CN219382830U - Aerophotography mapping device with multidirectional angle adjustment - Google Patents
Aerophotography mapping device with multidirectional angle adjustment Download PDFInfo
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- CN219382830U CN219382830U CN202223456895.9U CN202223456895U CN219382830U CN 219382830 U CN219382830 U CN 219382830U CN 202223456895 U CN202223456895 U CN 202223456895U CN 219382830 U CN219382830 U CN 219382830U
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Abstract
The utility model belongs to the technical field of aerial photography devices, and particularly relates to an aerial photography mapping device with multi-azimuth angle adjustment, which comprises an unmanned aerial vehicle and a camera device.
Description
Technical Field
The utility model belongs to the technical field of aerial photography devices, and particularly relates to an aerial photography mapping device with multi-azimuth angle adjustment.
Background
Mapping is to measure, collect and map the shape, size, spatial position and the like of natural geographic elements or surface artificial facilities. Mapping has wide application in economic construction and national defense construction. In urban and rural construction planning, homeland resource utilization, environmental protection and other works, various maps for land measurement and mapping must be performed for planning and management. In the construction of geological exploration, mineral exploitation, water conservancy, traffic, etc., control measurement, mine measurement, route measurement and topographic map drawing are necessary for geological survey and various building design construction.
At present, many aerial photography mapping devices are installed, because of limitations of an installation device, a camera used for carrying out the photography mapping devices cannot flexibly move, a shot picture is relatively one-sided, a shot range is relatively limited and narrow, a part of the device can move, the camera angle of the camera cannot be flexibly adjusted, variability and flexibility are low, the actual working use range is relatively small, and the flexible use requirement cannot be met.
Disclosure of Invention
In view of the above-mentioned shortcomings in the prior art, the present utility model provides an aerial photography mapping device with multi-azimuth angle adjustment, which is used for solving the problems in the background art.
In order to solve the technical problems, the utility model adopts the following technical scheme:
the aerophotography mapping device comprises an unmanned aerial vehicle and a camera device, wherein the unmanned aerial vehicle comprises a machine body, four propellers and a machine shell, the number of the propellers is four, the propellers are arranged on the machine body, and a fixed rod is arranged at the front end of the machine body;
the camera device comprises a connecting seat frame, a connecting arm and a camera, wherein the connecting seat frame is connected with a machine body, a first motor is vertically and fixedly installed on the connecting seat frame downwards, the connecting arm is rotatably installed on an output shaft of the first motor, a second motor is horizontally and fixedly installed on the connecting arm, a fixing seat is fixedly connected on an output shaft of the second motor, and the camera is installed on the fixing seat.
When the aerial photography mapping device is specifically used, in order to solve the problem that a camera instrument cannot flexibly move when the existing aerial photography mapping device is used, a shot picture is compared with a slice surface, the shot range is limited and narrow, the aerial photography mapping device comprises an unmanned aerial vehicle and a camera device, the device comprises two large components, wherein the camera device is installed on a body of the unmanned aerial vehicle through a connecting seat frame, a first motor and a connecting arm are installed on the connecting seat frame, one end of the connecting arm is connected with an output rotating shaft of the first motor, a second motor is installed at the other end of the connecting arm, a fixing seat is installed on the output rotating shaft of the second motor, the camera is installed on a sub-fixing seat, during use, the connecting arm can rotate in a horizontal plane through the operation of the first motor, meanwhile, the fixing seat can rotate in a vertical plane, the multi-angle photography mapping is realized, the multi-angle photography mapping of the camera horizontal plane and the multi-angle photography instrument is realized on the whole, and the flexibility of the camera device is improved.
Further, the upper end of the connecting seat frame is provided with a pipe clip, and the connecting seat frame is connected with a fixing rod of the machine body through the pipe clip.
Further, the middle part of the machine body is provided with a landing gear, and the front end of the bottom of the machine body is provided with an auxiliary supporting frame.
Further, an audible alarm device is installed on the unmanned aerial vehicle.
Further, the following: and a lamplight alarm device is arranged on the unmanned aerial vehicle.
When specifically using, in order to let photographic mapping device safety protection nature, install audible alarm and light alarm on unmanned aerial vehicle, they are connected with the inside electronic original paper of unmanned aerial vehicle.
Compared with the prior art, the utility model has the following beneficial effects:
1. the connecting arm rotates in the horizontal plane through the work of the first motor to realize multi-angle shooting and mapping, and meanwhile, the fixing seat rotates in the vertical plane through the work of the second motor to realize multi-angle shooting and mapping, so that the multi-angle shooting and mapping of the horizontal plane and the vertical plane of the camera are realized on the whole, the shooting angle of a shooting instrument is flexibly adjusted, and the variability and the flexibility of a shooting and mapping device are improved;
2. in order to make the photographic mapping device safe and protective, an acoustic alarm device and a lamplight alarm device are arranged on the unmanned aerial vehicle.
Drawings
FIG. 1 is a schematic perspective view of an aero-photogrammetry device with multi-azimuth angle adjustment (view angle I) according to an embodiment of the present utility model;
FIG. 2 is a schematic perspective view of an aero-photogrammetry device with multi-azimuth angle adjustment (view II) according to an embodiment of the present utility model;
FIG. 3 is a schematic perspective view of an aero-photogrammetry device with multi-azimuth angle adjustment (view three) according to an embodiment of the present utility model;
FIG. 4 is a schematic perspective view of an aerial survey device with a housing removed for multi-azimuth angular adjustment according to an embodiment of the present utility model;
FIG. 5 is a schematic perspective view of the removal propeller of FIG. 4;
FIG. 6 is a schematic perspective view of an imaging device in an embodiment of an aero-camera mapping device with multi-azimuth angle adjustment according to the present utility model;
reference numerals in the drawings of the specification include:
an unmanned plane 1 and a camera device 2;
the device comprises a machine body 101, a fixed rod 1011, a propeller 102, a machine shell 103, an acoustic alarm device 104, a light alarm device 105, an auxiliary supporting frame 106 and a landing gear 107;
a connecting seat frame 201, a pipe clamp 2011, a first motor 202, a connecting arm 203, a second motor 204, a fixing seat 205 and a camera 206.
Detailed Description
In order that those skilled in the art will better understand the present utility model, the following technical scheme of the present utility model will be further described with reference to the accompanying drawings and examples.
Wherein the drawings are for illustrative purposes only and are shown in schematic, non-physical, and not intended to be limiting of the present patent; for the purpose of better illustrating embodiments of the utility model, certain elements of the drawings may be omitted, enlarged or reduced and do not represent the size of the actual product; it will be appreciated by those skilled in the art that certain well-known structures in the drawings and descriptions thereof may be omitted.
The same or similar reference numbers in the drawings of embodiments of the utility model correspond to the same or similar components; in the description of the present utility model, it should be understood that, if the terms "upper", "lower", "left", "right", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, only for convenience in describing the present utility model and simplifying the description, rather than indicating or implying that the apparatus or elements being referred to must have a specific orientation, be constructed and operated in a specific orientation, so that the terms describing the positional relationships in the drawings are merely for exemplary illustration and should not be construed as limiting the present patent, and that the specific meaning of the terms described above may be understood by those of ordinary skill in the art according to specific circumstances.
In the description of the present utility model, unless explicitly stated and limited otherwise, the term "coupled" or the like should be interpreted broadly, as it may be fixedly coupled, detachably coupled, or integrally formed, as indicating the relationship of components; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between the two parts or interaction relationship between the two parts. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
Embodiment one:
as shown in fig. 1-6, the present utility model. Specifically, an aerophotography mapping device with multi-azimuth angle adjustment comprises an unmanned aerial vehicle 1 and a camera device 2, wherein the unmanned aerial vehicle 1 comprises a machine body 101, propellers 102 and a machine shell 103, the number of the propellers 102 is four, the propellers 102 are arranged on the machine body 101, and a fixed rod 1011 is arranged at the front end of the machine body 101; the camera device 2 comprises a connecting seat frame 201 and a connecting arm 203, and a camera 206, wherein the connecting seat frame 201 is connected with the machine body 101, a first motor 202 is vertically and fixedly installed on the connecting seat frame 201 downwards, the connecting arm 203 is rotatably installed on an output shaft of the first motor 202, a second motor 204 is horizontally and fixedly installed on the connecting arm 203, a fixing seat 205 is fixedly connected on an output shaft of the second motor 204, and the camera 206 is installed on the fixing seat 205. The upper end of the connection seat frame 201 is provided with a pipe clip 2011, and the connection seat frame 201 is connected with a fixed rod 1011 of the machine body 101 through the pipe clip 2011. The middle part of fuselage 101 is equipped with undercarriage 107, and fuselage 101 bottom front end is equipped with auxiliary stay 106. The unmanned aerial vehicle 1 is provided with an audible alarm 104.: the unmanned aerial vehicle 1 is provided with a light alarm device 105. In particular use, in order to make the photogrammetry device safe and protective, on the unmanned aerial vehicle 1, an acoustic alarm device 104 and a light alarm device 105 are installed, which are connected to the electronic components inside the unmanned aerial vehicle 1.
When specifically using, in order to overcome the problem that current aerial photography survey device can not remove in a flexible way when using the instrument of making a video recording for the picture that shoots is more unilateral, and the restriction of the scope comparison of shooting is narrow, we have designed an aerial photography survey device of diversified angle modulation, the device includes unmanned aerial vehicle 1 and two big subassemblies of camera device 2, wherein camera device 2 passes through connecting seat frame 201 and installs on unmanned aerial vehicle 1's fuselage 101, and the top of connecting seat frame 201 is equipped with pipe buckle clamp 2011, can be as shown in figure 5, connects on fuselage 101 front end's dead lever 1011, realizes camera device 2 and unmanned aerial vehicle 1's connection. The connecting seat frame 201 is provided with a first motor 202 and a connecting arm 203, one end of the connecting arm 203 is connected with an output rotating shaft of the first motor 202, the other end of the connecting arm 203 is provided with a second motor 204, the output rotating shaft of the second motor 204 is provided with a fixing seat 205, the camera 206 is provided with a sub-fixing seat 205, when in use, the connecting arm 203 can rotate in a horizontal plane to realize multi-angle camera mapping through the operation of the first motor 202, and meanwhile, the fixing seat 205 can rotate in a vertical plane through the operation of the second motor 204 to realize multi-angle camera mapping, so that the multi-angle camera mapping of the horizontal plane and the vertical plane of the camera 206 is realized on the whole, the camera angle of a camera instrument is flexibly adjusted, and the variability and the flexibility of a camera mapping device are improved.
The foregoing is merely exemplary of the present utility model, and the specific structures and features well known in the art are not described in any way herein, so that those skilled in the art will be able to ascertain all prior art in the field, and will not be able to ascertain any prior art to which this utility model pertains, without the general knowledge of the skilled person in the field, before the application date or the priority date, to practice the present utility model, with the ability of these skilled persons to perfect and practice this utility model, with the help of the teachings of this application, with some typical known structures or methods not being the obstacle to the practice of this application by those skilled in the art. It should be noted that modifications and improvements can be made by those skilled in the art without departing from the structure of the present utility model, and these should also be considered as the scope of the present utility model, which does not affect the effect of the implementation of the present utility model and the utility of the patent.
Claims (5)
1. An aerophotography mapping device of diversified angle modulation, its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle (1) and a camera device (2), wherein the unmanned aerial vehicle (1) comprises a machine body (101), propellers (102) and a machine shell (103), the number of the propellers (102) is four, the propellers are arranged on the machine body (101), and a fixed rod (1011) is arranged at the front end of the machine body (101);
the camera device (2) comprises a connecting seat frame (201), a connecting arm (203) and a camera (206), wherein the connecting seat frame (201) is connected with a machine body (101), a first motor (202) is vertically and fixedly installed on the connecting seat frame (201) downwards, the connecting arm (203) is rotatably installed on an output shaft of the first motor (202), a second motor (204) is horizontally and fixedly installed on the connecting arm (203), a fixing seat (205) is fixedly connected on an output shaft of the second motor (204), and the camera (206) is installed on the fixing seat (205).
2. An aero-photogrammetry device with multi-azimuth angular adjustment as claimed in claim 1, wherein: the upper end of the connecting seat frame (201) is provided with a pipe clip (2011), and the connecting seat frame (201) is connected with a fixed rod (1011) of the machine body (101) through the pipe clip (2011).
3. An aero-photogrammetry device with multi-azimuth angular adjustment as claimed in claim 2, wherein: the middle part of fuselage (101) is equipped with undercarriage (107), fuselage (101) bottom front end is equipped with auxiliary stay frame (106).
4. An aero-photogrammetry device with multi-azimuth angular adjustment as claimed in claim 3, wherein: an audible alarm device (104) is arranged on the unmanned aerial vehicle (1).
5. An aero-photogrammetry device with multi-azimuth angular adjustment as claimed in claim 4, wherein: and a lamplight alarm device (105) is arranged on the unmanned aerial vehicle (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223456895.9U CN219382830U (en) | 2022-12-23 | 2022-12-23 | Aerophotography mapping device with multidirectional angle adjustment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223456895.9U CN219382830U (en) | 2022-12-23 | 2022-12-23 | Aerophotography mapping device with multidirectional angle adjustment |
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| CN219382830U true CN219382830U (en) | 2023-07-21 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202223456895.9U Active CN219382830U (en) | 2022-12-23 | 2022-12-23 | Aerophotography mapping device with multidirectional angle adjustment |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117048865A (en) * | 2023-10-11 | 2023-11-14 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle carries laser rangefinder |
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- 2022-12-23 CN CN202223456895.9U patent/CN219382830U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117048865A (en) * | 2023-10-11 | 2023-11-14 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle carries laser rangefinder |
| CN117048865B (en) * | 2023-10-11 | 2023-12-19 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle carries laser rangefinder |
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