CN114476049B - Unmanned aerial vehicle convenient to patrol petroleum pipeline - Google Patents
Unmanned aerial vehicle convenient to patrol petroleum pipeline Download PDFInfo
- Publication number
- CN114476049B CN114476049B CN202210149372.5A CN202210149372A CN114476049B CN 114476049 B CN114476049 B CN 114476049B CN 202210149372 A CN202210149372 A CN 202210149372A CN 114476049 B CN114476049 B CN 114476049B
- Authority
- CN
- China
- Prior art keywords
- shell
- wing
- frame
- unmanned aerial
- aerial vehicle
- 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.)
- Active
Links
- 239000003208 petroleum Substances 0.000 title claims abstract description 24
- 230000007246 mechanism Effects 0.000 claims abstract description 49
- 238000012544 monitoring process Methods 0.000 claims abstract description 31
- 238000009434 installation Methods 0.000 claims description 16
- 238000007689 inspection Methods 0.000 claims description 14
- 230000001681 protective effect Effects 0.000 claims description 12
- 230000000903 blocking effect Effects 0.000 claims description 7
- 238000003780 insertion Methods 0.000 claims description 2
- 230000037431 insertion Effects 0.000 claims description 2
- 210000002105 tongue Anatomy 0.000 abstract 1
- 238000000034 method Methods 0.000 description 19
- 230000008569 process Effects 0.000 description 14
- 238000005096 rolling process Methods 0.000 description 11
- 238000012423 maintenance Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002146 bilateral effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/06—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/18—Heads with mechanism for moving the apparatus relatively to the stand
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V33/00—Structural combinations of lighting devices with other articles, not otherwise provided for
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The application discloses an unmanned aerial vehicle convenient for inspecting petroleum pipelines, which comprises a main body, a monitoring mechanism and a wing frame, wherein the main body comprises a main shell and a nose, the nose is arranged at the head part of the main shell and is fixedly connected with the main shell, the monitoring mechanism is arranged at the lower end surface of the main shell and is fixedly connected with the main shell, the wing frames are symmetrically arranged at two sides of the main shell and are detachably and fixedly connected with the main shell, the wing frames and the main shell are ensured to be stably arranged to be detachable by arranging the wing frames and the main body when a user needs to use, so that the user can conveniently and better flexibly replace the wing frames during loading, transporting and maintaining, the wing frames can be stably arranged by installing the wing frames at the upper end surface of the shell, the wing frames can be inserted into the middle part of the wing shells through inserting tongues when the wing frames need to be installed, and limit holes and inserting holes are mutually aligned.
Description
Technical Field
The application relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle which is convenient for inspecting petroleum pipelines.
Background
Unmanned plane is a unmanned plane which is controlled by radio remote control equipment and a self-provided program control device, has no cockpit, is provided with an autopilot, a program control device and other equipment, is aligned to track, position, remotely control, telemetere and digitally transmit by ground, naval or master remote control station personnel through radar and other equipment, and can often use corresponding unmanned plane to replace manual inspection task in petroleum pipeline inspection process.
The inventor of the application discovers that the existing unmanned aerial vehicle for inspecting petroleum pipelines has a simple structure, can only shoot at a fixed angle in the actual use process, so that the unmanned aerial vehicle cannot flexibly control and adjust the observation angle according to actual needs in the inspection process, cannot be flexibly stored when not used, is easy to damage, is inconvenient for long-distance inspection and use, and has a relatively fixed structure, and is inconvenient for users to flexibly dismount, so that the unmanned aerial vehicle is difficult to operate when maintenance is needed.
Disclosure of Invention
The application aims to provide an unmanned aerial vehicle which is convenient for inspecting petroleum pipelines, and aims to improve the defects that the existing unmanned aerial vehicle for inspecting petroleum pipelines is simple in structure, can only be shot at a fixed angle in the actual use process, so that the observation angle of the unmanned aerial vehicle cannot be flexibly controlled and adjusted according to actual needs in the inspection process, and can not be flexibly stored when the unmanned aerial vehicle is not used, the damage condition is easy to occur, the unmanned aerial vehicle cannot be conveniently inspected for a long time and remotely, the structure of the traditional unmanned aerial vehicle is relatively fixed, the unmanned aerial vehicle is inconvenient to flexibly disassemble, and the problem that the unmanned aerial vehicle is difficult to operate when maintenance is needed is solved.
The application is realized in the following way:
the utility model provides a conveniently patrol and examine unmanned aerial vehicle to petroleum pipeline, includes fuselage, monitoring mechanism and wing frame, the fuselage includes main shell and aircraft nose, the aircraft nose is installed at the head of main shell, and aircraft nose and main shell fixed connection, monitoring mechanism installs the lower terminal surface at the main shell, and monitoring mechanism and main shell fixed connection, wing frame symmetry sets up in the both sides of main shell, and wing frame and main shell can dismantle fixed connection, has solved the unmanned aerial vehicle that current petroleum pipeline patrolled and examined simple structure, often only can shoot with fixed angle in the in-process of in-service use, like this inconvenient unmanned aerial vehicle is in the in-process of patrolling and examining according to actual need control in a flexible way and is adjusted viewing angle, also unable nimble accomodate in the time of not using, the circumstances of damage appears very easily, and the unmanned aerial vehicle of being inconvenient for a long time patrol and examine the use, traditional unmanned aerial vehicle structure is comparatively fixed simultaneously, and inconvenient user is nimble dismantles, like this in the time operation of need maintenance comparatively difficult problem.
Further, the main shell includes casing and water conservancy diversion fin, water conservancy diversion fin symmetry sets up the end at the casing, and water conservancy diversion fin and casing fixed connection, the up end symmetry of casing is provided with the wing shell, wing shell and casing integrated into one piece, the mounting groove that is linked together with the wing shell has still been seted up at the middle part of casing up end, through setting up the structure to the main shell to guarantee the user and use through installing water conservancy diversion fin and wing shell to the casing, guarantee that the user can use through the stable installation wing frame of wing shell, use through guaranteeing stable installation fixed plate to the setting of mounting groove simultaneously.
Further, the protection box is still installed at the middle part of terminal surface under the casing, and the both sides of casing still symmetrically install and fall the frame, protection box and fall the frame all with casing fixed connection, conveniently accomodate and protect monitoring mechanism through setting up the protection box, guarantee the better use that falls of unmanned aerial vehicle through setting up to falling the frame simultaneously.
Further, the inside symmetry of mounting groove is provided with the jack, and the center department of mounting groove still installs connecting bolt, connecting bolt and casing vertical fixed connection, and install matched with stop nut on the connecting bolt, guarantee the stable installation of inserted bar through the setting to the jack, realize the purpose of fixing the fixed plate through setting up connecting bolt and stop nut simultaneously.
Further, still install the fixed plate in the mounting groove, four corners of terminal surface are provided with the inserted bar with jack matched with under the fixed plate, inserted bar and the perpendicular fixed connection of fixed plate, the centre bore corresponding with connecting bolt has still been seted up at the middle part of fixed plate, through the setting up to the fixed plate to guarantee stable installation inserted bar, the person of facilitating the use can carry out spacing and fixed purpose to the wing frame through the inserted bar, guarantees the purpose that connecting bolt can pass the fixed plate and fix through the setting up to the centre bore simultaneously.
Further, the monitoring mechanism comprises a driving frame, a movable frame and a shooting mechanism, wherein the movable frame is arranged in the middle of the driving frame, the shooting mechanism is arranged on the lower end face of the movable frame and is rotationally connected with the movable frame, a user can be ensured to install the movable frame through the driving frame by setting the structure of the monitoring mechanism, and the purpose of installing the shooting mechanism through the movable frame is facilitated for the user.
Further, the driving frame comprises a rotating motor and a threaded rod, the rotating motor is fixedly arranged on the lower end face of the shell, the threaded rod is horizontally arranged right below the shell, one end of the threaded rod is connected with the output end of the rotating motor, the other end of the threaded rod is rotationally connected with the shell, the purpose that a user can drive the threaded rod to flexibly rotate through controlling the rotating motor is guaranteed through structural arrangement of the driving frame, and the purpose that the movable block can be moved through the threaded rod is facilitated.
Further, the movable frame includes movable block and electric telescopic handle, the screw thread groove with threaded rod matched with is seted up at the middle part of movable block, and the bilateral symmetry of movable block is provided with removes the wheel, electric telescopic handle installs the lower terminal surface at the movable block, and electric telescopic handle rotates with the movable block to be connected, guarantees through setting up the structure to the movable frame that the user can install electric telescopic handle through the movable block, guarantees that the user can drive the purpose that changes shooting mechanism angle through controlling electric telescopic handle.
Further, shooting mechanism includes angle board, rolling disc and camera, the head at the angle board is installed to the rolling disc, and the rolling disc rotates with the angle board to be connected, camera fixed mounting is at the head of rolling disc, the middle part of angle board is fixed mounting has angle motor still, angle motor's output is connected with the center of rolling disc, still the symmetry is provided with the shot-light on the rolling disc, guarantees through setting up the structure to shooting mechanism that the user can install the rolling disc through the angle board, and the person of facilitating the use can install the camera through the rolling disc, guarantees that the user can drive the rolling disc through control angle motor and rotate change angle, and then realizes adjusting the different purpose of shining the position of shot-light.
Further, the wing frame includes main pterygoid lamina and side fender shell, the tip at main pterygoid lamina is installed to the side fender shell, and side fender shell and main pterygoid lamina fixed connection, the middle part of side fender shell is provided with the tongue, the spacing hole corresponding with the inserted bar has been seted up to the symmetry on the tongue, the power frame is still installed to the lower terminal surface of side fender shell, rotor motor is still installed to the symmetry on the power frame, rotor motor and power frame fixed connection, through setting up the structure to the wing frame to guarantee that main pterygoid lamina can be through the stable installation of side fender shell in the wing shell, simultaneously through setting up the tongue to the tongue in the stable insertion of inserting, simultaneously through setting up the power frame to stable installation rotor motor, guarantee that rotor motor drives the screw and provide power for unmanned aerial vehicle.
Compared with the prior art, the application has the beneficial effects that: the unmanned aerial vehicle structure and the use process for the conventional petroleum pipeline inspection are researched, the unmanned aerial vehicle convenient for the petroleum pipeline inspection is designed, a user can be ensured to stably arrange the wing frame and the airframe into a detachable mode when the unmanned aerial vehicle needs to be used, the unmanned aerial vehicle is convenient for the user to better flexibly replace during loading, transporting and maintaining, the wing frame can be stably arranged by arranging the wing shell on the upper end face of the shell, the wing frame can be inserted into the middle part of the wing shell through the inserting tongue when the wing frame needs to be arranged, the limiting hole and the inserting tongue are mutually aligned, the user can mutually fix the main shell and the inserting tongue through the fixing plate, the central hole is sleeved on the connecting bolt and then sequentially penetrates through the limiting hole and the inserting groove through the inserting rod to be fixed, the side blocking shell can be sleeved on the head part of the wing shell, the connection stability between the wing frame and the machine body is further ensured, the purpose of fixing the fixing plate can be realized by installing the limit nut on the connecting bolt after the fixing plate is installed, the fixing plate is convenient for a user to install and use quickly, when the user needs to replace the wing frame, the limit nut is only required to be detached from the connecting bolt, then the fixing plate is taken off from the connecting bolt, the locking can be canceled between the machine body and the wing frame, the wing frame can be easily taken off from the wing shell for replacement, the operation is very convenient, the monitoring mechanism is installed on the lower end face of the machine body to ensure that the exterior can be monitored in real time in the flight process of the unmanned aerial vehicle so as to facilitate the better completion of the inspection task, the rotation motor is fixedly installed on the lower end face of the main shell to realize flexible rotation of the driving threaded rod, simultaneously through the installation movable block that comes stable to the setting of threaded rod, guarantee that the user can realize driving the nimble purpose of removing of movable block through the rotation of control threaded rod, simultaneously guarantee that the movable block removes the in-process more stable through installing the movable wheel on the movable block, just so can control the movable block when the user does not need monitoring mechanism operation and drive the stable inside of removing the protective housing of shooting mechanism, guarantee to protect monitoring mechanism through the protective housing, avoid unmanned aerial vehicle to appear the condition of damaging monitoring mechanism in the removal in-process, just can remove it from the inside of protective housing when needs monitoring mechanism operation, then come nimble angle regulation angle plate's angle through control electric telescopic handle, and then reach the purpose of changing camera monitoring angle, the user sets up the shot-light on the rolling disc symmetrically simultaneously and realizes auxiliary lighting's purpose, guarantee that the user is better observes through the camera, moreover in-process user can also drive the rolling disc through controlling angle motor and rotate in a flexible way, just so can realize adjusting the shot-light and shine the purpose, it is very convenient to use.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some examples of the present application and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a perspective view of the device of the present application;
FIG. 2 is a top view of the device of FIG. 1;
FIG. 3 is a front view of the device of FIG. 1;
FIG. 4 is a perspective view of the device of FIG. 1 without the wing frame and mounting plate attached;
FIG. 5 is a top view of the device of FIG. 4;
FIG. 6 is a front view of the device of FIG. 4;
FIG. 7 is a perspective view of the wing mount shown in FIG. 1;
FIG. 8 is a schematic view of the mating configuration of the power frame and rotor motor of FIG. 2;
fig. 9 is a schematic structural view of the fixing plate shown in fig. 2.
In the figure: 1. a body; 11. a main housing; 111. a housing; 112. a diversion tail wing; 113. a wing shell; 114. a mounting groove; 115. a jack; 116. a connecting bolt; 117. a limit nut; 118. a protective box; 119. a falling frame; 12. a machine head; 13. a fixing plate; 131. a rod; 132. a central bore; 2. a monitoring mechanism; 21. a drive rack; 211. a rotating motor; 212. a threaded rod; 22. a movable frame; 221. a movable block; 222. an electric telescopic rod; 223. a moving wheel; 23. a photographing mechanism; 231. an angle plate; 232. a rotating disc; 233. a camera; 234. an angle motor; 235. a spotlight; 3. a wing frame; 31. a main wing plate; 32. a side shield shell; 321. inserting a tongue; 322. a limiting hole; 323. a power rack; 324. rotor motor.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present application more apparent, the technical solutions of the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present application, and it is apparent that the described embodiments are some embodiments of the present application, but not all embodiments. All other embodiments, based on the embodiments of the application, which are apparent to those of ordinary skill in the art without inventive faculty, are intended to be within the scope of the application. Thus, the following detailed description of the embodiments of the application, as presented in the figures, is not intended to limit the scope of the application, as claimed, but is merely representative of selected embodiments of the application. All other embodiments, based on the embodiments of the application, which are apparent to those of ordinary skill in the art without inventive faculty, are intended to be within the scope of the application.
Referring to the unmanned aerial vehicle which is convenient for inspecting petroleum pipelines and comprises a main body 1, a monitoring mechanism 2 and a wing frame 3, wherein the main body 1 comprises a main shell 11 and a nose 12, the nose 12 is arranged at the head part of the main shell 11, and the nose 12 is fixedly connected with the main shell 11, the unmanned aerial vehicle which is convenient for inspecting petroleum pipelines is designed by researching the structure and the using process of the unmanned aerial vehicle used for inspecting the traditional petroleum pipelines, the wing frame 3 and the main body 1 can be stably arranged to be detachable when a user needs to use, so that the wing frame 3 can be stably installed by installing the wing frame 113 on the upper end surface of the shell 111 during loading, transporting and maintaining, which is convenient for the user, when the wing frame 3 is required to be installed, the wing frame 3 can be inserted into the middle part of the wing shell 113 through the inserting tongue 321, and the limiting holes 322 and the inserting holes 115 are mutually aligned, so that a user can fix the main shell 11 and the inserting tongue 321 with each other through the fixing plate 13, sleeve the central hole 132 into the connecting bolt 116, then sequentially penetrate through the limiting holes 322 and the inserting holes 115 through the inserting rods 131 to fix, the side blocking shell 32 can be sleeved on the head part of the wing shell 113, the stability of connection between the wing frame 3 and the body 1 is further ensured, after the fixing plate 13 is installed, the purpose of fixing the fixing plate 13 can be realized through installing the limiting nuts 117 on the connecting bolt 116, the wing frame 3 can be quickly installed and used by a user, when the user is required to replace the wing frame 3, the limiting nuts 117 are only required to be detached from the connecting bolt 116, then the fixing plate 13 is taken down from the connecting bolt 116, then the locking between the machine body 1 and the wing frame 3 can be removed, the wing frame 3 can be easily taken down from the wing shell 113 for replacement, the operation is very convenient, the exterior can be monitored in real time in the flying process of the unmanned aerial vehicle by installing the monitoring mechanism 2 on the lower end face of the machine body 1, so that the unmanned aerial vehicle can better complete the inspection task, the driving threaded rod 212 can flexibly rotate by fixedly installing the rotating motor 211 on the lower end face of the main shell 11, meanwhile, the movable block 221 is stably arranged by arranging the threaded rod 212, the purpose of driving the movable block 221 to flexibly move can be ensured by controlling the rotation of the threaded rod 212, meanwhile, the movable block 221 is more stable in the moving process of the movable block 221 is ensured by installing the movable block 221, therefore, when a user does not need to operate the monitoring mechanism 2, the movable block 221 can be controlled to drive the shooting mechanism 23 to stably move into the protective box 118, the monitoring mechanism 2 is protected through the protective box 118, the condition that the unmanned aerial vehicle damages the monitoring mechanism 2 in the moving process is avoided, the unmanned aerial vehicle can be moved out of the protective box 118 when the monitoring mechanism 2 is required to operate, then the angle of the angle adjusting plate 231 is flexibly adjusted by controlling the electric telescopic rod 222, the aim of changing the monitoring angle of the camera 233 is fulfilled, meanwhile, the purpose of auxiliary illumination is realized by symmetrically arranging the spot lamps 235 on the rotating disc 232 by the user, the user can observe the spot lamps better through the camera 233, and the user can also drive the rotating disc 232 to flexibly rotate by controlling the angle motor 234 in the using process, so that the aim of adjusting the irradiation position of the spot lamps 235 can be realized, the unmanned aerial vehicle is very convenient to use, the unmanned aerial vehicle which effectively solves the problem that the existing petroleum pipeline inspection unmanned aerial vehicle is simple in structure, can only shoot at a fixed angle in the actual use process, so that the unmanned aerial vehicle cannot flexibly control and adjust the observation angle according to the actual needs in the inspection process, cannot be flexibly stored when not used, is very easy to damage, is inconvenient for long-time long-distance inspection and use, and meanwhile, the traditional unmanned aerial vehicle is relatively fixed in structure, is inconvenient for a user to flexibly dismount, so that the problem that the unmanned aerial vehicle is difficult to operate when maintenance is needed is solved;
the main shell 11 comprises a shell 111 and a guide tail 112, the guide tail 112 is symmetrically arranged at the tail end of the shell 111, the guide tail 112 is fixedly connected with the shell 111, the upper end face of the shell 111 is symmetrically provided with a wing shell 113, the wing shell 113 and the shell 111 are integrally formed, the middle part of the upper end face of the shell 111 is also provided with a mounting groove 114 communicated with the wing shell 113, the structure of the main shell 11 is used for ensuring that a user can mount the guide tail 112 and the wing shell 113 for use through the shell 111, the user can stably mount the wing frame 3 for use through the wing shell 113, meanwhile, the mounting groove 114 is used for ensuring stable mounting of a fixed plate 13, the middle part of the lower end face of the shell 111 is also provided with a protective box 118, two sides of the shell 111 are symmetrically provided with a drop frame 119, the protective box 118 and the drop frame 119 are fixedly connected with the shell 111, the monitoring mechanism 2 is conveniently stored and protected through the arrangement of the protective box 118, the unmanned aerial vehicle is ensured to fall better through the arrangement of the falling frame 119, the jack 115 is symmetrically arranged in the installation groove 114, the connecting bolt 116 is further arranged at the center of the installation groove 114, the connecting bolt 116 is vertically and fixedly connected with the shell 111, the connecting bolt 116 is provided with the matched limit nut 117, the stable installation of the inserting rod 131 is ensured through the arrangement of the jack 115, the fixing plate 13 is simultaneously realized through the arrangement of the connecting bolt 116 and the limit nut 117, the fixing plate 13 is further arranged in the installation groove 114, the four corners of the lower end face of the fixing plate 13 are provided with inserting rods 131 matched with the jack 115, the inserting rods 131 are vertically and fixedly connected with the fixing plate 13, the middle part of the fixing plate 13 is further provided with a center hole 132 corresponding to the connecting bolt 116, through the arrangement of the fixing plate 13, the stable installation of the inserted link 131 is ensured, so that a user can conveniently limit and fix the wing frame 3 through the inserted link 131, and meanwhile, through the arrangement of the center hole 132, the purpose that the connecting bolt 116 can penetrate through the fixing plate 13 for fixing is ensured;
the monitoring mechanism 2 is arranged on the lower end face of the main shell 11, the monitoring mechanism 2 is fixedly connected with the main shell 11, the monitoring mechanism 2 comprises a driving frame 21, a movable frame 22 and a shooting mechanism 23, the movable frame 22 is arranged in the middle of the driving frame 21, the shooting mechanism 23 is arranged on the lower end face of the movable frame 22, the shooting mechanism 23 is rotationally connected with the movable frame 22, a user can mount the movable frame 22 through the driving frame 21 by arranging the structure of the monitoring mechanism 2, the user can conveniently mount the shooting mechanism 23 through the movable frame 22, the driving frame 21 comprises a rotating motor 211 and a threaded rod 212, the rotating motor 211 is fixedly arranged on the lower end face of the shell 111, the threaded rod 212 is horizontally arranged under the shell 111, one end of the threaded rod 212 is connected with the output end of the rotating motor 211, the other end of the threaded rod 212 is rotationally connected with the shell 111, the purpose that a user can drive the threaded rod 212 to flexibly rotate by controlling the rotating motor 211 is ensured by setting the structure of the driving frame 21, the purpose that the user can drive the movable block 221 by controlling the threaded rod 212 is facilitated, the movable frame 22 comprises the movable block 221 and the electric telescopic rod 222, the middle part of the movable block 221 is provided with a thread groove matched with the threaded rod 212, the two sides of the movable block 221 are symmetrically provided with the moving wheel 223, the electric telescopic rod 222 is arranged on the lower end surface of the movable block 221, the electric telescopic rod 222 is rotationally connected with the movable block 221, the electric telescopic rod 222 is ensured by setting the structure of the movable frame 22, the purpose that the user can drive the shooting mechanism 23 to change the angle by controlling the electric telescopic rod 222 is ensured, the shooting mechanism 23 comprises an angle plate 231, a rotating disc 232 and a camera 233, the rotating disc 232 is arranged on the head part of the angle plate 231, the rotating disc 232 is rotationally connected with the angle plate 231, the camera 233 is fixedly arranged at the head of the rotating disc 232, the middle part of the angle plate 231 is fixedly provided with the angle motor 234, the output end of the angle motor 234 is connected with the center of the rotating disc 232, the rotating disc 232 is symmetrically provided with the spotlight 235, the structure of the shooting mechanism 23 is arranged to ensure that a user can install the rotating disc 232 through the angle plate 231, the user can conveniently install the camera 233 through the rotating disc 232, and the user can drive the rotating disc 232 to rotate and change angles through controlling the angle motor 234, so that the aim of adjusting different irradiation positions of the spotlight 235 is fulfilled;
wing frame 3 symmetry sets up in the both sides of main casing 11, and wing frame 3 and main casing 11 can dismantle fixed connection, wing frame 3 includes main wing plate 31 and side fender shell 32, the tip at main wing plate 31 is installed to side fender shell 32, and side fender shell 32 and main wing plate 31 fixed connection, the middle part of side fender shell 32 is provided with inserts tongue 321, the spacing hole 322 corresponding with inserted bar 131 has been seted up to the symmetry on inserting tongue 321, power frame 323 is still installed to the lower terminal surface of side fender shell 32, rotor motor 324 is still installed to the symmetry on the power frame 323, rotor motor 324 and power frame 323 fixed connection, through setting up the structure to wing frame 3, guarantee that main wing plate 31 can be through the stable installation of side fender shell 32 in wing shell 113, simultaneously through the setting up to inserting tongue 321 in the stable wing shell 113, simultaneously guarantee better to insert tongue 321 and fix through setting up to power frame 323 stable installation motor 324, guarantee that motor 324 drives the screw to provide power for the unmanned aerial vehicle.
The device obtained through the design can basically meet the requirement of being convenient for the unmanned aerial vehicle to patrol the petroleum pipeline, but the designer further improves the device on the basis of the aim of further improving the functions of the unmanned aerial vehicle.
The above description is only of the preferred embodiments of the present application and is not intended to limit the present application, and various modifications and variations may be made to the present application by those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application should be included in the protection scope of the present application.
Claims (7)
1. The utility model provides a conveniently patrol unmanned aerial vehicle of examining to petroleum pipeline, includes fuselage (1), monitoring mechanism (2) and wing frame (3), its characterized in that: the machine body (1) comprises a main shell (11) and a machine head (12), the machine head (12) is arranged at the head of the main shell (11), the machine head (12) is fixedly connected with the main shell (11), the monitoring mechanism (2) is arranged on the lower end face of the main shell (11), the monitoring mechanism (2) is fixedly connected with the main shell (11), the wing frames (3) are symmetrically arranged on two sides of the main shell (11), and the wing frames (3) are detachably and fixedly connected with the main shell (11); the main shell (11) comprises a shell (111) and a guide tail fin (112), wherein the guide tail fin (112) is symmetrically arranged at the tail end of the shell (111), the guide tail fin (112) is fixedly connected with the shell (111), a wing shell (113) is symmetrically arranged on the upper end surface of the shell (111), the wing shell (113) and the shell (111) are integrally formed, and an installation groove (114) communicated with the wing shell (113) is formed in the middle of the upper end surface of the shell (111); the middle part of the lower end surface of the shell (111) is also provided with a protective box (118), two sides of the shell (111) are symmetrically provided with drop frames (119), and the protective box (118) and the drop frames (119) are fixedly connected with the shell (111); the inside symmetry of mounting groove (114) is provided with jack (115), and the center department of mounting groove (114) still installs connecting bolt (116), connecting bolt (116) and casing (111) vertical fixed connection, and install matched with stop nut (117) on connecting bolt (116).
2. The unmanned aerial vehicle convenient for inspecting petroleum pipelines according to claim 1, wherein a fixing plate (13) is further installed in the installation groove (114), four corners of the lower end face of the fixing plate (13) are provided with inserted bars (131) matched with the insertion holes (115), the inserted bars (131) are vertically and fixedly connected with the fixing plate (13), and a central hole (132) corresponding to the connecting bolt (116) is further formed in the middle of the fixing plate (13).
3. The unmanned aerial vehicle for facilitating inspection of petroleum pipelines according to claim 2, wherein the monitoring mechanism (2) comprises a driving frame (21), a movable frame (22) and a shooting mechanism (23), the movable frame (22) is installed in the middle of the driving frame (21), the shooting mechanism (23) is installed on the lower end face of the movable frame (22), and the shooting mechanism (23) is rotationally connected with the movable frame (22).
4. An unmanned aerial vehicle for facilitating inspection of petroleum pipelines according to claim 3, wherein the driving frame (21) comprises a rotating motor (211) and a threaded rod (212), the rotating motor (211) is fixedly arranged on the lower end face of the casing (111), the threaded rod (212) is horizontally arranged right below the casing (111), one end of the threaded rod (212) is connected with the output end of the rotating motor (211), and the other end of the threaded rod (212) is rotationally connected with the casing (111).
5. The unmanned aerial vehicle convenient to patrol petroleum pipelines according to claim 4, wherein the movable frame (22) comprises a movable block (221) and an electric telescopic rod (222), a thread groove matched with the threaded rod (212) is formed in the middle of the movable block (221), moving wheels (223) are symmetrically arranged on two sides of the movable block (221), the electric telescopic rod (222) is mounted on the lower end face of the movable block (221), and the electric telescopic rod (222) is rotationally connected with the movable block (221).
6. The unmanned aerial vehicle for conveniently inspecting petroleum pipelines according to claim 5, wherein the shooting mechanism (23) comprises an angle plate (231), a rotating disc (232) and a camera (233), the rotating disc (232) is installed at the head of the angle plate (231), the rotating disc (232) is rotationally connected with the angle plate (231), the camera (233) is fixedly installed at the head of the rotating disc (232), an angle motor (234) is fixedly installed in the middle of the angle plate (231), the output end of the angle motor (234) is connected with the center of the rotating disc (232), and a spotlight (235) is symmetrically arranged on the rotating disc (232).
7. The unmanned aerial vehicle convenient for inspecting petroleum pipelines according to any one of claims 2-6, wherein the wing frame (3) comprises a main wing plate (31) and a side blocking shell (32), the side blocking shell (32) is arranged at the end part of the main wing plate (31), the side blocking shell (32) is fixedly connected with the main wing plate (31), an inserting tongue (321) is arranged in the middle of the side blocking shell (32), limiting holes (322) corresponding to the inserting rods (131) are symmetrically formed in the inserting tongue (321), a power frame (323) is further arranged on the lower end face of the side blocking shell (32), a rotor motor (324) is symmetrically arranged on the power frame (323), and the rotor motor (324) is fixedly connected with the power frame (323).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210149372.5A CN114476049B (en) | 2022-02-18 | 2022-02-18 | Unmanned aerial vehicle convenient to patrol petroleum pipeline |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210149372.5A CN114476049B (en) | 2022-02-18 | 2022-02-18 | Unmanned aerial vehicle convenient to patrol petroleum pipeline |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN114476049A CN114476049A (en) | 2022-05-13 |
| CN114476049B true CN114476049B (en) | 2023-11-28 |
Family
ID=81483344
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210149372.5A Active CN114476049B (en) | 2022-02-18 | 2022-02-18 | Unmanned aerial vehicle convenient to patrol petroleum pipeline |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114476049B (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013048339A1 (en) * | 2011-09-27 | 2013-04-04 | Singapore Technologies Aerospace Ltd | An unmanned aerial vehicle |
| WO2016141742A1 (en) * | 2015-03-12 | 2016-09-15 | 杨华东 | Fixed-wing unmanned aircraft capable of being quickly disassembled and installed |
| WO2018113202A1 (en) * | 2016-12-23 | 2018-06-28 | 深圳市道通智能航空技术有限公司 | Detachable pan-tilt connection device and unmanned aerial vehicle |
| CN108438200A (en) * | 2018-05-11 | 2018-08-24 | 南京航天猎鹰飞行器技术有限公司 | A kind of fixed-wing unmanned plane of fast demountable wing |
| CN208360486U (en) * | 2018-06-29 | 2019-01-11 | 深圳臻迪信息技术有限公司 | A kind of wing of unmanned plane wing quick-disassembly structure and unmanned plane |
| CN211281480U (en) * | 2019-11-14 | 2020-08-18 | 强国羽翼无人机应用技术有限公司 | Portable survey and drawing unmanned aerial vehicle |
| CN113165732A (en) * | 2018-11-30 | 2021-07-23 | 斯凯卡诺公司 | Aircraft with enhanced pitch control and interchangeable components |
| CN214824104U (en) * | 2021-04-30 | 2021-11-23 | 航天数维高新技术股份有限公司 | Unmanned aerial vehicle |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9623969B2 (en) * | 2015-01-17 | 2017-04-18 | Brian Dale Nelson | Multicopter with detachable wing |
-
2022
- 2022-02-18 CN CN202210149372.5A patent/CN114476049B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013048339A1 (en) * | 2011-09-27 | 2013-04-04 | Singapore Technologies Aerospace Ltd | An unmanned aerial vehicle |
| WO2016141742A1 (en) * | 2015-03-12 | 2016-09-15 | 杨华东 | Fixed-wing unmanned aircraft capable of being quickly disassembled and installed |
| WO2018113202A1 (en) * | 2016-12-23 | 2018-06-28 | 深圳市道通智能航空技术有限公司 | Detachable pan-tilt connection device and unmanned aerial vehicle |
| CN108438200A (en) * | 2018-05-11 | 2018-08-24 | 南京航天猎鹰飞行器技术有限公司 | A kind of fixed-wing unmanned plane of fast demountable wing |
| CN208360486U (en) * | 2018-06-29 | 2019-01-11 | 深圳臻迪信息技术有限公司 | A kind of wing of unmanned plane wing quick-disassembly structure and unmanned plane |
| CN113165732A (en) * | 2018-11-30 | 2021-07-23 | 斯凯卡诺公司 | Aircraft with enhanced pitch control and interchangeable components |
| CN211281480U (en) * | 2019-11-14 | 2020-08-18 | 强国羽翼无人机应用技术有限公司 | Portable survey and drawing unmanned aerial vehicle |
| CN214824104U (en) * | 2021-04-30 | 2021-11-23 | 航天数维高新技术股份有限公司 | Unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN114476049A (en) | 2022-05-13 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106151827B (en) | Detachable screen type display | |
| CN206542120U (en) | Overhead transmission line damages auto-mending machine | |
| CN114476049B (en) | Unmanned aerial vehicle convenient to patrol petroleum pipeline | |
| CN115781756B (en) | Single lamp controller aerial automatic replacement device based on UAV platform | |
| CN106025983A (en) | Overhead wire cable deicing unmanned plane | |
| CN214844000U (en) | Aeroengine detects with examining test table | |
| CN203845019U (en) | Unmanned helicopter inspection tour device carrying device for substation | |
| CN217805290U (en) | A tracer particle throws device for unmanned aerial vehicle video current surveying | |
| CN216291122U (en) | Aviation video acquisition recording device based on PCIE bus | |
| CN220640247U (en) | A vertical take-off and landing fixed-wing electric power inspection drone | |
| CN213008787U (en) | But angle regulation's unmanned aerial vehicle aviation magnetic method magnetometer probe's fixing base | |
| CN210165097U (en) | Parking area surveillance camera head cloud platform device | |
| CN212047922U (en) | Unmanned aerial vehicle for monitoring | |
| CN210319119U (en) | A high-altitude monitoring installation structure that is easy to repair and maintain | |
| CN207791186U (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN220315327U (en) | Unmanned aerial vehicle survey and drawing's camera lens protective structure | |
| CN219687019U (en) | Vehicle-mounted air conditioner protective cover | |
| CN219247945U (en) | Wireless tripod head camera | |
| CN217348245U (en) | 10KV pole tower remote data acquisition machine-mounted device | |
| CN217836049U (en) | Unmanned aerial vehicle aerial survey device | |
| CN218662366U (en) | A injection apparatus that is used for unmanned aerial vehicle to carry on formula dry ice scrubbing system | |
| CN217673263U (en) | Wind turbine blade inspection device based on unmanned aerial vehicle | |
| CN218216362U (en) | Overhead line maintenance system | |
| CN222859726U (en) | Unmanned aerial vehicle removes snow stick and throws device | |
| CN109212708B (en) | High definition optical lens and support of taking photo by plane |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |