is not readily susceptible to rigid collision, prolong the service life.
Detailed description of the invention
Fig. 1 is positive structure diagram of the invention；
Fig. 2 is amplification profile structural schematic diagram at A in Fig. 1 of the invention；
Fig. 3 is chamber cross-sectional structural schematic diagram of the invention；
Fig. 4 is damping the schematic diagram of the section structure of the invention；
Fig. 5 is system block diagram of the invention.
In figure: 1, first motor；2, turn ball；3, thermal imaging camera；4, ear；5, fixed frame；6, undercarriage；7, damping machine
Structure；701, reset spring；702, movable block；703, support；8, fixed link；9, the second motor；10, solar panel；11, nothing
Man-machine main body；12, hub body；13, propeller blade；14, chamber；15, buffer board；16, fixed block；17, spring leaf；18, electric power storage
Pond；19, wireless communication module；20, central processing module；21, GPS locator；22, identification module.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig. 1-5, a kind of embodiment provided by the invention: one kind can automatically detect internal and surface damage
Unmanned plane, including fixed frame 5, unmanned plane main body 11 and propeller blade 13, the outside of unmanned plane main body 11 be equipped with the sun
Energy solar panel 10, and the bottom end inside unmanned plane main body 11 is provided with chamber 14, one end inside chamber 14 is equipped with battery
18, and central processing module 20 is installed in the chamber 14 of 18 side of battery, in the chamber 14 of 20 lower section of central processing module
Wireless communication module 19 is installed, and GPS locator 21, GPS positioning are installed in the chamber 14 of 19 side of wireless communication module
The model of device 21 can be GF07, be equipped with identification module 22 in the chamber 14 of 21 side of GPS locator, the four of unmanned plane main body 11
A corner is mounted on fixed link 8, and the top of fixed link 8 is mounted on the second motor 9, and the model of the second motor 9 can be
The output end of Y90S-2, the second motor 9 are fixed with hub body 12 by shaft, and the two sides of hub body 12 are provided with propeller blade
13, the two sides of hub body 12 are respectively and fixedly provided with fixed block 16, propeller blade 13 close to one end of fixed block 16 with 16 phase of fixed block
Hingedly, and the top of fixed block 16 is provided with curled portion, and the bottom end between fixed block 16 and propeller blade 13 is provided with
Spring leaf 17, and spring leaf 17 is recessed towards the direction far from propeller blade 13；
As shown in Fig. 2, device lands, preceding second motor 9 can stop operating first, and propeller blade 13 can be because of spring leaf 17
Elastic force flips up, and propeller blade 13, furthermore after being folded to a certain degree, screw blade are damaged when preventing device from landing
Piece 13 is in contact with curled portion, and curled portion limitation propeller blade 13 continues to fold, and prevents propeller blade 13 from folding excessively；
Four corners of 11 bottom of unmanned plane main body pass through damping 7 and are fixed with buffer board 15, and the bottom of buffer board 15
End is equipped with fixed frame 5, and the inside of fixed frame 5 is fixed with thermal imaging camera 3, and the model of thermal imaging camera 3 can be DS-
2TD4035D, fixed frame 5 is in reverse U-shaped structure, and the two sides inside fixed frame 5 are provided with ear 4 by turning ball 2,
Ear 4 is connect with thermal imaging camera 3, and the two sides of fixed frame 5 are mounted on first motor 1, and the model of first motor 1 can be
Y90L-2, and the output end of first motor 1 passes through shaft and connect with ball 2 is turned；
When shooting, first motor 1 is rotated by shaft band turn ball 2, allows to adjust the shooting angle of thermal imaging camera 3,
Meet various shooting demands；
Damping 7 includes support 703, movable block 702 and reset spring 701, and the bottom end of damping 7 is respectively and fixedly provided with support
703, and the longitudinal section of support 703 is in " recessed " type structure, the inside of support 703 passes through reset spring 701 and is fixed with activity
Block 702, and the top of movable block 702 is connect with the bottom end of unmanned plane main body 11；
As shown in figure 4, when device lands, the shaking force that can be generated with ground face contact, so that unmanned plane main body 11 is pressed down against
Movable block 702, movable block 702 pass through the screen resilience of reset spring 701 in 703 internal slide of support and pressed home spring 701
The shaking force of a part is absorbed, the impact force that slowing device generates when landing, avoiding device is by rigid collision；
The both ends of 11 bottom of unmanned plane main body are provided with undercarriage 6, the output end point of thermal imaging camera 3 and GPS locator 21
It is not electrically connected by the input terminal of conducting wire and central processing module 20, and the output end of central processing module 20 passes through lead respectively
Line and the input terminal of first motor 1, the second motor 9 and identification module 22 are electrically connected, and the output end of identification module 22 passes through
The input terminal of conducting wire and wireless communication module 19 is electrically connected.
Working principle: in use, luminous energy is transformed into electric energy by solar panel 10, electric current is transmitted by photovoltaic controller
It powers into battery 18 for device, thermal imaging camera 3 shoots petroleum pipeline outer wall situation when device flight, and utilizes thermal imaging
System, identifies the leakage of the heat-insulated hidden danger and transmission medium inside petroleum pipeline, the output end of thermal imaging camera 3 by conducting wire with
The input terminal of central processing module 20 is electrically connected, and the output end of central processing module 20 is defeated by conducting wire and identification module 22
Enter end to be electrically connected, by the petroleum pipeline damage information of identification, module 19 is transmitted to background terminal progress by wireless communication later
Detection, when shooting, first motor 1 allows to adjust the shooting angle of thermal imaging camera 3 by the shaft band rotation of turn ball 2,
Meet various shooting demands, when device lands, shaking force can be generated with ground face contact, so that unmanned plane main body 11 is pressed down against
Movable block 702, movable block 702 pass through the screen resilience of reset spring 701 in 703 internal slide of support and pressed home spring 701
The shaking force of a part, the impact force that slowing device generates when landing are absorbed, avoiding device is extended by rigid collision and uses the longevity
Life, while before device landing, the second motor 9 can stop operating first, and propeller blade 13 can be because of the bullet of spring leaf 17
Power flips up, when preventing device from landing damage propeller blade 13, fold to a certain extent after, propeller blade 13 with
Curled portion is in contact, and curled portion limitation propeller blade 13 continues to fold, and prevents propeller blade 13 from folding excessively, in addition,
GPS locator 21 in device is convenient for sending the real time position of unmanned plane main body 11 to the monitoring center of background terminal, in real time
Flight path is recorded, position is provided when device is lost, convenient for giving for change.
It is obvious to a person skilled in the art that invention is not limited to the details of the above exemplary embodiments, Er Qie
In the case where without departing substantially from spirit or essential attributes of the invention, the present invention can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the present invention is by appended power
Benefit requires rather than above description limits, it is intended that all by what is fallen within the meaning and scope of the equivalent elements of the claims
Variation is included within the present invention.Any reference signs in the claims should not be construed as limiting the involved claims.
Claims (6)
1. the unmanned plane that one kind can automatically detect internal and surface damage, including fixed frame (5), unmanned plane main body (11)
With propeller blade (13), it is characterised in that: it is equipped with solar panel (10) on the outside of the unmanned plane main body (11), and
The internal bottom end of unmanned plane main body (11) is provided with chamber (14), and the internal one end of the chamber (14) is equipped with battery
(18), it and in the chamber (14) of battery (18) side is equipped with central processing module (20), the central processing module (20)
It is equipped with wireless communication module (19) in the chamber (14) of lower section, and installation in the chamber (14) of wireless communication module (19) side
Have GPS locator (21), be equipped with identification module (22) in the chamber (14) of GPS locator (21) side, it is described nobody
Four corners of owner's body (11) are mounted on fixed link (8), and the top of fixed link (8) is mounted on the second motor (9),
The output end of second motor (9) is fixed with hub body (12) by shaft, and the two sides of hub body (12) are provided with propeller
Blade (13), four corners of unmanned plane main body (11) bottom pass through damping (7) and are fixed with buffer board (15),
And the bottom end of buffer board (15) is equipped with fixed frame (5), the inside of the fixed frame (5) is fixed with thermal imaging camera (3), described
The both ends of unmanned plane main body (11) bottom are provided with undercarriage (6).
2. the unmanned plane that one kind according to claim 1 can automatically detect internal and surface damage, feature exist
In: the fixed frame (5) is in reverse U-shaped structure, and the two sides of fixed frame (5) inside are provided with ear by turning ball (2)
Piece (4), the ear (4) connect with thermal imaging camera (3).
3. the unmanned plane that one kind according to claim 2 can automatically detect internal and surface damage, feature exist
In: the two sides of the fixed frame (5) are mounted on first motor (1), and the output end of first motor (1) passes through shaft and turns
Ball (2) connection.
4. the unmanned plane that one kind according to claim 1 can automatically detect internal and surface damage, feature exist
In: the damping (7) includes support (703), movable block (702) and reset spring (701), the bottom of damping (7)
End is respectively and fixedly provided with support (703), and the longitudinal section of support (703) is in " recessed " type structure, and the inside of the support (703) is logical
It crosses reset spring (701) to be fixed with movable block (702), and bottom end of the top of movable block (702) with unmanned plane main body (11)
Connection.
5. the unmanned plane that one kind according to claim 1 can automatically detect internal and surface damage, feature exist
In: the two sides of the hub body (12) are respectively and fixedly provided with fixed block (16), and the one of the propeller blade (13) close fixed block (16)
End is hinged with fixed block (16), and the top of fixed block (16) is provided with curled portion.
6. the unmanned plane that one kind according to claim 5 can automatically detect internal and surface damage, feature exist
In: the bottom end between the fixed block (16) and propeller blade (13) is provided with spring leaf (17), and spring leaf (17) is equal
It is recessed towards the direction far from propeller blade (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910582332.8A CN110254717A (en) | 2019-06-28 | 2019-06-28 | A kind of unmanned plane that internal and surface damage can be detected automatically |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910582332.8A CN110254717A (en) | 2019-06-28 | 2019-06-28 | A kind of unmanned plane that internal and surface damage can be detected automatically |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110254717A true CN110254717A (en) | 2019-09-20 |
Family
ID=67923361
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910582332.8A Pending CN110254717A (en) | 2019-06-28 | 2019-06-28 | A kind of unmanned plane that internal and surface damage can be detected automatically |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110254717A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN111086640A (en) * | 2020-03-06 | 2020-05-01 | 国网福建省电力有限公司三明供电公司 | Automatic inspection unmanned aerial vehicle based on visual identification |
| CN113022831A (en) * | 2021-04-29 | 2021-06-25 | 集美大学 | Vibration-damping noise-reducing self-adaptive ship lateral thruster |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN111086640A (en) * | 2020-03-06 | 2020-05-01 | 国网福建省电力有限公司三明供电公司 | Automatic inspection unmanned aerial vehicle based on visual identification |
| CN113022831A (en) * | 2021-04-29 | 2021-06-25 | 集美大学 | Vibration-damping noise-reducing self-adaptive ship lateral thruster |
| CN113022831B (en) * | 2021-04-29 | 2022-06-07 | 集美大学 | Vibration-damping noise-reducing self-adaptive ship lateral thruster |
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Application publication date: 20190920 |
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