CN217918412U - A aircraft for geographical mapping for plateau area - Google Patents
A aircraft for geographical mapping for plateau area Download PDFInfo
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- CN217918412U CN217918412U CN202221216727.XU CN202221216727U CN217918412U CN 217918412 U CN217918412 U CN 217918412U CN 202221216727 U CN202221216727 U CN 202221216727U CN 217918412 U CN217918412 U CN 217918412U
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- fixedly connected
- mapping
- camera
- subassembly
- aircraft
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- 238000013507 mapping Methods 0.000 title claims abstract description 46
- 230000003139 buffering effect Effects 0.000 claims abstract description 5
- 238000004140 cleaning Methods 0.000 claims description 17
- 238000013016 damping Methods 0.000 claims description 8
- 238000007789 sealing Methods 0.000 claims description 7
- 230000000694 effects Effects 0.000 abstract description 9
- 230000008602 contraction Effects 0.000 description 9
- 230000001174 ascending effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000002633 protecting effect Effects 0.000 description 1
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Abstract
The utility model discloses an aircraft is used in geographical mapping in plateau area belongs to the unmanned aerial vehicle field, an aircraft is used in geographical mapping in plateau area, including the unmanned aerial vehicle body, the bottom fixedly connected with connecting plate of unmanned aerial vehicle body, the bottom fixedly connected with casing of connecting plate, the inside of casing is provided with shrink subassembly, shrink subassembly's shrink end is provided with the mapping camera, be provided with the clearance subassembly that is used for clearing up the mapping camera on the shrink subassembly, the both sides of connecting plate bottom all are provided with the buffering subassembly, through shrink subassembly's setting, can drive the mapping camera and carry out concertina movement, have guaranteed that the mapping camera is not carrying out the mapping during operation, can carry out the shrink protection to the mapping camera, and through clearing up subassembly's setting, be convenient for clear up the camera end of mapping camera, avoid unmanned aerial vehicle when the high altitude, fog appears in its camera terminal surface, influence the problem of plotting effect.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field, more specifically say, relate to an aircraft for geographical mapping for plateau area.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a wireless remote control device and a self-contained program control device; the personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The landing aircraft can automatically land in the same way as the landing process of a common aircraft, can also be recovered by a remote control parachute or a barrier net, and is widely used for aerial reconnaissance, monitoring, communication, anti-diving, electronic interference and the like.
Through patent search, the application number: CN202220100230.5 drives the second rotation axis through step motor and rotates, and the second rotation axis then can drive and survey the camera and rotate to reach and shoot to all directions, however at actual operation's in-process, unmanned aerial vehicle soars in the high altitude, often can be infected with by the moisture in the atmosphere, and then causes the blur of camera sight, thereby influences the mapping effect.
SUMMERY OF THE UTILITY MODEL
1. Technical problem to be solved
Problem to exist among the prior art, the utility model aims to provide an aircraft is used in geographical mapping in plateau area can drive the mapping camera and carry out concertina movement, has guaranteed that the mapping camera is not carrying out the survey and drawing during operation, can contract the protection to the mapping camera, and through the setting of clearance subassembly, be convenient for clear up the camera end of mapping camera moreover, avoid unmanned aerial vehicle when the high altitude, fog appears in its camera terminal surface, influences the problem of plotting effect.
2. Technical scheme
In order to solve the problem, the utility model adopts the following technical proposal.
An aircraft for geographical surveying and mapping in plateau areas comprises an unmanned aerial vehicle body, wherein a connecting plate is fixedly connected to the bottom of the unmanned aerial vehicle body, a shell is fixedly connected to the bottom of the connecting plate, a contraction assembly is arranged inside the shell, a surveying and mapping camera is arranged at the contraction end of the contraction assembly, a cleaning assembly for cleaning the surveying and mapping camera is arranged on the contraction assembly, and buffering assemblies are arranged on two sides of the bottom of the connecting plate;
through shrink component's setting, can drive the survey and drawing camera and carry out concertina movement, guaranteed the survey and drawing camera and when not carrying out the survey and drawing work, can contract the survey and drawing camera, protect through the casing.
Furthermore, the shrink component is including seting up in the opening of casing bottom to and sliding connection in lifter plate between the shells inner wall both sides, the bottom fixedly connected with mounting bracket of lifter plate, survey and drawing camera is fixed in the inside of mounting bracket.
Furthermore, the bottom fixedly connected with closing plate of mounting bracket, the locating hole has all been seted up to four corners of closing plate, and four locating levers of bottom fixedly connected with of casing, the top fixedly connected with sealing washer of closing plate, shells inner wall's top fixedly connected with motor, the output shaft fixedly connected with lead screw of motor, the surface of lead screw and the inside threaded connection of lifter plate.
Further, the clearance subassembly include sliding connection in the inside carriage of lifter plate, the bottom fixedly connected with cleaning pad of carriage, and cleaning pad and surveying and mapping camera's end face contact, and support fixedly connected with electric telescopic handle is passed through to one side at the top of lifter plate, electric telescopic handle's flexible end and carriage fixed connection.
Further, the buffering subassembly is including being fixed in the U type frame of connecting plate bottom, sliding connection has the frame that falls to the ground between the front of U type frame and the back, the top fixedly connected with T type pole that falls to the ground frame, the surface cover of T type pole is equipped with the damping cover, the damping cover is fixed in the inside of U type frame.
Furthermore, the top of the T-shaped rod is fixedly connected with a buffer spring, and the top end of the buffer spring is fixed at the top of the inner wall of the U-shaped frame.
3. Advantageous effects
Compared with the prior art, the utility model has the advantages of:
this technical scheme passes through the setting of survey and drawing camera, be convenient for survey and draw the geographical environment in plateau area, and setting through shrink component, can drive survey and drawing camera and carry out concertina movement, survey and drawing camera is not carrying out the survey and drawing during operation having guaranteed, can contract survey and drawing camera, protect through the casing, improve survey and drawing camera's protecting effect, the service life of the air conditioner is prolonged, and setting through the clearance subassembly, be convenient for clear up survey and drawing camera's camera end, avoid unmanned aerial vehicle when the high altitude, fog appears in its camera terminal surface, influence survey and drawing effect's problem.
Drawings
Fig. 1 is a front view structural schematic diagram of the present invention;
fig. 2 is a schematic structural view of the housing of the present invention;
fig. 3 is a structural sectional view of the housing of the present invention;
fig. 4 is a schematic structural view of the middle buffering assembly of the present invention.
The reference numbers in the figures illustrate:
1. an unmanned aerial vehicle body; 2. a connecting plate; 3. a housing; 4. a retraction assembly; 41. a lifting plate; 42. a mounting frame; 43. a sealing plate; 44. positioning holes; 45. positioning a rod; 46. a motor; 47. a screw rod; 5. surveying and mapping cameras; 6. cleaning the assembly; 61. a carriage; 62. a cleaning pad; 63. an electric telescopic rod; 7. a buffer assembly; 71. a U-shaped frame; 72. a ground falling frame; 73. a T-shaped rod; 74. a damping sleeve; 75. a buffer spring.
Detailed Description
The technical solution in the embodiment of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiment of the present invention; obviously, the described embodiments are only a part of the embodiments of the present invention, and not all embodiments, and all other embodiments obtained by those skilled in the art without making creative efforts based on the embodiments of the present invention belong to the protection scope of the present invention.
Example 1:
referring to fig. 1-4, an aircraft for geographical mapping in plateau areas comprises an unmanned aerial vehicle body 1, wherein a connecting plate 2 is fixedly connected to the bottom of the unmanned aerial vehicle body 1, a shell 3 is fixedly connected to the bottom of the connecting plate 2, a contraction component 4 is arranged inside the shell 3, a mapping camera 5 is arranged at a contraction end of the contraction component 4, a cleaning component 6 for cleaning the mapping camera 5 is arranged on the contraction component 4, and buffer components 7 are arranged on two sides of the bottom of the connecting plate 2;
the arrangement of the surveying and mapping camera 5 is convenient for surveying and mapping the geographical environment of the plateau area, and the arrangement of the contraction component 4 can drive the surveying and mapping camera 5 to perform telescopic motion, so that the surveying and mapping camera 5 can be ensured to be contracted when the surveying and mapping work is not performed on the surveying and mapping camera 5;
the shell 3 is used for protection, so that the protection effect of the surveying and mapping camera 5 is improved, and the service life of the surveying and mapping camera is prolonged;
through the setting of clearance subassembly 6, be convenient for clear up the end of making a video recording of survey and drawing camera 5, avoid unmanned aerial vehicle when the high altitude, its terminal surface of making a video recording fog appears, influences the problem of plotting effect.
Referring to fig. 2-3, the retraction assembly 4 includes a through opening formed at the bottom of the housing 3, and a lifting plate 41 slidably connected between two sides of the inner wall of the housing 3, a mounting frame 42 is fixedly connected to the bottom of the lifting plate 41, and the surveying and mapping camera 5 is fixed inside the mounting frame 42;
through the motion about the lifter plate 41, can drive survey and drawing camera 5 up-and-down motion, through survey and drawing camera 5 ascending motion, can contract to the inside of casing 3, protect, through survey and drawing camera 5 decurrent motion, can carry out the survey and drawing work.
Referring to fig. 2-3, a sealing plate 43 is fixedly connected to the bottom of the mounting frame 42, positioning holes 44 are formed in four corners of the sealing plate 43, four positioning rods 45 are fixedly connected to the bottom of the housing 3, a sealing ring is fixedly connected to the top of the sealing plate 43, a motor 46 is fixedly connected to the top of the inner wall of the housing 3, a lead screw 47 is fixedly connected to an output shaft of the motor 46, and the outer surface of the lead screw 47 is in threaded connection with the inside of the lifting plate 41;
Referring to fig. 2-3, the cleaning assembly 6 includes a sliding frame 61 slidably connected inside the lifting plate 41, a cleaning pad 62 is fixedly connected to the bottom of the sliding frame 61, the cleaning pad 62 contacts with the end surface of the surveying and mapping camera 5, an electric telescopic rod 63 is fixedly connected to one side of the top of the lifting plate 41 through a support, and the telescopic end of the electric telescopic rod 63 is fixedly connected to the sliding frame 61;
electric telescopic handle 63 is connected with external power and control switch for drive carriage 61 side-to-side movement, through the motion about carriage 61, can drive cleaning pad 62 side-to-side movement, and then carry out cleaning to mapping camera 5, avoid high altitude fog, cause sheltering from of mapping camera 5 sight, improve the effect of survey and drawing.
Referring to fig. 4, the buffer assembly 7 includes a U-shaped frame 71 fixed at the bottom of the connecting plate 2, a ground falling frame 72 is slidably connected between the front and the back of the U-shaped frame 71, a T-shaped rod 73 is fixedly connected to the top of the ground falling frame 72, a damping sleeve 74 is sleeved on the outer surface of the T-shaped rod 73, and the damping sleeve 74 is fixed inside the U-shaped frame 71;
the impact force is transmitted to the T-shaped rod 73 by the contact of the floor frame 72 with the ground, so that the T-shaped rod moves upward, is buffered by the buffer spring 75, and is convenient for reducing the vibration amplitude by the arrangement of the damping sleeve 74.
Referring to fig. 4, a buffer spring 75 is fixedly connected to the top of the T-shaped rod 73, and the top end of the buffer spring 75 is fixed to the top of the inner wall of the U-shaped frame 71;
the impact of the upward movement of the T-bar 73 is cushioned and offset by the elastic force of the cushion spring 75 itself, thereby providing a cushion effect.
When in use: through motor 46's start-up, can drive lead screw 47 and rotate, rotation through lead screw 47, can drive lifter plate 41 up-and-down motion, motion about through lifter plate 41, can drive survey and drawing camera 5 up-and-down motion through mounting bracket 42, through the decurrent motion of survey and drawing camera 5, can carry out the plotting work, and start through electric telescopic handle 63, can drive carriage 61 side-to-side motion, motion about through carriage 61, can drive cleaning pad 62 side-to-side motion, and then carry out cleaning to survey and drawing camera 5, avoid high altitude fog, cause the sheltering from of survey and drawing camera 5 sight, through the ascending motion of survey and drawing camera 5, can contract to the inside of casing 3, protect, setting through closing plate 43, be convenient for carry out the shutoff to the opening of casing 3 bottom, improve the comprehensive nature of protection.
The foregoing is only a preferred embodiment of the present invention; the scope of the present invention is not limited thereto. Any person skilled in the art should also be able to cover the protection scope of the present invention by replacing or changing the technical solution and the modified concept of the present invention within the technical scope of the present invention.
Claims (6)
1. The utility model provides an aircraft is used in geographical survey and drawing for plateau area, includes unmanned aerial vehicle body (1), its characterized in that: the utility model discloses an unmanned aerial vehicle body, including unmanned aerial vehicle body (1), bottom fixedly connected with connecting plate (2), the bottom fixedly connected with casing (3) of connecting plate (2), the inside of casing (3) is provided with shrink subassembly (4), the shrink end of shrink subassembly (4) is provided with mapping camera (5), be provided with on shrink subassembly (4) and be used for clearance subassembly (6) to mapping camera (5) clearance, the both sides of connecting plate (2) bottom all are provided with buffering subassembly (7).
2. An aircraft for geographical mapping in plateau areas according to claim 1, characterized in that: shrink subassembly (4) including seting up in the opening of casing (3) bottom, and sliding connection in lifter plate (41) between casing (3) inner wall both sides, the bottom fixedly connected with mounting bracket (42) of lifter plate (41), mapping camera (5) are fixed in the inside of mounting bracket (42).
3. An aircraft for geographical mapping in plateau areas according to claim 2, characterized in that: the bottom fixedly connected with closing plate (43) of mounting bracket (42), locating hole (44) have all been seted up to four corners of closing plate (43), and four locating levers (45) of bottom fixedly connected with of casing (3), the top fixedly connected with sealing washer of closing plate (43), top fixedly connected with motor (46) of casing (3) inner wall, the output shaft fixedly connected with lead screw (47) of motor (46), the surface of lead screw (47) and the inside threaded connection of lifter plate (41).
4. The aircraft for geographical mapping in plateau areas according to claim 2, wherein: clearance subassembly (6) include sliding connection in carriage (61) of lifter plate (41) inside, the bottom fixedly connected with cleaning pad (62) of carriage (61), and the end face contact of cleaning pad (62) and survey and drawing camera (5), and support fixedly connected with electric telescopic handle (63) is passed through to one side at the top of lifter plate (41), the flexible end and carriage (61) fixed connection of electric telescopic handle (63).
5. The aircraft for geographical mapping in plateau areas according to claim 1, wherein: buffer unit (7) is including being fixed in U type frame (71) of connecting plate (2) bottom, sliding connection has between the front of U type frame (71) and the back frame (72) that falls, the top fixedly connected with T type pole (73) of frame (72) that falls, the surface cover of T type pole (73) is equipped with damping cover (74), damping cover (74) are fixed in the inside of U type frame (71).
6. The aircraft for geographical mapping in plateau areas according to claim 5, wherein: the top of the T-shaped rod (73) is fixedly connected with a buffer spring (75), and the top end of the buffer spring (75) is fixed at the top of the inner wall of the U-shaped frame (71).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221216727.XU CN217918412U (en) | 2022-05-18 | 2022-05-18 | A aircraft for geographical mapping for plateau area |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221216727.XU CN217918412U (en) | 2022-05-18 | 2022-05-18 | A aircraft for geographical mapping for plateau area |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217918412U true CN217918412U (en) | 2022-11-29 |
Family
ID=84177794
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221216727.XU Active CN217918412U (en) | 2022-05-18 | 2022-05-18 | A aircraft for geographical mapping for plateau area |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217918412U (en) |
-
2022
- 2022-05-18 CN CN202221216727.XU patent/CN217918412U/en active Active
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