CN210310880U - Unmanned aerial vehicle topography survey device - Google Patents
Unmanned aerial vehicle topography survey device Download PDFInfo
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- CN210310880U CN210310880U CN201920741429.4U CN201920741429U CN210310880U CN 210310880 U CN210310880 U CN 210310880U CN 201920741429 U CN201920741429 U CN 201920741429U CN 210310880 U CN210310880 U CN 210310880U
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Abstract
The utility model discloses an unmanned aerial vehicle topography measuring device, include: remote control unmanned aerial vehicle body, topography survey ware and transparent protection casing, the bottom central point of remote control unmanned aerial vehicle body puts department spiral connection and has multidirectional shock attenuation frame, the topography survey ware passes through the mount pad spiral to be fixed on multidirectional shock attenuation frame, and the bottom of topography survey ware is connected with measuring probe. The utility model discloses in, rotate through the transparent protection casing outside in the measuring probe outside and be connected with U type clearance frame, when carrying out high altitude measurement topography, when dust steam is adhered to in the transparent protection casing outside, can drive U type clearance frame and rotate through driving motor to clear up transparent protection casing in the high altitude is automatic, do not need the descending manual clearance that clears up, prevent to influence the measuring accuracy degree, the improvement work efficiency who is showing.
Description
Technical Field
The utility model relates to a topographic survey device technical field especially relates to an unmanned aerial vehicle topographic survey device.
Background
Unmanned aerial vehicles are unmanned aerial vehicles operated by radio remote control equipment and self-contained program control devices, or are operated by vehicle-mounted computers completely or intermittently and autonomously, and can be divided into military and civil use according to application fields, and the unmanned aerial vehicles are divided into reconnaissance planes and target planes. In the civil aspect, the application of the unmanned aerial vehicle industry is really just needed for the unmanned aerial vehicle, and the unmanned aerial vehicle is currently applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like, so that the application of the unmanned aerial vehicle is greatly expanded, and the developed countries are also actively used in the industry and develop the unmanned aerial vehicle technology.
Unmanned aerial vehicle topography measuring device is exactly through the device that unmanned aerial vehicle carried on the topographic survey ware and carries out the topographic survey, traditional unmanned aerial vehicle topographic survey device structure is comparatively simple, measuring probe on the topographic survey ware lacks the measure of automatic clearance of going on, when unmanned aerial vehicle carried on topographic survey device when flying at high altitude, need descend when attaching to dust or steam on the measuring probe and manually clear up, the troublesome poeration, measure the degree of accuracy that influences the measurement simultaneously after that, seriously influence work efficiency.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle topography measuring device who proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme: an unmanned aerial vehicle terrain measurement device, comprising: remotely controlling the unmanned aerial vehicle body, the topographic survey meter and the transparent protective cover;
the bottom center of the remote control unmanned aerial vehicle body is spirally connected with a multidirectional damping frame;
the topographic surveying instrument is spirally fixed on the multidirectional shock absorption frame through a mounting seat, and the bottom of the topographic surveying instrument is connected with a surveying probe;
the transparent protective cover is fixedly sleeved at the bottom end of the topographic surveying instrument, the outer side of the transparent protective cover is rotatably connected with a U-shaped cleaning frame through a rotating connecting shaft, and the U-shaped cleaning frame is mutually attached to the outer side of the transparent protective cover.
As a further description of the above technical solution:
the device also comprises a driving motor;
the driving motor is fixedly connected to the mounting seat through a connecting rod, and the driving motor is rotatably connected with a rotating connecting shaft on the U-shaped cleaning frame through a coupler.
As a further description of the above technical solution:
the bilateral symmetry welding of remote control unmanned aerial vehicle body has two rotor side bearers, and the fixedly connected with of rotor side bearer rotates the rotor.
As a further description of the above technical solution:
be located two on the same side of remote control unmanned aerial vehicle body be connected with the connection side bearer between the rotor side bearer top, and connect two symmetrical auxiliary stay frames that have two V-arrangement distributions in side bearer terminal position department, wherein, two auxiliary stay frame's top distribution and two rotor side bearers and this body hookup location department welding of remote control unmanned aerial vehicle.
As a further description of the above technical solution:
a triangular structure is formed among the auxiliary supporting frame, the rotor wing side frame and the connecting side frame.
As a further description of the above technical solution:
the unmanned aerial vehicle also comprises an unmanned aerial vehicle empennage;
a horizontal tail wing and a vertical tail wing are fixed at the tail end of the unmanned aerial vehicle tail wing;
the horizontal tail and the vertical tail are mutually perpendicular to form a cross distribution.
Advantageous effects
The utility model provides an unmanned aerial vehicle topography measuring device. The method has the following beneficial effects:
(1): this unmanned aerial vehicle topography measuring device rotates through the transparent protection casing outside in the measuring probe outside and is connected with U type clearance frame, when carrying out the high altitude survey topography, when dust steam is adhered to in the transparent protection casing outside, can drive U type clearance frame and rotate through driving motor to clear up transparent protection casing in the high altitude is automatic, do not need the descending manual clearance of clearing up, prevent to influence the measuring accuracy degree, the improvement work efficiency who is showing.
(2): this unmanned aerial vehicle topography survey device is connected with connection side bearer and auxiliary stay frame through between the rotor side bearer with one side, can support the rotor side bearer through connecting side bearer and auxiliary stay frame, strengthen the stability of rotor side bearer, stability when horizontal fin and the perpendicular fin in the unmanned aerial vehicle fin can strengthen the remote control unmanned aerial vehicle body and remove simultaneously to reduce the vibrations that the remote control unmanned aerial vehicle carried on the flight of topographic survey ware and examined time measuring, improve the degree of accuracy to topographic survey, strengthen this unmanned aerial vehicle topography survey device's practicality.
Drawings
Fig. 1 is a schematic view of the overall structure of a topographic surveying device for an unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic structural diagram of the middle topography measuring device of the present invention;
fig. 3 is the utility model discloses the structure schematic diagram of remote control unmanned aerial vehicle body.
Illustration of the drawings:
1. remotely controlling the unmanned aerial vehicle body; 2. a multidirectional shock-absorbing mount; 3. a mounting seat; 4. a topography measurer; 5. a measuring probe; 6. a transparent protective cover; 7. a connecting rod; 8. a drive motor; 9. rotating the connecting shaft; 10. a U-shaped cleaning frame; 11. a rotor side frame; 111. rotating the rotor; 112. connecting the side frames; 113. an auxiliary support frame; 12. an unmanned aerial vehicle empennage; 121. a horizontal rear wing; 122. a vertical tail.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1 and 2, an unmanned aerial vehicle terrain measurement device includes: the unmanned aerial vehicle comprises a remote control unmanned aerial vehicle body 1, a topographic survey meter 4 and a transparent protective cover 6;
the bottom center of the remote control unmanned aerial vehicle body 1 is spirally connected with a multidirectional damping frame 2;
the topographic measuring device 4 is spirally fixed on the multidirectional shock absorption frame 2 through the mounting seat 3, and the bottom of the topographic measuring device 4 is connected with the measuring probe 5;
Also comprises a driving motor 8;
the driving motor 8 is fixedly connected to the mounting base 3 through a connecting rod 7, and the driving motor 8 is rotatably connected with a rotating connecting shaft 9 on the U-shaped cleaning frame 10 through a coupler.
Two rotor side frames 11 are symmetrically welded on two sides of the remote control unmanned aerial vehicle body 1, and the rotor side frames 11 are fixedly connected with rotary rotors 111.
The working principle is as follows: this unmanned aerial vehicle topography measuring device is when using, can fly through 1 carry-on topography measuring ware 4 of remote control unmanned aerial vehicle body, then carry out topography measuring through measuring probe 5 of 4 bottoms of topography measuring ware, when measuring, when being attached to dust and steam influence normal measurement on transparent protection casing 6 in the measuring probe 5 outside, the staff can control driving motor 8 through the remote control, driving motor 8 rotates U type clearance frame 10 that connecting axle 9 drove the 6 outsides of transparent protection casing through the shaft coupling cooperation, U type clearance frame 10 can clear up dust and steam on transparent protection casing 6 automatically, realize clearing up transparent protection casing 6 automatically in the high altitude, do not need the manual clearance that clears up that descends, prevent to influence the measuring accuracy, the improvement topography measuring's that is showing efficiency.
Referring to fig. 3, a connecting side frame 112 is connected between the top ends of two rotor side frames 11 located on the same side of the remote control unmanned aerial vehicle body 1, and two symmetrical auxiliary support frames 113 distributed in a V shape are arranged at the terminal positions of the connecting side frame 112, wherein the top ends of the two auxiliary support frames 113 are welded to the connecting positions of the two rotor side frames 11 and the remote control unmanned aerial vehicle body 1.
The auxiliary support frame 113 forms a triangular structure with the rotor side frame 11 and the connecting side frame 112.
Referring to fig. 3, further comprising an unmanned aerial vehicle tail 12;
a horizontal tail wing 121 and a vertical tail wing 122 are fixed at the tail end of the unmanned aerial vehicle tail wing 12;
horizontal rear wing 121 and vertical rear wing 122 are arranged perpendicular to each other in a cruciform shape.
Stability when horizontal tail 121 and vertical tail 122 can strengthen remote control unmanned aerial vehicle body 1 and remove to reduce the vibrations when remote control unmanned aerial vehicle body 1 carries on the flight detection of topographic survey ware 4, improve the degree of accuracy to the topographic survey ware 4 topographic survey.
In the description herein, references to the description of "one embodiment," "an example," "a specific example," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. An unmanned aerial vehicle terrain measurement device, comprising: the unmanned aerial vehicle remote control system comprises a remote control unmanned aerial vehicle body (1), a topographic survey meter (4) and a transparent protective cover (6);
the bottom center of the remote control unmanned aerial vehicle body (1) is spirally connected with a multidirectional damping frame (2);
the topographic surveying instrument (4) is spirally fixed on the multidirectional shock absorption frame (2) through the mounting seat (3), and the bottom of the topographic surveying instrument (4) is connected with the surveying probe (5);
transparent protection casing (6) are fixed cup joints in the bottom of topography survey ware (4), and the outside of transparent protection casing (6) is rotated through rotating connecting axle (9) and is connected with U type clearance frame (10), the outside of U type clearance frame (10) and transparent protection casing (6) is laminated each other.
2. A drone terrain measurement arrangement as claimed in claim 1, characterised by further comprising a drive motor (8);
the driving motor (8) is fixedly connected to the mounting base (3) through a connecting rod (7), and the driving motor (8) is rotatably connected with a rotating connecting shaft (9) on the U-shaped cleaning frame (10) through a coupler.
3. The terrain measurement device of unmanned aerial vehicles according to claim 1, characterized in that two rotor side frames (11) are symmetrically welded to both sides of the remote-controlled unmanned aerial vehicle body (1), and the rotor (111) is rotated by the fixed connection of the rotor side frames (11).
4. The unmanned aerial vehicle terrain measuring device of claim 3, characterized in that a connecting side frame (112) is connected between the top ends of the two rotor side frames (11) on the same side of the remote control unmanned aerial vehicle body (1), and two auxiliary supporting frames (113) with two V-shaped distributions are symmetrically arranged at the terminal position of the connecting side frame (112), wherein the top distribution of the two auxiliary supporting frames (113) is welded with the connecting position of the two rotor side frames (11) and the remote control unmanned aerial vehicle body (1).
5. The unmanned aerial vehicle terrain measurement device of claim 4, wherein the auxiliary support frame (113) forms a triangular structure with the rotor side frame (11) and the connecting side frame (112).
6. The unmanned aerial vehicle terrain measurement device of claim 1, further comprising an unmanned aerial vehicle tail (12);
a horizontal tail wing (121) and a vertical tail wing (122) are fixed at the tail end of the unmanned aerial vehicle tail wing (12);
the horizontal tail (121) and the vertical tail (122) are mutually perpendicular and distributed in a cross shape.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201920741429.4U CN210310880U (en) | 2019-05-22 | 2019-05-22 | Unmanned aerial vehicle topography survey device |
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| CN201920741429.4U CN210310880U (en) | 2019-05-22 | 2019-05-22 | Unmanned aerial vehicle topography survey device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111412898A (en) * | 2020-04-16 | 2020-07-14 | 中国建筑股份有限公司 | Large-area deformation photogrammetry method based on ground-air coupling |
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2019
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111412898A (en) * | 2020-04-16 | 2020-07-14 | 中国建筑股份有限公司 | Large-area deformation photogrammetry method based on ground-air coupling |
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