CN216887225U - Unmanned aerial vehicle for engineering survey - Google Patents
Unmanned aerial vehicle for engineering survey Download PDFInfo
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- CN216887225U CN216887225U CN202122482725.7U CN202122482725U CN216887225U CN 216887225 U CN216887225 U CN 216887225U CN 202122482725 U CN202122482725 U CN 202122482725U CN 216887225 U CN216887225 U CN 216887225U
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- aerial vehicle
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- threaded rod
- engineering survey
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Abstract
The utility model discloses an unmanned aerial vehicle for engineering measurement, which comprises an unmanned aerial vehicle body, wherein an adjusting base is fixedly mounted on the unmanned aerial vehicle body, a camera is arranged on the adjusting base, a foam block is fixedly mounted at the bottom end of the unmanned aerial vehicle body, an arm rod is fixedly mounted on the unmanned aerial vehicle body, a driving mechanism is fixedly mounted on the arm rod, an output shaft is connected to the driving mechanism in a transmission manner, a turntable is fixedly mounted on the output shaft, a threaded rod is inserted into the turntable, and a sleeve block is sleeved on the threaded rod. This kind of unmanned aerial vehicle for engineering survey based on 5G signal transmission, the modern design, easy operation, the adaptation environment is many, has higher practical value.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle for engineering survey.
Background
Unmanned aerial vehicle can be used for the electric power to patrol and examine the shooting, the very extensively in the field that unmanned aerial vehicle used, be equipped with high definition digital video camera and GPS positioning system on unmanned aerial vehicle, can follow the electric wire netting and fix a position independently and cruise, the image is shot in real-time conveying, the control personnel can be synchronous on the computer, current unmanned aerial vehicle most of all can only descend on the land, unmanned aerial vehicle will compel to land when not having the electricity, when compelling to descend under the position having water the condition, make unmanned aerial vehicle descend in water easily, and thereby most of unmanned aerial vehicle screw easy touching causes the damage on the object when flying, change very trouble. Therefore, the unmanned aerial vehicle for engineering survey is provided by improving the unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problems, the utility model provides the following technical scheme:
the utility model discloses an unmanned aerial vehicle for engineering measurement, which comprises an unmanned aerial vehicle body, wherein an adjusting base is fixedly mounted on the unmanned aerial vehicle body, a camera is arranged on the adjusting base, a foam block is fixedly mounted at the bottom end of the unmanned aerial vehicle body, an arm rod is fixedly mounted on the unmanned aerial vehicle body, a driving mechanism is fixedly mounted on the arm rod, an output shaft is connected to the driving mechanism in a transmission manner, a turntable is fixedly mounted on the output shaft, a threaded rod is inserted into the turntable, a sleeve block is sleeved on the threaded rod, a sleeve ring is sleeved on the sleeve block, a pull rod is hinged to the sleeve ring and hinged to a slider, the slider is mounted in a limiting groove, the limiting groove is arranged in the turntable, and a propeller is arranged on the turntable.
As a preferred technical scheme of the utility model, the unmanned aerial vehicle body is fixedly provided with a support frame, and the support frame is fixedly provided with a rubber mat.
As a preferred technical scheme of the utility model, a groove structure is arranged in the rotary table, and the bottom end of the threaded rod is inserted in the groove.
As a preferred technical scheme of the utility model, the turntable is provided with an inserting structure, and the cross section of the limiting groove is trapezoidal.
As a preferred technical scheme of the utility model, the sleeve block is internally provided with internal threads, and the sleeve block and the threaded rod form a spiral rotating structure.
As a preferred technical scheme of the utility model, a sliding groove structure is arranged in the limiting groove, and the sliding groove and the sliding block form a sliding structure.
The utility model has the beneficial effects that:
1. according to the unmanned aerial vehicle for engineering measurement, the foam block is matched with the rubber mat for use, when the electric quantity of the unmanned aerial vehicle body is insufficient and the unmanned aerial vehicle body needs to be forced to land on the water surface, the unmanned aerial vehicle body can float on the water surface through the foam block, and the unmanned aerial vehicle body is prevented from directly sinking into the water;
2. this kind of unmanned aerial vehicle for engineering survey uses through threaded rod and cover block cooperation, when needs are changed the screw, the cover block carries out the rebound when rotating the threaded rod, makes the lantern ring remove through the removal of cover block to the lantern ring of being convenient for removes through pull rod pulling slider, thereby is convenient for carry out single dismantlement to the screw and comes out the change.
Drawings
The accompanying drawings, which are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate embodiments of the utility model and together with the description serve to explain the principles of the utility model and not to limit the utility model. In the drawings:
fig. 1 is a perspective view of an unmanned aerial vehicle for engineering survey according to the present invention;
fig. 2 is an enlarged schematic structural diagram of a point a in fig. 1 of the unmanned aerial vehicle for engineering survey of the present invention;
FIG. 3 is a perspective view of a turntable of an unmanned aerial vehicle for engineering survey according to the present invention;
fig. 4 is a schematic view of a front view cross section structure of a turntable of the unmanned aerial vehicle for engineering survey.
In the figure: 1. an unmanned aerial vehicle body; 101. adjusting the base; 102. a camera; 103. a foam block; 104. a support frame; 105. a rubber pad; 2. an arm lever; 201. a drive mechanism; 202. an output shaft; 203. a turntable; 204. a threaded rod; 205. sleeving blocks; 206. a collar; 207. a pull rod; 208. a slider; 209. a limiting groove; 211. and a propeller.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are described herein for the purpose of illustration and explanation and not limitation.
Example (b): as shown in fig. 1-4, the unmanned aerial vehicle for engineering survey comprises an unmanned aerial vehicle body 1, an adjusting base 101 is fixedly installed on the unmanned aerial vehicle body 1, a camera 102 is installed on the adjusting base 101, a foam block 103 is fixedly installed at the bottom end of the unmanned aerial vehicle body 1, an arm rod 2 is fixedly installed on the unmanned aerial vehicle body 1, a driving mechanism 201 is fixedly installed on the arm rod 2, an output shaft 202 is connected onto the driving mechanism 201 in a transmission manner, a rotary table 203 is fixedly installed on the output shaft 202, a threaded rod 204 is inserted onto the rotary table 203, a sleeve block 205 is sleeved on the threaded rod 204, a sleeve ring 206 is sleeved on the sleeve block 205, a pull rod 207 is hinged onto the sleeve ring 206, the pull rod 207 is hinged onto a slide block 208, the slide block 208 is installed in a limiting groove 209, the limiting groove 209 is opened in the rotary table 203, and a propeller 211 is installed on the rotary table 203.
Wherein, fixed mounting has support frame 104 on the unmanned aerial vehicle body 1, and fixed mounting has cushion 105 on the support frame 104, and cushion 105 can be convenient for unmanned aerial vehicle body 1 descends and carries out the shock attenuation on the ground, prevents to cause the damage to the inside components and parts of unmanned aerial vehicle body 1.
Wherein, carousel 203 is inside to be provided with groove structure, and threaded rod 204 bottom is inserted and is established in the recess, and the bottom of the threaded rod 204 of being convenient for rotates in the recess of carousel 203.
Wherein, be provided with on the carousel 203 and insert and establish the structure, the cross section of spacing groove becomes trapezoidal form, and the screw 211 of being convenient for is inserted and is established and fix in the trapezoidal inslot.
Wherein, the inside internal thread that is provided with of cover block 205, and cover block 205 and threaded rod 204 constitute spiral rotary type structure, and the rotation through threaded rod 204 makes cover block 205 remove.
Wherein, the inside spout structure that is provided with of spacing groove 209, and the spout constitutes slidingtype structure with slider 208, stability when increasing slider 208 and removing.
The working principle is as follows: this unmanned aerial vehicle body 1 facial make-up is equipped with camera 102, regulation through adjusting base 101 makes camera 102 shoot the angle and adjusts, when forced landing on the surface of water when unmanned aerial vehicle body 1 does not have the electric quantity, fixed mounting has foam block 103 on unmanned aerial vehicle body 1, can make unmanned aerial vehicle body 1 float on the surface of water through foam block 103, it is more stable that unmanned aerial vehicle body 1 is to increase buoyancy through cushion 105, when needs carry out single change to screw 211, rotate screw 204, the cover is equipped with sleeve block 205 on screw 204, the rotation through screw 204 makes sleeve block 205 remove, sleeve block 205's removal makes lantern ring 206 remove through pull rod 207 pulling slider 208, thereby be convenient for take out the screw 211 of establishing at the dovetail groove, change single screw 211, very practicality.
Finally, it should be noted that: in the description of the present invention, it should be noted that the terms "vertical", "upper", "lower", "horizontal", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, which are only for convenience of description and simplification of the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and operate, and thus, should not be construed as limiting the present invention.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the utility model. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle for engineering survey, includes unmanned aerial vehicle body (1), its characterized in that, fixed mounting has regulation base (101) on unmanned aerial vehicle body (1), and adjusts base (101) facial make-up and be equipped with camera (102), the bottom fixed mounting of unmanned aerial vehicle body (1) has foam piece (103), fixed mounting has armed lever (2) on unmanned aerial vehicle body (1), and fixed mounting has actuating mechanism (201) on armed lever (2), driving mechanism (201) goes up the drive connection and has output shaft (202), and fixed mounting has carousel (203) on output shaft (202), be equipped with threaded rod (204) on inserting on carousel (203), and the cover is equipped with nest block (205) on threaded rod (204), the cover is equipped with lantern ring (206) on nest block (205), and articulated on lantern ring (206) have pull rod (207), and pull rod (207) articulates on slider (208), slider (208) are installed in spacing groove (209), and spacing groove (209) are seted up in carousel (203), carousel (203) facial make-up is equipped with screw (211).
2. The unmanned aerial vehicle for engineering measurement as claimed in claim 1, wherein the unmanned aerial vehicle body (1) is fixedly provided with a support frame (104), and the support frame (104) is fixedly provided with a rubber mat (105).
3. Unmanned aerial vehicle for engineering survey of claim 1, characterized in that carousel (203) is inside to be provided with the groove structure, and threaded rod (204) bottom is inserted and is established in the recess.
4. The unmanned aerial vehicle for engineering survey as claimed in claim 1, wherein the turntable (203) is provided with an inserting structure, and the cross section of the limiting groove (209) is trapezoidal.
5. The unmanned aerial vehicle for engineering survey of claim 1, characterized in that, the inside of cover piece (205) is provided with the internal thread, and set piece (205) and threaded rod (204) constitute spiral rotary type structure.
6. The unmanned aerial vehicle for engineering survey of claim 1, characterized in that, the inside of spacing groove (209) is provided with the spout structure, and the spout constitutes the slidingtype structure with slider (208).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122482725.7U CN216887225U (en) | 2021-10-15 | 2021-10-15 | Unmanned aerial vehicle for engineering survey |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122482725.7U CN216887225U (en) | 2021-10-15 | 2021-10-15 | Unmanned aerial vehicle for engineering survey |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216887225U true CN216887225U (en) | 2022-07-05 |
Family
ID=82194488
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122482725.7U Active CN216887225U (en) | 2021-10-15 | 2021-10-15 | Unmanned aerial vehicle for engineering survey |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216887225U (en) |
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2021
- 2021-10-15 CN CN202122482725.7U patent/CN216887225U/en active Active
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