CN112520029B - Unmanned aerial vehicle mapping device - Google Patents
Unmanned aerial vehicle mapping device Download PDFInfo
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- CN112520029B CN112520029B CN202011497660.7A CN202011497660A CN112520029B CN 112520029 B CN112520029 B CN 112520029B CN 202011497660 A CN202011497660 A CN 202011497660A CN 112520029 B CN112520029 B CN 112520029B
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- 238000013507 mapping Methods 0.000 title claims abstract description 22
- 238000013016 damping Methods 0.000 claims description 10
- 238000005096 rolling process Methods 0.000 claims description 6
- 230000008878 coupling Effects 0.000 abstract description 7
- 238000010168 coupling process Methods 0.000 abstract description 7
- 238000005859 coupling reaction Methods 0.000 abstract description 7
- 230000000694 effects Effects 0.000 abstract description 3
- 230000005389 magnetism Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 206010028836 Neck pain Diseases 0.000 description 1
- 235000008331 Pinus X rigitaeda Nutrition 0.000 description 1
- 235000011613 Pinus brutia Nutrition 0.000 description 1
- 241000018646 Pinus brutia Species 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013480 data collection Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000000452 restraining effect Effects 0.000 description 1
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- 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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- 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
- B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
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- 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
- B64C25/18—Operating mechanisms
- B64C25/24—Operating mechanisms electric
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- 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
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- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Closed-Circuit Television Systems (AREA)
- Studio Devices (AREA)
Abstract
The utility model relates to an unmanned aerial vehicle surveying and mapping device, including unmanned aerial vehicle, camera, remote control panel and display panel, be provided with the coupling mechanism who has the connection camera on the unmanned aerial vehicle, coupling mechanism includes the connecting seat of being connected with unmanned aerial vehicle, sets up horizontal rotating assembly on the connecting seat, sets up the vertical runner assembly on horizontal rotating assembly and sets up the clamping component who is used for fixed camera on the vertical runner assembly, horizontal rotating assembly's axis of rotation is laid along vertical direction, vertical rotating assembly's axis of rotation is laid along the horizontal direction. This application has the effect that improves user's adjustment camera and gathers direction stability.
Description
Technical Field
The application relates to the field of unmanned aerial vehicle survey and drawing, especially, relate to an unmanned aerial vehicle surveying and drawing device.
Background
The unmanned aerial vehicle surveying and mapping device is an auxiliary device for measuring and collecting the shape, size, spatial position, attributes and the like of natural geographic elements or surface artificial facilities, and is widely used in the surveying and mapping field.
Present unmanned aerial vehicle mapping device includes unmanned aerial vehicle, fixed camera, remote control panel and the display panel who sets up on unmanned aerial vehicle, and the user passes through remote control panel control unmanned aerial vehicle's flight, and camera data collection transmits to display panel on.
To the correlation technique among the above-mentioned, the inventor finds that the camera is mostly the snap-on unmanned aerial vehicle, if want the collection direction of adjustment camera, need control unmanned aerial vehicle and rotate, and unmanned aerial vehicle easily produces great shake at the rotation in-process to lead to the effect of making a video recording relatively poor, data acquisition is not very accurate.
Disclosure of Invention
In order to improve the stability of user's adjustment camera collection direction, this application provides an unmanned aerial vehicle mapping device.
The application provides a pair of unmanned aerial vehicle mapping device adopts following technical scheme:
the utility model provides an unmanned aerial vehicle mapping device, includes unmanned aerial vehicle, camera, remote control panel and display panel, be provided with the coupling mechanism who is used for connecting the camera on the unmanned aerial vehicle, coupling mechanism includes the connecting seat of being connected with unmanned aerial vehicle, set up horizontal rotating component on the connecting seat, set up vertical rotating assembly on horizontal rotating assembly and set up the clamping component who is used for fixed camera on vertical rotating assembly, horizontal rotating assembly's axis of rotation is laid along vertical direction, vertical rotating assembly's axis of rotation is laid along the horizontal direction.
Through adopting above-mentioned technical scheme, when using unmanned aerial vehicle mapping device to reconnoiter, the user passes through clamping component with the camera and fixes on coupling mechanism at first, then user operation remote control panel, control unmanned aerial vehicle flight, the camera is transmitted to display panel to the picture of shooing on, when the shooting angle of camera is adjusted to needs, the rotation of user accessible control level runner assembly and vertical runner assembly control camera, until the camera rotate to the angle that the user needs can, horizontal runner assembly and vertical runner assembly can drive the camera and carry out arbitrary angle change to the space of unmanned aerial vehicle below, improve user adjustment camera collection direction stability.
Optionally, the horizontal rotating assembly comprises a rotating frame fixedly connected with the connecting seat, a rotating disc rotatably arranged on the rotating frame, and a horizontal rotating motor which is fixed on the rotating frame along the vertical direction and coaxially connected with the rotating disc;
the longitudinal rotating assembly comprises a rotating seat rotating along with the rotating disc, a fixed seat rotatably arranged on the rotating seat and a longitudinal rotating motor fixed on the rotating seat along the horizontal direction and driving the fixed seat to rotate.
Through adopting above-mentioned technical scheme, when the shooting angle that the user need control the camera, the user starts the level and rotates the motor, the level rotates the motor and drives the rolling disc rotation, the rolling disc drives the camera and rotates along the horizontal direction, then start the longitudinal rotation motor, the longitudinal rotation motor drives the fixing base and takes place to rotate, and then drive the rotation that the camera took place longitudinal direction, reach user's needs up to the shooting angle of camera, the shooting angle of user's adjustment camera has been made things convenient for.
Optionally, the rotating seat comprises a rotating sleeve rotatably connected with the rotating frame and a gear ring coaxially sleeved in the rotating sleeve, a rotating axis of the rotating sleeve is arranged along the vertical direction, the rotating disc is provided with a gear, the rotating disc is kneaded with teeth of the gear ring, and the fixed seat is rotatably connected with one end of the rotating sleeve, which is far away from the rotating frame.
Through adopting above-mentioned technical scheme, when the horizontal turned angle who uses horizontal runner assembly control camera, start the horizontal rotation motor, the horizontal rotation motor drives the rolling disc and rotates, and the carousel drives the ring gear and rotates, and the ring gear drives the rotating sleeve and rotates, and then drives the camera and takes place to rotate, and the setting of rolling disc and ring gear has improved the stability when vertical runner assembly of horizontal runner assembly control rotates.
Optionally, the clamping assembly comprises a clamping frame connected with one end of the fixed seat, which is far away from the rotating seat, and two groups of clamping pieces arranged on the clamping frame in parallel;
the clamping piece includes with clamping frame fixed connection's first semicircle ring, one end and first semicircle ring articulated second semicircle ring and be used for the retaining member of fixed first semicircle ring and second semicircle ring, first semicircle ring and second semicircle ring form a ring of holding the camera tightly under the connection of retaining member, the retaining member sets up to the bolt.
Through adopting above-mentioned technical scheme, when using clamping component to press from both sides the fastening timing to the camera, open two clamping pieces earlier, unload the bolt through the pine, to keeping away from the direction rotation second semicircle ring of first semicircle ring, in first semicircle ring can be established to the card to the camera, then with the bolt with first semicircle ring and second semicircle ring fixed can, made things convenient for the staff to use clamping component to install or dismantle the camera.
Optionally, unmanned aerial vehicle is including the organism that is used for fixed camera, set up the wing at four extreme angle departments of organism respectively, set up at the wing and deviate from the power blade of organism one end and set up four landing legs in the organism below, the landing leg sets up to the landing leg that has shock-absorbing function.
Through adopting above-mentioned technical scheme, the landing leg on the unmanned aerial vehicle has shock-absorbing function, can effectual reduction unmanned aerial vehicle the vibrations that produce when descending, and then reduce the damage that unmanned aerial vehicle caused the camera when descending.
Optionally, the supporting leg comprises a telescopic sleeve connected with the machine body, a telescopic rod sleeved in the telescopic sleeve in a sliding manner, a placing plate connected with one end of the telescopic rod, which deviates from the telescopic sleeve, and a damping spring arranged in the telescopic sleeve, wherein two ends of the damping spring are respectively connected with the telescopic sleeve and the telescopic rod.
Through adopting above-mentioned technical scheme, when unmanned aerial vehicle descends subaerially, unmanned aerial vehicle is slow to fall into subaerially, and it is inconsistent with ground to place the board in the landing leg, and the telescopic link receives pressure this moment, drives damping spring and takes place deformation, makes telescopic link and flexible cover take place slight relative slip, and then alleviates the subaerial vibrations that produce of descending to unmanned aerial vehicle.
Optionally, a driving piece is arranged on the machine body and drives the supporting legs to rotate towards the machine wing, an accommodating groove for accommodating the supporting legs is formed in the machine wing, and the driving piece comprises a driving motor which is embedded in the machine body and coaxially connected with the supporting legs.
Through adopting above-mentioned technical scheme, when unmanned aerial vehicle rises on the ground, the resistance that unmanned aerial vehicle received mainly is the windage resistance, the size of windage resistance is directly proportional with unmanned aerial vehicle's lifting surface area, in order to reduce the windage resistance that unmanned aerial vehicle received, set up the landing leg and the organism to rotate and be connected, through starting driving motor, driving motor can drive the landing leg and rotate to the holding tank on the wing in, hide the landing leg, and then make unmanned aerial vehicle lack the windage resistance area of a landing leg, and then has had certain promotion to unmanned aerial vehicle's duration.
Optionally, the fin is provided with a fixing member in the accommodating groove for fixing the supporting leg, and the fixing member includes a fixing electromagnet embedded in the fin and a fixing magnetic block embedded in a position where the supporting leg faces the electromagnet.
Through adopting above-mentioned technical scheme, when the landing leg holds in the holding tank of machine wing, in order to improve the stability of landing leg, set up the mounting for this, fixed electro-magnet circular telegram produces magnetism, attracts mutually with the fixed magnetic path magnetism on the landing leg, with the stable restriction of landing leg in the holding tank, when letting need changeing the landing leg from the machine wing, need at first open the mounting, for the outage of fixed electro-magnet, the mounting is opened, can start driving motor and drive the landing leg and leave the machine wing.
Optionally, the limiting part used for fixing the supporting leg in the supporting state is arranged on the machine body, and the limiting part comprises a clamping groove plate arranged on the machine body and used for clamping the supporting leg, a limiting electromagnet arranged on the clamping groove plate, and a limiting magnetic block which is embedded on the supporting leg and is opposite to the limiting electromagnet.
Through adopting above-mentioned technical scheme for improve the stability of landing leg when supporting the organism state, set up the restriction piece on the organism, when the landing leg is located the draw-in groove board and is in the state that supports the organism, for the circular telegram of restriction electro-magnet, restriction electro-magnet produces magnetism, with the magnetism of restriction magnetic path on the landing leg magnetism, stability when having increased the landing leg and being in support state, when needs rotate the landing leg, to needs will restrict the electro-magnet outage, can start driving motor, move the landing leg away from the draw-in groove board.
Optionally, a GPS locator is arranged on the machine body, and the GPS locator is in signal connection with the control panel.
Through adopting the above-mentioned technical scheme, after unmanned aerial vehicle lifts off, the user need be raised the head just to unmanned aerial vehicle, then operation remote control panel, control unmanned aerial vehicle's flight, but the long-time head raising of user, the neck pain can appear, it is bigger to user's damage, set up the GPS locater for this reason on the organism, fix a position the height and the longitude and latitude at unmanned aerial vehicle place, and transmit to control panel on, the user can be according to the height and the flight of longitude and latitude control unmanned aerial vehicle that show on control panel, and needn't raise the head and look at unmanned aerial vehicle, and then made things convenient for the user to control the vogue to unmanned aerial vehicle.
In summary, the present application includes at least one of the following beneficial technical effects:
1. the connecting mechanism is arranged on the unmanned aerial vehicle, so that the camera can be driven to carry out any angle change on the space below the unmanned aerial vehicle, the requirement that a user shoots different angles by using the camera is met, and the stability of the camera when the shooting angle changes is improved;
2. after the unmanned aerial vehicle is lifted off, the supporting legs can be hidden in the wings, so that the area of wind resistance borne by the unmanned aerial vehicle is reduced, and the cruising ability of the unmanned aerial vehicle can be improved;
3. through set up the GPS locater on the organism, the user can be according to the height and the flight of longitude and latitude control unmanned aerial vehicle that show on the control panel, and needn't look at unmanned aerial vehicle again, and then made things convenient for the user to control the vogue to unmanned aerial vehicle.
Drawings
Fig. 1 is an overall schematic diagram of an embodiment of the present application.
Fig. 2 is a cross-sectional view of a leg embodied in an embodiment of the present application.
Fig. 3 is a cross-sectional view of an embodiment of the present application embodying a coupling mechanism.
Description of reference numerals: 1. an unmanned aerial vehicle; 11. a body; 111. a drive motor; 12. a machine wing; 121. accommodating a tank; 13. a power blade; 2. a support leg; 21. a telescopic sleeve; 22. a telescopic rod; 23. placing the plate; 24. a damping spring; 3. a fixing member; 31. fixing the electromagnet; 32. A fixed magnetic block; 4. a limiting member; 41. a slot clamping plate; 42. a restraining electromagnet; 43. a restricting magnetic block; 5. a GPS locator; 6. a connecting mechanism; 61. a connecting seat; 7. a horizontal rotation assembly; 71. a rotating frame; 72. rotating the disc; 73. a horizontal rotation motor; 8. a longitudinal rotation assembly; 81. rotating the base; 811. rotating the sleeve; 812. a ring gear; 82. a fixed seat; 83. longitudinally rotating the motor; 9. a clamping assembly; 91. a clamping frame; 92. a clamping member; 921. a first semicircular ring; 922. a second semi-circular ring; 923. a bolt; 924. a rubber pad; 10. a camera; 101. a remote control panel; 102. a display panel.
Detailed Description
The present application is described in further detail below with reference to figures 1-3.
The embodiment of the application discloses unmanned aerial vehicle mapping device. Referring to fig. 1, the surveying and mapping device includes unmanned aerial vehicle 1, camera 10, remote control panel 101 and display panel 102, and camera 10 sets up on unmanned aerial vehicle 1, and remote control panel 101 and unmanned aerial vehicle 1 signal connection, remote control panel 101 are used for controlling unmanned aerial vehicle 1's flight, and display panel 102 and camera 10 signal connection for show and record the picture that camera 10 shot.
As shown in fig. 1 and fig. 2, the unmanned aerial vehicle 1 includes a body 11, wings 12, power blades 13 and landing legs 2, the wings 12, the power blades 13 and the landing legs 2 are all provided with four, the four wings 12 are respectively fixed at four end angles of the body 11 along the horizontal direction, the four power blades 13 are respectively arranged at one ends of the four wings 12 departing from the body 11, the four landing legs 2 are respectively arranged below the four end angles of the body 11 for supporting the body 11, and the four landing legs 2 are respectively opposite to the four wings 12.
Be provided with GPS locater 5 on the organism 11, GPS fixes a position in the altitude that can unmanned aerial vehicle 1 and the longitude and latitude at place and detects, and GPS locater 5 and remote control panel 101 signal connection show remote control panel 101 with unmanned aerial vehicle 1's altitude and longitude and latitude on, the user can be according to unmanned aerial vehicle 1's altitude and longitude and latitude control unmanned aerial vehicle 1's flight.
The supporting leg 2 is a supporting leg 2 with a shock absorption function, the supporting leg 2 comprises a telescopic sleeve 21, a telescopic rod 22, a placing plate 23 and a shock absorption spring 24, the telescopic sleeve 21 is connected with the lower end part at the corner of the machine body 11, the telescopic rod 22 is slidably arranged in the telescopic sleeve 21 in a penetrating way, the placing plate 23 is fixed at one end of the telescopic rod 22 departing from the telescopic sleeve 21, and when the supporting legs 2 are in the state of supporting the machine body 11, the placing plate 23 can be completely propped against the ground, the damping spring 24 is arranged in the telescopic sleeve 21, one end of the damping spring 24 is fixedly connected with the telescopic sleeve 21, the other end of the damping spring 24 is fixedly connected with the telescopic rod 22, when unmanned aerial vehicle 1 descends to subaerial, the board 23 of placing in landing leg 2 is inconsistent with ground, and telescopic link 22 receives pressure this moment, drives damping spring 24 and takes place deformation, makes telescopic link 22 and telescopic sleeve 21 take place slight relative slip, and then alleviates the vibrations that unmanned aerial vehicle 1 descends to subaerial production.
In order to reduce the windage area size that unmanned aerial vehicle 1 received at the flight in-process, set up landing leg 2 to rotate with organism 11 and be connected, telescopic sleeve 21 in landing leg 2 rotates with organism 11 to be connected, the embedded driving motor 111 that is equipped with telescopic sleeve 21 coaxial coupling of organism 11, driving motor 111 drives landing leg 2 and can rotate to the direction towards wing 12, and set up the holding tank 121 that holds landing leg 2 on wing 12, after unmanned aerial vehicle 1 is liftoff, the user starts driving motor 111, drive landing leg 2 and rotate to holding tank 121 on wing 12 in, can be to reducing the windage area that unmanned aerial vehicle 1 received at the wind row in-process.
In order to improve the stability of the leg 2 in the stored state or the state of supporting the body 11, the fin 12 is provided with a fixing member 3 for fixing the leg 2 in the stored state, and the body 11 is provided with a restricting member 4 for fixing the leg 2 in the state of supporting the body 11.
Fixing piece 3 includes fixed electromagnet 31 and fixed magnet, fixed electromagnet 31 inlays the one end of establishing at wing 12 and keeping away from organism 11, and fixed electromagnet 31 is located holding tank 121, landing leg 2 is being provided with fixed magnet just to fixed electromagnet 31's rigidity, telescopic link 22 fixed connection in fixed magnet and the landing leg 2, restriction piece 4 includes draw-in groove board 41, restriction electromagnet 42 and restriction magnetic path 43, draw-in groove board 41 is fixed in the below of organism 11 extreme angle department, and be arranged in the telescope tube 21 of card in landing leg 2, restriction electromagnet 42 inlays and establishes in draw-in groove board 41, restriction magnetic path 43 inlays and establishes the position just to restriction electromagnet 42 at telescope tube 21, fixed electromagnet 31 and restriction electromagnet 42 all are connected with organism 11 electricity.
As shown in fig. 1 and 3, a connecting mechanism 6 for fixing the camera 10 is disposed at a lower end portion of the machine body 11, the connecting mechanism 6 includes a connecting seat 61, a horizontal rotating assembly 7, a longitudinal rotating assembly 8 and a clamping assembly 9, the connecting seat 61 is fixed at the lower end portion of the machine body 11, the horizontal rotating assembly 7 is disposed on the connecting seat 61 and can drive the camera 10 to rotate in a horizontal direction, the longitudinal rotating assembly 8 is disposed on the horizontal rotating assembly 7 and can drive the camera 10 to rotate in a vertical direction, and the clamping assembly 9 is disposed on the longitudinal rotating assembly 8 and is used for fixing the camera 10 on the longitudinal rotating assembly 8.
The horizontal rotating component 7 comprises a rotating frame 71, a rotating disc 72 and a horizontal rotating motor 73, the rotating frame 71 is fixed on the connecting seat 61, the rotating disc 72 is rotatably arranged on the rotating frame 71, the rotating disc 72 is arranged along the horizontal direction, the horizontal rotating motor 73 is fixed on the rotating frame 71 along the vertical direction, an output shaft of the horizontal rotating motor 73 is coaxially connected with the rotating disc 72, the longitudinal rotating component 8 comprises a rotating seat 81, a fixed seat 82 and a longitudinal rotating motor 83, the rotating seat 81 comprises a rotating sleeve 811 and a gear ring 812, the rotating sleeve 811 of the rotating sleeve 811 is arranged on the rotating frame 71, the gear ring 812 is coaxially sleeved and fixed on the inner peripheral wall of the rotating sleeve 811, the rotating disc 72 is provided with a gear, the rotating disc 72 is meshed with the gear ring 812, the fixed seat 82 is rotatably arranged on the rotating sleeve 811, the rotating axis of the fixed seat 82 is arranged along the horizontal direction, the longitudinal rotating motor 83 is fixed on the rotating sleeve 811 along the horizontal direction, and the output shaft of the longitudinal rotation motor 83 is coaxially and fixedly connected with the fixed seat 82.
The clamping assembly 9 is arranged on the fixed seat 82, the clamping assembly 9 comprises a clamping frame 91 and clamping pieces 92, the clamping frame 91 is fixedly arranged at the lower end part of the fixed seat 82, the clamping pieces 92 are arranged in two groups, the two groups of clamping pieces 92 are arranged in parallel, the clamping pieces 92 comprise first semi-circular rings 921, second semicircle ring 922 and bolt 923, first semicircle ring 921 opening is fixed the setting downwards in one side of clamping frame 91, the one end of second semicircle ring 922 is articulated with the one end of first semicircle ring 921, the other end of second semicircle ring 922 and the other end of first semicircle ring 921 pass through bolt 923 fixed connection, first semicircle ring 921 and second semicircle ring 922 form a circular ring of hugging closely camera 10 under the connection of bolt 923, all the adhesive bonding is fixed with rubber pad 924 on the internal perisporium of first semicircle ring 921 and second semicircle ring 922, a damage for reducing clamping assembly 9 and producing camera 10.
The implementation principle of the unmanned aerial vehicle surveying and mapping device in the embodiment of the application is as follows: when the user uses unmanned aerial vehicle 1 mapping device to survey and draw, the user is at first fixed on fixing base 82 through clamping assembly 9 with camera 101, then user operation remote control panel 101, according to the height that shows on the remote control panel 101 and longitude and latitude control unmanned aerial vehicle 1's flight, after unmanned aerial vehicle 1 rises to the air, user start-up driving motor 111, accomodate landing leg 2 in the wing 12, simultaneously camera 10 transmits to the picture of shooing on display panel 102, when needs adjust the shooting angle of camera 10, the user starts horizontal rotation motor 73 and longitudinal rotation motor 83, can drive camera 10 and carry out the angle change in unmanned aerial vehicle 1's below.
The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: equivalent changes in structure, shape and principle of the present application shall be covered by the protection scope of the present application.
Claims (8)
1. An unmanned aerial vehicle mapping device, includes unmanned aerial vehicle (1), camera (10), remote control panel (101) and display panel (102), its characterized in that: the unmanned aerial vehicle (1) is provided with a connecting mechanism (6) used for connecting a camera (10), the connecting mechanism (6) comprises a connecting seat (61) connected with the unmanned aerial vehicle (1), a horizontal rotating assembly (7) arranged on the connecting seat (61), a longitudinal rotating assembly (8) arranged on the horizontal rotating assembly (7) and a clamping assembly (9) arranged on the longitudinal rotating assembly (8) and used for fixing the camera (10), the rotating axis of the horizontal rotating assembly (7) is arranged along the vertical direction, and the rotating axis of the longitudinal rotating assembly (8) is arranged along the horizontal direction;
the horizontal rotating assembly (7) comprises a rotating frame (71) fixedly connected with the connecting seat (61), a rotating disc (72) rotatably arranged on the rotating frame (71) and a horizontal rotating motor (73) which is fixed on the rotating frame (71) along the vertical direction and is coaxially connected with the rotating disc (72); the longitudinal rotating assembly (8) comprises a rotating seat (81) rotating along with the rotating disc (72), a fixed seat (82) rotatably arranged on the rotating seat (81), and a longitudinal rotating motor (83) which is fixed on the rotating seat (81) along the horizontal direction and drives the fixed seat (82) to rotate;
rotate seat (81) and include rotating sleeve (811) and the coaxial ring gear (812) of establishing in rotating sleeve (811) with rotating turret (71) rotation and be connected, the axis of rotation that rotates sleeve (811) is laid along vertical direction, rolling disc (72) set up to the gear, rolling disc (72) and ring gear (812) tooth meshing, fixing base (82) are connected with rotating sleeve (811) one end rotation that deviates from rotating turret (71).
2. Unmanned aerial vehicle mapping device according to claim 1, characterized in that: the clamping assembly (9) comprises a clamping frame (91) connected with one end of the fixed seat (82) departing from the rotating seat (81) and two groups of clamping pieces (92) arranged on the clamping frame (91) in parallel;
clamping piece (92) include with clamping frame (91) fixed connection's first semicircle ring (921), one end and first semicircle ring (921) articulated second semicircle ring (922) and be used for fixed first semicircle ring (921) and second semicircle ring (922), first semicircle ring (921) and second semicircle ring (922) form a ring of holding camera (10) tightly under the connection of retaining member, the retaining member sets up to bolt (923).
3. An unmanned aerial vehicle surveying and mapping apparatus as defined in claim 1, wherein: unmanned aerial vehicle (1) including organism (11) that are used for fixed camera (10), set up wing (12) in four extreme angle departments of organism (11), set up power blade (13) that deviate from organism (11) one end at wing (12) and set up four landing leg (2) in organism (11) below, landing leg (2) set up to landing leg (2) that have shock-absorbing function.
4. An unmanned aerial vehicle surveying and mapping apparatus as claimed in claim 3, wherein: landing leg (2) including telescopic sleeve (21) be connected with organism (11), slip the cover establish telescopic link (22) in telescopic sleeve (21), deviate from board (23) and the damping spring (24) of placing that telescopic sleeve (21) one end is connected and setting in telescopic sleeve (21) with telescopic link (22), the both ends of damping spring (24) are connected with telescopic sleeve (21) and telescopic link (22) respectively.
5. Unmanned aerial vehicle mapping device according to claim 3, characterized in that: the novel electric power steering engine is characterized in that a driving piece for driving the supporting legs (2) to rotate towards the machine wings (12) is arranged on the engine body (11), accommodating grooves (121) for accommodating the supporting legs (2) are formed in the machine wings (12), and the driving piece comprises a driving motor (111) which is embedded in the engine body (11) and is coaxially connected with the supporting legs (2).
6. An unmanned aerial vehicle surveying and mapping apparatus as claimed in claim 5, wherein: the fin (12) is provided with a fixing piece (3) used for fixing the supporting leg (2) in the accommodating groove (121), and the fixing piece (3) comprises a fixing electromagnet (31) embedded in the fin (12) and a fixing magnetic block (32) embedded in the position, opposite to the electromagnet, of the supporting leg (2).
7. Unmanned aerial vehicle mapping device according to claim 6, characterized in that: be provided with restriction piece (4) when being used for fixed landing leg (2) to be in support state on organism (11), restriction piece (4) are including setting up draw-in groove board (41) on organism (11) and be used for the card to establish landing leg (2), setting up restriction electro-magnet (42) on draw-in groove board (41) and inlay and establish on landing leg (2) just to restriction magnetic path (43) of restriction electro-magnet (42).
8. An unmanned aerial vehicle surveying and mapping apparatus as claimed in claim 3, wherein: the GPS locator (5) is arranged on the machine body (11), and the GPS locator (5) is in signal connection with the control panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011497660.7A CN112520029B (en) | 2020-12-17 | 2020-12-17 | Unmanned aerial vehicle mapping device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011497660.7A CN112520029B (en) | 2020-12-17 | 2020-12-17 | Unmanned aerial vehicle mapping device |
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| Publication Number | Publication Date |
|---|---|
| CN112520029A CN112520029A (en) | 2021-03-19 |
| CN112520029B true CN112520029B (en) | 2022-08-23 |
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| CN202011497660.7A Active CN112520029B (en) | 2020-12-17 | 2020-12-17 | Unmanned aerial vehicle mapping device |
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| CN108639343A (en) * | 2018-05-03 | 2018-10-12 | 日照职业技术学院 | A kind of mapping unmanned plane |
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| CN210351340U (en) * | 2019-09-29 | 2020-04-17 | 天津华来科技有限公司 | Cloud platform structure and camera |
| CN211442798U (en) * | 2019-11-01 | 2020-09-08 | 山东慧宇航空遥感技术有限公司 | Unmanned aerial vehicle for three-dimensional modeling of aerial surveying and mapping |
| CN211107962U (en) * | 2019-11-20 | 2020-07-28 | 武汉数智云绘技术有限公司 | Mounting bracket for surveying and mapping unmanned aerial vehicle |
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