CN117087888A - But shooting angle autogiration's remote sensing survey and drawing unmanned aerial vehicle - Google Patents
But shooting angle autogiration's remote sensing survey and drawing unmanned aerial vehicle Download PDFInfo
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- CN117087888A CN117087888A CN202311152752.5A CN202311152752A CN117087888A CN 117087888 A CN117087888 A CN 117087888A CN 202311152752 A CN202311152752 A CN 202311152752A CN 117087888 A CN117087888 A CN 117087888A
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- 238000013507 mapping Methods 0.000 claims abstract description 32
- 230000007246 mechanism Effects 0.000 claims abstract description 27
- 230000002159 abnormal effect Effects 0.000 claims description 39
- 230000000903 blocking effect Effects 0.000 claims description 20
- 238000002955 isolation Methods 0.000 claims description 19
- 230000033001 locomotion Effects 0.000 claims description 18
- 230000005540 biological transmission Effects 0.000 claims description 9
- 238000001125 extrusion Methods 0.000 claims description 9
- 238000007790 scraping Methods 0.000 claims description 8
- 238000004140 cleaning Methods 0.000 claims description 7
- 238000009958 sewing Methods 0.000 claims description 6
- 230000003068 static effect Effects 0.000 claims description 6
- 230000000007 visual effect Effects 0.000 claims 3
- 238000003384 imaging method Methods 0.000 description 10
- 238000009434 installation Methods 0.000 description 7
- 230000003139 buffering effect Effects 0.000 description 6
- 208000012661 Dyskinesia Diseases 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000000630 rising effect Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 238000003825 pressing Methods 0.000 description 3
- 241000883990 Flabellum Species 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 241001465754 Metazoa Species 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000001174 ascending effect Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000012780 transparent material Substances 0.000 description 1
- 230000036642 wellbeing Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
-
- 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
-
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U60/00—Undercarriages
- B64U60/50—Undercarriages with landing legs
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- 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
- F16M11/08—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting around a vertical axis, e.g. panoramic heads
-
- 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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention belongs to the technical field of unmanned aerial vehicles, in particular to a remote sensing surveying and mapping unmanned aerial vehicle with an automatically rotating shooting angle, when the remote sensing surveying and mapping unmanned aerial vehicle in the prior art is used, the shooting angle of a carried shooting module can be adjusted only through the rotation of the unmanned aerial vehicle, the shooting angle can not be adjusted at any time according to the requirement, and the remote sensing surveying and mapping unmanned aerial vehicle has strong limitation and reduces the surveying and mapping efficiency; the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a plurality of support arms are arranged on the unmanned aerial vehicle body and are connected with a lifting self-moving mechanism; the lifting self-moving mechanism comprises a lifting cylinder arranged on the support arm, a lifting rotating shaft is arranged on the lifting cylinder, one end of the lifting rotating shaft is fixedly connected with the fan blades, and the other end of the lifting rotating shaft is provided with a lifting rotating groove; through the whole mechanism of stadia, the required angle of shooting of module of making a video recording of real-time adjustment avoids adjusting the angle of shooting through unmanned aerial vehicle body rotation, has reduced the limitation of device when using, has promoted the efficiency of survey and drawing simultaneously.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a remote sensing surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle.
Background
Unmanned aerial vehicles, abbreviated as "unmanned aerial vehicles", abbreviated as "UAVs", are unmanned aerial vehicles that are operated by means of radio remote control devices and self-contained programmed control devices, or are operated autonomously, either entirely or intermittently, by an onboard computer. Unmanned aircraft tend to be more suitable for tasks that are too "fooled, messy, or dangerous" than manned aircraft. Unmanned aerial vehicles can be classified into military and civilian applications according to the field of application. For military purposes, unmanned aerial vehicles are classified into reconnaissance and drones. In civil aspect, the unmanned aerial vehicle and the industrial application are really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and the developed countries are also actively expanding the application of industries and developing unmanned aerial vehicle technologies.
When the remote sensing surveying unmanned aerial vehicle in the prior art is used, the carried camera module can only adjust the shooting angle through the rotation of the unmanned aerial vehicle, can not adjust the shooting angle at any time according to the requirement, has strong limitation, and simultaneously reduces the surveying efficiency.
Disclosure of Invention
Aiming at the situation, in order to overcome the defects of the prior art, the invention provides the remote sensing surveying and mapping unmanned aerial vehicle capable of automatically rotating the shooting angle, and the problems in the background art are effectively solved.
In order to achieve the above purpose, the present invention provides the following technical solutions: the remote sensing surveying and mapping unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein a plurality of support arms are arranged on the unmanned aerial vehicle body, and the support arms are connected with a lifting self-moving mechanism;
the lifting self-moving mechanism comprises a lifting cylinder arranged on the support arm, a lifting rotating shaft is arranged on the lifting cylinder, one end of the lifting rotating shaft is fixedly connected with the fan blades, the other end of the lifting rotating shaft is provided with a lifting rotating groove, the lifting rotating groove is connected with a lifting rotating block, the lifting rotating block is connected with the output end of a lifting motor, lifting clamping seats are symmetrically arranged on the lifting motor, and the two lifting clamping seats are connected with the lifting cylinder together; the unmanned aerial vehicle body is fixedly provided with an inserting box and a linkage base, and the linkage base is connected with the descending motion slow-moving mechanism; the inserting box and the isolating square box are connected through a clamping and fastening unit.
Preferably, the clamping and fastening unit comprises a first rubber block and a second rubber block which are connected with the square isolation box in a matched manner; the movable square box is connected with the double-system sewing and linking assembly in a matched manner; the first rubber blocks are fixedly connected with the partition plates arranged in the inserting box, the second rubber blocks are fixedly connected with the clamping square plates, clamping rods are symmetrically arranged on the clamping square plates, and the two clamping rods penetrate through the inserting box and are fixedly connected with the blocking circular plate.
Preferably, the clamping rod is sleeved with a clamping spring, one end of the clamping spring is fixedly connected with the inserting box, and the other end of the clamping spring is fixedly connected with the blocking circular plate; a lifting handle is fixedly arranged on the blocking circular plate; the stop circular plate is provided with a limit sliding block which is in sliding connection with a limit sliding groove arranged on the unmanned aerial vehicle body; and a limiting rod is fixedly arranged on the limiting sliding groove, a limiting spring is sleeved on the limiting rod, one end of the limiting spring is fixedly connected with the limiting sliding groove, and the other end of the limiting spring is fixedly connected with the limiting sliding block.
Preferably, the descending and slow moving mechanism comprises a linkage rotating shaft arranged on a linkage base, a linkage square block is arranged on the linkage rotating shaft, a linkage plate is arranged on the linkage square block, a descending round block is fixedly arranged on the linkage plate, and a buffer cushion is arranged on the descending round block; the two ends of the linkage rotating shaft penetrate through the linkage base and are fixedly connected with the abnormal inclined block, and the abnormal inclined block is connected with the abnormal inclined rod; the two ends of the abnormal inclined rod are fixedly connected with abnormal bases fixedly arranged on the unmanned aerial vehicle body; the special-shaped oblique rod is characterized in that a special-shaped spring is sleeved on the special-shaped oblique rod, one end of the special-shaped spring is fixedly connected with the special-shaped base, the other end of the special-shaped spring is fixedly connected with the special-shaped oblique block, an extension plate is arranged on the special-shaped oblique block, a movable contact piece is arranged on the extension plate, the movable contact piece is connected with a static contact piece arranged on the special-shaped base in a matched mode, and the movable contact piece is connected with a fixed locking control assembly in a contact mode.
Preferably, the double-system sewing assembly comprises a brake inserting plate arranged on the outer plate of the square box for isolating movement, and the brake inserting plate is connected with a brake inserting slot arranged on the square box for inserting movement; the movable square box is connected with the movable square plate in a matched manner, a plurality of positioning blocks are arranged on the movable square plate, and the positioning blocks are connected with positioning grooves arranged on the movable box in a sliding manner; the inner bottom surface of the inserting box is fixedly connected with the annular moving square plate through an extrusion spring, a plurality of annular moving long blocks are mounted on the annular moving square plate and are connected with an annular moving sleeve arranged in the inserting box in a matched mode, one main magnetic sheet is mounted in the annular moving sleeve, the main magnetic sheet is connected with auxiliary magnetic sheets arranged on the annular moving long blocks in a matched mode, and the main magnetic sheet is connected with an eye distance adjusting mechanism in a contact mode.
Preferably, a plurality of annular moving racks are arranged on the annular moving square plate, the annular moving racks are meshed with an annular moving gear, an annular moving threaded shaft is arranged on the annular moving gear, one end of the annular moving threaded shaft is connected with the double-acting plate, and the other end of the annular moving threaded shaft is in transmission connection with the inserting box; the double-acting square plate is arranged on the annular moving threaded shaft in a threaded manner, and a limiting block is arranged on the double-acting square plate and is in sliding connection with a limiting rod fixedly arranged on the inserting box; the double-acting square plate is fixedly provided with a double-acting different plate, the double-acting different plate is provided with a double-acting rod, one end of the double-acting rod is fixedly connected with the double-acting circular plate, and the other end of the double-acting rod is fixedly connected with the movable square plate; the double-acting rod is sleeved with a double-acting spring, one end of the double-acting spring is fixedly connected with the movable square plate, and the other end of the double-acting spring is fixedly connected with the double-acting differential plate.
Preferably, the fixed lock accuse subassembly is including the symmetry setting up the locking square board on spacing slider, and fixed mounting has flexible motor on the locking square board, is equipped with the locking square on flexible motor's the output, and the locking square cooperates with the locking square groove that is equipped with on the unmanned aerial vehicle body to be connected and sets up.
Preferably, the sight distance adjusting mechanism comprises a distance moving clamping seat arranged on the inserting and moving box, a sight distance motor is fixedly arranged on the distance moving clamping seat, a moment moving gear is arranged at the output end of the sight distance motor, the moment moving gear is in meshed connection with a moment moving toothed ring, the moment moving toothed ring is fixedly connected with a moment moving round box, auxiliary clamping plates are symmetrically arranged on one side of the moment moving round box, and the two auxiliary clamping plates are jointly connected with the camera module; the other side is fixedly connected with a matched rotating block, and the matched rotating block is connected with a matched rotating groove arranged in the inserting box; the outer side wall of the moment-driven round box is fixedly provided with a rotating toothed ring which is connected with the scraping and leveling component.
Preferably, the scraping and leveling component comprises a plurality of rotating gears meshed with the rotating toothed ring, rotating shafts are arranged on the rotating gears, the rotating shafts penetrate through a cleaning transverse plate arranged on the unmanned aerial vehicle body and are connected with driving pulleys, the driving pulleys are connected with driven pulleys through a transmission belt, driven shafts are arranged on the driven pulleys, the driven shafts penetrate through the cleaning transverse plate and are connected with driven bevel gears, the driven bevel gears are meshed with and connected with driving bevel gears, driving shafts are arranged on the driving bevel gears, and the driving shafts penetrate through driving base transmission arranged on the cam unmanned aerial vehicle body and are connected with the driving base.
Preferably, the cam is matched and connected with a touch abnormal plate, the touch abnormal plate is fixedly connected with the touch square plate, touch rods are symmetrically arranged on the touch square plate, one end of each touch rod is fixedly connected with the touch circular plate, and the other end of each touch rod is fixedly connected with the double-acting square plate; the touch rod is sleeved with a touch spring, one end of the touch spring is fixedly connected with the touch circular plate, the other end of the touch spring is fixedly connected with the touch square plate, and the touch square plate is provided with a brush plate.
Compared with the prior art, the invention has the beneficial effects that:
(1) When the annular moving square plate moves downwards, the annular moving long block enters the annular moving sleeve, the main magnetic sheet is in contact with the auxiliary magnetic sheet, the sight distance motor is electrified, an operator controls the sight distance motor through the controller, the output end of the sight distance motor drives the moment moving gear to rotate, then the moment moving gear ring is meshed to rotate, the moment moving round box is limited and rotated in the matching rotating groove through the matching rotating block, therefore, the angle required to be shot by the shooting module can be adjusted in real time, the shooting angle is prevented from being adjusted through the rotation of the unmanned aerial vehicle body, the limitation of the device in use is reduced, and meanwhile, the mapping efficiency is improved;
(2) When the annular moving square plate descends, the annular moving racks are driven to move, the annular moving racks are meshed with the annular moving gear to rotate, the annular moving threaded shaft is enabled to rotate, the double-acting square plate is enabled to move in the direction of the inserting box and the isolating square box through limiting blocks in a limiting mode, the double-acting springs on the double-acting rod are enabled to be in a buffer state, then a rubber layer on the double-acting square plate is enabled to clamp and connect the inserting box and the isolating square box, friction force connected between the inserting box and the isolating square box is improved, errors in mapping caused by shaking of the isolating square box are avoided, and accuracy of mapping is improved;
(3) When the moment-driven round box rotates, the moment-driven round box drives the rotating toothed ring to rotate and enables the moment-driven round box to engage with a plurality of rotating gears to rotate, the rotating gears rotate at a higher speed due to different sizes and transmission ratios of the moment-driven round box and the rotating shaft drives the driven pulleys to rotate, so that the driven bevel gears engage with the driving bevel gears to rotate, and then the cams on the driving rotating shaft rotate; the movable square plates on the double-sewing-connection assembly move to the side surfaces of the inserting box and the separating square box and are contacted with each other, so that the plurality of brush plates are driven to move to the periphery of the inserting box and the separating square box, when the movable square plates are contacted with the touch abnormal plates through rotation of the cam, the touch square plates are enabled to move on the touch rod in a limiting mode, the touch springs are enabled to be in a buffer state, when the cam is not contacted with the touch abnormal plates any more, the touch square plates are enabled to reset and move through reset of the touch springs, when the shooting angle of the shooting module is adjusted, the brush plates are enabled to repeatedly scrape the outer side surfaces of the separating square boxes, sundries such as dust adhered to the separating square boxes during flying are prevented from affecting mapping of the shooting module, and the accuracy and the working efficiency of mapping are improved;
(4) The operator aligns the brake plugboard on the square isolation box to the brake slot on the square isolation box, the square isolation box is pressed downwards, the inner plate on the square isolation box contacts the first rubber block and the second rubber block, the square clamping plate on the second rubber block is enabled to move in a limiting mode on the square isolation box through the limiting rod, the clamping spring is in a buffering state, the movable circular plate is enabled to move in a limiting sliding groove in a limiting mode through the limiting sliding block, the limiting spring on the limiting rod is in a buffering state, when the second rubber block on the square clamping plate contacts a groove formed in the inner plate on the square isolation box, the limiting spring and the clamping spring are reset, the provided elastic force drives the square clamping plate to move in a resetting mode and enter the groove, so that the square isolation box is fixed at the current position, meanwhile, the square isolation box is enabled to move in a limiting mode through the limiting rod and the first rubber block, shaking generated during flying is avoided, the situation that the square isolation box is out of position is caused, the square isolation box is enabled to move in a limiting mode, the situation that the two-sided imaging module is installed, the situation that the two-sided imaging camera is not is well is guaranteed, and the imaging quality of a user is well is prevented from being met when the two-sided imaging module is well, and the imaging quality is well-being well-ensured when the imaging camera is being well-up;
(5) When the descending and slow moving mechanism falls down, the movable contact piece arranged on the extension plate contacts with the static contact piece arranged on the abnormal base, signals are sent to the controller, the controller sends an interrupt signal to the telescopic motor, the output end of the telescopic motor is reset and moves, then the locking square block is not connected with the locking square groove any more, the limit setting of the limit sliding block is relieved, an operator can perform operations such as installation, disassembly and debugging on the isolation square box and the camera module, and when the unmanned aerial vehicle body takes off, the descending and slow moving mechanism is reset, the two contact pieces are not contacted any more, the controller sends a starting signal to the telescopic motor, the output end of the telescopic motor drives the locking square block to move into the locking square groove, the limit sliding block on the clamping and fastening unit is limited at the current position and is prevented from moving, the installation setting of the isolation square box is relieved due to uncertain factors in flight measurement, and safety of the unmanned aerial vehicle is improved;
(6) When the isolating square box is installed, the annular square plate is enabled to move in the locating groove in a limiting mode through downward pressing, a plurality of extrusion springs are in a buffer state, after the installation is completed, the isolating square box is not continuously applied with force, the extrusion springs which want to reset drive the grooves on the isolating square box to prop against the clamping square plate through the annular square plate and cannot move continuously, the isolating square box is clamped at the maximum limiting position through elasticity generated by the extrusion springs and cannot move, the imaging mapping of the imaging module is prevented from being influenced by annular movement of the isolating square box during flying, and the accuracy of mapping is improved while the stability of the isolating square box is improved;
(7) In order to avoid the conditions such as the strong vibration that causes when descending can lead to unmanned aerial vehicle body and the module of making a video recording of establishing to damage, at first move the circle piece and contact ground through descending when descending, absorb most impact force through the blotter, the stability of unmanned aerial vehicle body when descending has been promoted, make two descend the circle piece and move away from relatively through the linkage pivot, make the epaxial abnormal movement oblique piece of linkage pivot spacing removal in abnormal movement oblique pole, and make the abnormal movement spring be in the state of buffering, the impact force that makes its buffering power that provides offsets with the impact force that the unmanned aerial vehicle body brought when descending disappears, the stability of unmanned aerial vehicle body when descending has been promoted, thereby unmanned aerial vehicle body and the life of module of making a video recording have been promoted.
Drawings
The accompanying drawings are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate the invention and together with the embodiments of the invention, serve to explain the invention.
In the drawings:
FIG. 1 is a schematic diagram of the overall structure of the present invention;
FIG. 2 is a schematic view of the lifting and self-moving mechanism of the present invention;
FIG. 3 is a schematic view of the structure of the descent control device of the present invention;
FIG. 4 is a schematic diagram of a clamping and tightening unit according to the present invention;
FIG. 5 is a schematic view of a range adjustment mechanism according to the present invention;
FIG. 6 is a schematic view of the bottom structure of the present invention;
FIG. 7 is a schematic view of a dual-system sewing assembly according to the present invention;
FIG. 8 is a schematic view of the structure of the present invention at A in a partially enlarged manner;
FIG. 9 is a schematic view of a scraping and leveling assembly according to the present invention;
in the figure: 1. an unmanned aerial vehicle body; 2. a support arm; 3. lifting a cylinder; 4. lifting the rotating shaft; 5. a fan blade; 6. a lifting rotating groove; 7. lifting the rotating block; 8. a lifting motor; 9. lifting the clamping seat; 10. a plug-in box; 11. a linkage base; 12. a square box is isolated; 13. a first rubber block; 14. a second rubber block; 15. clamping a square plate; 16. clamping the rod; 17. a round blocking plate; 18. clamping a spring; 19. a handle; 20. a limit sliding block; 21. limiting sliding grooves; 22. a limit rod; 23. a limit spring; 24. a linkage rotating shaft; 25. a linkage square; 26. a linkage plate; 27. descending the round block; 28. a cushion pad; 29. a transaction oblique block; 30. a differential inclined rod; 31. a transaction base; 32. a spring for abnormal movement; 33. an extension plate; 34. a movable contact; 35. a stationary contact; 36. a brake insert plate; 37. a brake slot; 38. a circular square plate; 39. a positioning block; 40. a positioning groove; 41. extruding a spring; 42. a loop moving long block; 43. a sleeve is annularly moved; 44. a main magnetic sheet; 45. auxiliary magnetic sheets; 46. a circular rack; 47. a ring gear; 48. a ring-moving threaded shaft; 49. a double-acting plate; 50. double-acting square boards; 51. a stopper; 52. a stopper rod; 53. double-acting different plates; 54. a double-acting rod; 55. double-acting circular plates; 56. attaching a square plate; 57. a double-acting spring; 58. locking the square plate; 59. a telescopic motor; 60. locking the square; 61. locking the square groove; 62. a distance-moving clamping seat; 63. a stadia motor; 64. a moment gear; 65. a moment-driven toothed ring; 66. moment round box; 67. auxiliary clamping plates; 68. a camera module; 69. a rotating block is matched; 70. a rotating groove is matched; 71. rotating the toothed ring; 72. rotating the gear; 73. rotating the rotating shaft; 74. clearing the transverse plate; 75. a driving pulley; 76. a transmission belt; 77. a driven pulley; 78. a driven rotating shaft; 79. a driven bevel gear; 80. a drive bevel gear; 81. a driving rotating shaft; 82. a cam; 83. an active base; 84. touching the different plate; 85. touching the square plate; 86. a touch lever; 87. touching the circular plate; 88. a touch spring; 89. and brushing the plate.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and fully with reference to the accompanying drawings, in which it is evident that the embodiments described are only some, but not all embodiments of the invention; all other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
The embodiment is given by fig. 1 to 9, and the invention comprises an unmanned aerial vehicle body 1, wherein a plurality of support arms 2 are arranged on the unmanned aerial vehicle body 1, and the support arms 2 are connected with a lifting self-moving mechanism; the lifting self-moving mechanism comprises a lifting cylinder 3 arranged on a support arm 2, wherein a lifting rotating shaft 4 is arranged on the lifting cylinder 3, one end of the lifting rotating shaft 4 is fixedly connected with a plurality of fan blades 5, the other end of the lifting rotating shaft is provided with a lifting rotating groove 6, the lifting rotating groove 6 is connected with a lifting rotating block 7, the lifting rotating block 7 is connected with the output end of a lifting motor 8, lifting clamping seats 9 are symmetrically arranged on the lifting motor 8, and the two lifting clamping seats 9 are jointly connected with the lifting cylinder 3; the unmanned aerial vehicle body 1 is fixedly provided with a plug-in box 10 and a linkage base 11, and the linkage base 11 is connected with a descending motion slow-moving mechanism; the inserting box 10 and the isolating square box 12 are connected through a clamping and fastening unit;
through starting rising motor 8, the rising that its output was ascending rotates piece 7 and drives rising pivot 4 and rotate, then rotates through two flabellum 5, makes unmanned aerial vehicle body 1 take off through lift and thrust that a plurality of flabellum 5 rotated and produce, and a plurality of rising motor 8 are controlled by the controller and are controlled motor pivoted speed, make it shoot the survey and drawing to the target area through camera module 68, promoted the work efficiency of survey and drawing.
The clamping and fastening unit of the embodiment comprises a first rubber block 13 and a second rubber block 14 which are connected with the square isolation box 12 in a matched manner; the movable square box 12 is connected with the double-system sewing and linking assembly in a matched manner; the first rubber blocks 13 are fixedly connected with the partition plates arranged in the inserting box 10, the second rubber blocks 14 are fixedly connected with the clamping square plates 15, clamping rods 16 are symmetrically arranged on the clamping square plates 15, and the two clamping rods 16 penetrate through the inserting box 10 and are fixedly connected with the blocking circular plate 17 together; the clamping rod 16 is sleeved with a clamping spring 18, one end of the clamping spring 18 is fixedly connected with the inserting box 10, and the other end of the clamping spring is fixedly connected with the blocking circular plate 17; a lifting handle 19 is fixedly arranged on the blocking circular plate 17; the stop circular plate 17 is provided with a limit sliding block 20, and the limit sliding block 20 is in sliding connection with a limit sliding groove 21 arranged on the unmanned aerial vehicle body 1; a limiting rod 22 is fixedly arranged on the limiting chute 21, a limiting spring 23 is sleeved on the limiting rod 22, one end of the limiting spring 23 is fixedly connected with the limiting chute 21, and the other end of the limiting spring is fixedly connected with the limiting slide block 20;
the operator aligns the brake insert plate 36 on the blocking square box 12 with the brake insert slot 37 on the inserting box 10, the inner plate on the blocking square box 12 contacts the first rubber block 13 and the second rubber block 14 by pressing the blocking square box 12 downwards, the clamping square plate 15 on the second rubber block 14 moves on the inserting box 10 in a limiting way through the clamping rod 16, the clamping spring 18 is in a buffering state, the blocking circular plate 17 moves in a limiting way in the limiting slide groove 21 through the limiting slide block 20, the limiting spring 23 on the limiting rod 22 is in a buffering state, when the second rubber block 14 on the clamping square plate 15 contacts the groove arranged at the inner plate on the blocking square box 12, the limiting spring 23 and the clamping spring 18 are reset, the elasticity that provides drives and presss from both sides the square board 15 and reset and remove and get into in the recess to will separate and move square box 12 fixed in current position, simultaneously contact and separate and move square box 12 through second rubber piece 14 and first rubber piece 13 simultaneously, increased the resistance that separates and move square box 12 and removed, avoid shaking produced when the flight and lead to separating and move square box 12 dislocation, thereby accomplished the installation operation that separates and move square box 12, separate and move square box 12 and be two-sided transparent material, thereby provide the safety guarantee to camera module 68, avoid making it strike the barrier and cause the damage when the flight, avoided can meet various bad weather etc. and lead to camera module 68 camera lens to blur when the flight, the efficiency of shooing when the survey has been promoted, the precision of survey has been promoted simultaneously.
The descending and slow moving mechanism of the embodiment comprises a linkage rotating shaft 24 arranged on a linkage base 11, a linkage square block 25 is arranged on the linkage rotating shaft 24, a linkage plate 26 is arranged on the linkage square block 25, a descending round block 27 is fixedly arranged on the linkage plate 26, and a cushion pad 28 is arranged on the descending round block 27; two ends of the linkage rotating shaft 24 penetrate through the linkage base 11 and are fixedly connected with the abnormal inclined block 29, and the abnormal inclined block 29 is connected with the abnormal inclined rod 30; the two ends of the abnormal inclined rod 30 are fixedly connected with abnormal bases 31 fixedly arranged on the unmanned aerial vehicle body 1; the abnormal inclined rod 30 is sleeved with an abnormal spring 32, one end of the abnormal spring 32 is fixedly connected with the abnormal base 31, the other end of the abnormal spring is fixedly connected with the abnormal inclined block 29, the abnormal inclined block 29 is provided with an extension plate 33, the extension plate 33 is provided with a movable contact piece 34, the movable contact piece 34 is connected with a static contact piece 35 arranged on the abnormal base 31 in a matched manner, and the contact of the movable contact piece 34 and the static contact piece 35 is connected with a fixed locking control assembly;
in order to avoid the conditions that the unmanned aerial vehicle body 1 and the built-in camera module 68 are damaged due to strong vibration caused during landing, the ground is contacted by the descending circular blocks 27 during landing, most of impact force is absorbed by the cushion pad 28, the stability of the unmanned aerial vehicle body 1 during landing is improved, the two descending circular blocks 27 relatively move away from each other through the linkage rotating shaft 24, the abnormal inclined blocks 29 on the linkage rotating shaft 24 move in the abnormal inclined rods 30 in a limiting mode, the abnormal springs 32 are in a buffer mode, the buffer force provided by the abnormal springs is offset with the impact force brought by the unmanned aerial vehicle body 1 during landing, and the stability of the unmanned aerial vehicle body 1 during landing is improved, so that the service lives of the unmanned aerial vehicle body 1 and the camera module 68 are prolonged.
The double-sewing-connection assembly of the embodiment comprises a brake inserting plate 36 arranged on the outer plate of the square isolation box 12, wherein the brake inserting plate 36 is connected with a brake inserting groove 37 arranged on the square isolation box 10; the isolating square box 12 is connected with the annular square plate 38 in a matched manner, a plurality of positioning blocks 39 are arranged on the annular square plate 38, and the positioning blocks 39 are connected with positioning grooves 40 arranged on the inserting box 10 in a sliding manner; the inner bottom surface of the inserting box 10 is fixedly connected with the annular moving square plate 38 through an extrusion spring 41, a plurality of annular moving long blocks 42 are arranged on the annular moving square plate 38, the annular moving long blocks 42 are connected with an annular moving sleeve 43 arranged in the inserting box 10 in a matched mode, a main magnetic sheet 44 is arranged in one annular moving sleeve 43, the main magnetic sheet 44 is connected with an auxiliary magnetic sheet 45 arranged on the annular moving long blocks 42 in a matched mode, and contact between the main magnetic sheet 44 and the auxiliary magnetic sheet 45 is connected with a vision distance adjusting mechanism; a plurality of annular racks 46 are arranged on the annular square plate 38, the annular racks 46 are meshed with an annular gear 47, an annular threaded shaft 48 is arranged on the annular gear 47, one end of the annular threaded shaft 48 is connected with a double-acting plate 49, and the other end of the annular threaded shaft is in transmission connection with the inserting box 10; the double-acting square plate 50 is arranged on the annular moving threaded shaft 48 in a threaded manner, the double-acting square plate 50 is provided with a limiting block 51, and the limiting block 51 is in sliding connection with a limiting rod 52 fixedly arranged on the inserting box 10; the double-acting square plate 50 is fixedly provided with a double-acting different plate 53, the double-acting different plate 53 is provided with a double-acting rod 54, one end of the double-acting rod 54 is fixedly connected with a double-acting circular plate 55, and the other end of the double-acting rod 54 is fixedly connected with a movable square plate 56; the double-acting rod 54 is sleeved with a double-acting spring 57, one end of the double-acting spring 57 is fixedly connected with the movable square plate 56, and the other end of the double-acting spring 57 is fixedly connected with the double-acting differential plate 53;
when the blocking square box 12 is installed, the annular square plate 38 is limited to move in the positioning groove 40 through the positioning block 39 by pressing downwards, so that the plurality of extrusion springs 41 are in a buffer state, after the installation is finished, the extrusion springs 41 which want to reset drive the grooves on the blocking square box 12 to prop against the clamping square plate 15 through the annular square plate 38 and cannot move, the blocking square box 12 is clamped at the maximum limiting position by the elasticity generated by the extrusion springs 41 and cannot move, the imaging and mapping of the imaging module 68 are prevented from being influenced by the annular movement of the blocking square box 12 during the flying, the stability of the blocking square box 12 is improved, and the accuracy of mapping is improved; when the annular moving square plate 38 descends, the annular moving racks 46 are driven to move, the annular moving racks are meshed with the annular moving gear 47 to rotate, the annular moving threaded shaft 48 is driven to rotate, the double-acting square plate 50 is limited to move on the limiting rod 52 through the limiting block 51, the movable pasting square plate 56 moves towards the direction of the inserting box 10 and the movable isolating square box 12, the double-acting springs 57 on the double-acting rod 54 are in a buffer state, the rubber layer on the movable pasting square plate 56 is then used for clamping and connecting the inserting box 10 and the movable isolating square box 12, the friction force connected between the inserting box 10 and the movable isolating square box 12 is improved, mapping errors caused by shaking of the movable isolating square box 12 are avoided, and mapping accuracy is improved.
The fixed lock control assembly of the embodiment comprises a locking square plate 58 symmetrically arranged on a limit sliding block 20, a telescopic motor 59 is fixedly arranged on the locking square plate 58, a locking square block 60 is arranged on the output end of the telescopic motor 59, and the locking square block 60 is connected with a locking square groove 61 arranged on the unmanned aerial vehicle body 1 in a matched manner;
when the descent motion slowing mechanism is fallen down, the movable contact piece 34 arranged on the extension plate 33 contacts the static contact piece 35 arranged on the abnormal motion base 31, a signal is sent to the controller, the controller sends an interrupt signal to the telescopic motor 59, the output end of the telescopic motor 59 is reset and moved, then the locking square block 60 is not connected with the locking square groove 61 any more, the limit setting of the limit sliding block 20 is relieved, an operator can perform operations such as installation, disassembly and debugging on the movable square box 12 and the camera shooting module 68, after the unmanned aerial vehicle body 1 takes off, the descent motion slowing mechanism is reset, then the two contact pieces are not contacted any more, the controller sends a starting signal to the telescopic motor 59, the output end of the controller drives the locking square block 60 to move and enter the locking square groove 61, the limit sliding block 20 on the clamping and fastening unit is limited at the current position and is prevented from moving, the installation setting of the movable square box 12 is relieved due to the fact that the clamping and the uncertain factors and the like are avoided in the drawing of the flight measurement, and the safety of the device is improved when the unmanned aerial vehicle body is used.
The sight distance adjusting mechanism of the embodiment comprises a distance moving clamping seat 62 arranged on the inserting moving box 10, a sight distance motor 63 is fixedly arranged on the distance moving clamping seat 62, a moment moving gear 64 is arranged at the output end of the sight distance motor 63, the moment moving gear 64 is meshed with a moment moving toothed ring 65, the moment moving toothed ring 65 is fixedly connected with a moment moving round box 66, auxiliary clamping plates 67 are symmetrically arranged on one side of the moment moving round box 66, and the two auxiliary clamping plates 67 are jointly connected with a camera module 68; the other side is fixedly connected with a matching rotating block 69, and the matching rotating block 69 is connected with a matching rotating groove 70 arranged in the inserting box 10; a rotating toothed ring 71 is fixedly arranged on the outer side wall of the rectangular movable round box 66, and the rotating toothed ring 71 is connected with the scraping and leveling component;
when the annular moving square plate 38 moves downwards, the annular moving long block 42 enters the annular moving sleeve 43, the main magnetic sheet 44 is in contact with the auxiliary magnetic sheet 45, the sight motor 63 is electrified, an operator controls the sight motor 63 through the controller, the output end of the sight motor drives the moment moving gear 64 to rotate, then the moment moving toothed ring 65 is meshed to rotate, the moment moving round box 66 is limited to rotate in the matching rotating groove 70 through the matching rotating block 69, therefore, the angle required to be shot by the shooting module 68 can be adjusted in real time, the shooting angle is prevented from being adjusted through the rotation of the unmanned aerial vehicle body 1, the limitation of the device in use is reduced, and meanwhile, the mapping efficiency is improved.
The scraping and cleaning assembly of the embodiment comprises a plurality of rotating gears 72 in meshed connection with a rotating toothed ring 71, rotating shafts 73 are mounted on the rotating gears 72, the rotating shafts 73 penetrate through a cleaning transverse plate 74 arranged on an unmanned aerial vehicle body 1 and are connected with a driving pulley 75, the driving pulley 75 is connected with a driven pulley 77 through a driving belt 76, a driven rotating shaft 78 is mounted on the driven pulley 77, the driven rotating shaft 78 penetrates through the cleaning transverse plate 74 and is connected with a driven bevel gear 79, the driven bevel gear 79 is in meshed connection with a driving bevel gear 80, a driving rotating shaft 81 is mounted on the driving bevel gear 80, and the driving rotating shaft 81 penetrates through a driving base 83 arranged on the unmanned aerial vehicle body 1 and is in transmission connection with a cam 82; the cam 82 is matched and connected with a touch abnormal plate 84, the touch abnormal plate 84 is fixedly connected with a touch square plate 85, touch bars 86 are symmetrically arranged on the touch square plate 85, one end of each touch bar 86 is fixedly connected with a touch circular plate 87, and the other end of each touch bar 86 is fixedly connected with the double-acting square plate 50; a touch spring 88 is sleeved on the touch rod 86, one end of the touch spring 88 is fixedly connected with a touch circular plate 87, the other end of the touch spring is fixedly connected with a touch square plate 85, and a brush plate 89 is arranged on the touch square plate 85;
when the moment-driven round box 66 rotates, the moment-driven round box drives the rotating toothed ring 71 to rotate and enables the moment-driven round box to engage with a plurality of rotating gears 72 to rotate, the rotating gears 72 rotate at a higher speed due to different sizes and transmission ratios of the moment-driven round box and the rotating rotary shaft 73 drives the driven pulley 77 to rotate, so that the driven bevel gear 79 engages with the driving bevel gear 80 to rotate, and then the cam 82 on the driving rotary shaft 81 rotates; because the movable contact plate 56 on the double-sewing assembly moves to the side surfaces of the inserting box 10 and the isolating contact box 12 and contacts with each other, the plurality of brush plates 89 are driven to move to the periphery of the inserting box 10 and the isolating contact box 12, when the movable contact plate contacts with the touching abnormal plate 84 through the rotation of the cam 82, the touching contact plate 85 is limited to move on the touching rod 86, the touching spring 88 is in a buffer state, when the cam 82 does not contact with the touching abnormal plate 84 any more, the touching contact plate 85 is reset to move through the reset of the touching spring 88, when the shooting angle of the shooting module 68 is adjusted, the brush plates 89 are used for scraping the outer side surface of the isolating contact box 12 in a reciprocating manner, sundries such as dust adhered on the isolating contact box 12 during flying are prevented from affecting the mapping of the shooting module 68, and the mapping precision and the working efficiency of the mapping are improved.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (10)
1. But shooting angle autogiration's remote sensing survey unmanned aerial vehicle, its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein a plurality of support arms (2) are arranged on the unmanned aerial vehicle body (1), and the support arms (2) are connected with a lifting automatic moving mechanism;
the lifting automatic moving mechanism comprises a lifting cylinder (3) arranged on a support arm (2), wherein a lifting rotating shaft (4) is arranged on the lifting cylinder (3), one end of the lifting rotating shaft (4) is fixedly connected with a plurality of fan blades (5), a lifting rotating groove (6) is arranged at the other end of the lifting rotating shaft, the lifting rotating groove (6) is connected with a lifting rotating block (7), the lifting rotating block (7) is connected with the output end of a lifting motor (8), lifting clamping seats (9) are symmetrically arranged on the lifting motor (8), and the two lifting clamping seats (9) are jointly connected with the lifting cylinder (3); the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein an inserting box (10) and a linkage base (11) are fixedly arranged on the unmanned aerial vehicle body (1), and the linkage base (11) is connected with a descending motion slow-moving mechanism; the inserting box (10) is connected with the isolating square box (12) through a clamping and fastening unit.
2. The remotely sensed surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle according to claim 1, wherein: the clamping and fastening unit comprises a first rubber block (13) and a second rubber block (14) which are connected with the square isolation box (12) in a matched manner; the movable square box (12) is connected with the double-system sewing-connecting assembly in a matched manner; the two clamping rods (16) penetrate through the plug-in box (10) and are fixedly connected with the baffle plate (17) together.
3. The remotely sensed surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle according to claim 2, wherein: the clamping rod (16) is sleeved with a clamping spring (18), one end of the clamping spring (18) is fixedly connected with the inserting box (10), and the other end of the clamping spring is fixedly connected with the blocking circular plate (17); a lifting handle (19) is fixedly arranged on the blocking circular plate (17); a limit sliding block (20) is arranged on the blocking circular plate (17), and the limit sliding block (20) is arranged in a sliding connection with a limit sliding groove (21) arranged on the unmanned aerial vehicle body (1); a limiting rod (22) is fixedly arranged on the limiting chute (21), a limiting spring (23) is sleeved on the limiting rod (22), one end of the limiting spring (23) is fixedly connected with the limiting chute (21), and the other end of the limiting spring is fixedly connected with the limiting slide block (20).
4. The remotely sensed surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle according to claim 1, wherein: the descending and slow moving mechanism comprises a linkage rotating shaft (24) arranged on a linkage base (11), a linkage square block (25) is arranged on the linkage rotating shaft (24), a linkage plate (26) is arranged on the linkage square block (25), a descending round block (27) is fixedly arranged on the linkage plate (26), and a cushion pad (28) is arranged on the descending round block (27); the two ends of the linkage rotating shaft (24) penetrate through the linkage base (11) and are fixedly connected with the abnormal inclined block (29), and the abnormal inclined block (29) is connected with the abnormal inclined rod (30); the two ends of the abnormal inclined rod (30) are fixedly connected with abnormal bases (31) fixedly arranged on the unmanned aerial vehicle body (1); the utility model discloses a fixed lock is controlled in the setting that moves on the slope of change (30), cover is equipped with change spring (32) on change slope (30), and the one end and the change base (31) fixed connection of change spring (32) set up, and the other end and change slope piece (29) fixed connection set up, installs extension board (33) on the change slope piece (29), is equipped with movable contact piece (34) on extension board (33), and movable contact piece (34) are connected with static contact piece (35) cooperation that are equipped with on the change base (31) and are set up, and the contact and the fixed lock of both are locked the subassembly and are connected and set up.
5. The remotely sensed surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle according to claim 2, wherein: the double-system sewing assembly comprises a brake inserting plate (36) arranged on the outer plate of the square isolation box (12), and the brake inserting plate (36) is connected with a brake slot (37) arranged on the square isolation box (10); the movable square box (12) is connected with the annular movable square plate (38) in a matched mode, a plurality of positioning blocks (39) are arranged on the annular movable square plate (38), and the positioning blocks (39) are connected with positioning grooves (40) arranged on the movable box (10) in a sliding mode; the inner bottom surface of the inserting box (10) is fixedly connected with the annular moving square plate (38) through an extrusion spring (41), a plurality of annular moving long blocks (42) are installed on the annular moving square plate (38), the annular moving long blocks (42) are connected with an annular moving sleeve (43) arranged in the inserting box (10) in a matched mode, one main magnetic sheet (44) is installed in the annular moving sleeve (43), the main magnetic sheet (44) is connected with an auxiliary magnetic sheet (45) arranged on the annular moving long blocks (42) in a matched mode, and the main magnetic sheet (44) is connected with an eye distance adjusting mechanism in a contact mode.
6. The remotely sensed surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle according to claim 5, wherein: a plurality of annular moving racks (46) are arranged on the annular moving square plate (38), the annular moving racks (46) are meshed with an annular moving gear (47), an annular moving threaded shaft (48) is arranged on the annular moving gear (47), one end of the annular moving threaded shaft (48) is connected with a double-acting plate (49), and the other end of the annular moving threaded shaft is in transmission connection with the inserting box (10); the double-acting square plate (50) is arranged on the annular moving threaded shaft (48) in a threaded manner, the double-acting square plate (50) is provided with a limiting block (51), and the limiting block (51) is in sliding connection with a limiting rod (52) fixedly arranged on the inserting box (10); a double-acting different plate (53) is fixedly arranged on the double-acting square plate (50), a double-acting rod (54) is arranged on the double-acting different plate (53), one end of the double-acting rod (54) is fixedly connected with a double-acting circular plate (55), and the other end of the double-acting rod is fixedly connected with a movable square plate (56); the double-acting rod (54) is sleeved with a double-acting spring (57), one end of the double-acting spring (57) is fixedly connected with the movable square plate (56), and the other end of the double-acting spring is fixedly connected with the double-acting different plate (53).
7. The remotely sensed surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle according to claim 4, wherein: the fixed lock locking and controlling assembly comprises locking square plates (58) symmetrically arranged on the limiting sliding blocks (20), a telescopic motor (59) is fixedly arranged on the locking square plates (58), a locking square block (60) is arranged at the output end of the telescopic motor (59), and the locking square block (60) is connected with a locking square groove (61) arranged on the unmanned aerial vehicle body (1) in a matched mode.
8. The remotely sensed surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle according to claim 5, wherein: the visual range adjusting mechanism comprises a range motion clamping seat (62) arranged on the inserting and moving box (10), a visual range motor (63) is fixedly arranged on the range motion clamping seat (62), a range motion gear (64) is arranged at the output end of the visual range motor (63), the range motion gear (64) is meshed with a range motion toothed ring (65), the range motion toothed ring (65) is fixedly connected with a range motion round box (66), auxiliary clamping plates (67) are symmetrically arranged on one side of the range motion round box (66), and the two auxiliary clamping plates (67) are jointly connected with a camera module (68); the other side is fixedly connected with a matching rotating block (69), and the matching rotating block (69) is connected with a matching rotating groove (70) arranged in the inserting box (10); the outer side wall of the moment-driven round box (66) is fixedly provided with a rotating toothed ring (71), and the rotating toothed ring (71) is connected with the scraping and leveling component.
9. The remotely sensed surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle according to claim 8, wherein: the scraping and leveling assembly comprises a plurality of rotating gears (72) which are meshed with a rotating toothed ring (71), rotating shafts (73) are arranged on the rotating gears (72), the rotating shafts (73) penetrate through a cleaning transverse plate (74) arranged on the unmanned aerial vehicle body (1) to be connected with a driving pulley (75), the driving pulley (75) is connected with a driven pulley (77) through a driving belt (76), a driven rotating shaft (78) is arranged on the driven pulley (77), the driven rotating shaft (78) penetrates through the cleaning transverse plate (74) to be connected with a driven bevel gear (79), the driven bevel gear (79) is meshed with a driving bevel gear (80), a driving rotating shaft (81) is arranged on the driving bevel gear (80), and the driving rotating shaft (81) penetrates through a driving base (83) arranged on the cam (82) unmanned aerial vehicle body (1) to be connected in a driving mode.
10. The remotely sensed surveying and mapping unmanned aerial vehicle capable of automatically rotating a shooting angle according to claim 9, wherein: the cam (82) is matched and connected with the touch abnormal plate (84), the touch abnormal plate (84) is fixedly connected with the touch square plate (85), the touch square plate (85) is symmetrically provided with touch rods (86), one end of each touch rod (86) is fixedly connected with the touch circular plate (87), and the other end of each touch rod is fixedly connected with the double-acting square plate (50); the touch rod (86) is sleeved with a touch spring (88), one end of the touch spring (88) is fixedly connected with a touch circular plate (87), the other end of the touch spring is fixedly connected with a touch square plate (85), and a brush plate (89) is arranged on the touch square plate (85).
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202311152752.5A CN117087888A (en) | 2023-09-07 | 2023-09-07 | But shooting angle autogiration's remote sensing survey and drawing unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202311152752.5A CN117087888A (en) | 2023-09-07 | 2023-09-07 | But shooting angle autogiration's remote sensing survey and drawing unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN117963195A (en) * | 2024-03-28 | 2024-05-03 | 建潘鲲鹭物联网技术研究院(厦门)有限公司 | Intelligent power transmission network inspection device and method based on unmanned aerial vehicle |
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2023
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117963195A (en) * | 2024-03-28 | 2024-05-03 | 建潘鲲鹭物联网技术研究院(厦门)有限公司 | Intelligent power transmission network inspection device and method based on unmanned aerial vehicle |
| CN117963195B (en) * | 2024-03-28 | 2024-06-14 | 建潘鲲鹭物联网技术研究院(厦门)有限公司 | Intelligent power transmission network inspection device and method based on unmanned aerial vehicle |
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