CN217110943U - Total powerstation device based on unmanned aerial vehicle - Google Patents
Total powerstation device based on unmanned aerial vehicle Download PDFInfo
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- CN217110943U CN217110943U CN202220936244.0U CN202220936244U CN217110943U CN 217110943 U CN217110943 U CN 217110943U CN 202220936244 U CN202220936244 U CN 202220936244U CN 217110943 U CN217110943 U CN 217110943U
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Abstract
The utility model relates to a total station device based on unmanned aerial vehicle, belong to the surveying and mapping technology field, specifically include and install the mount between unmanned aerial vehicle's the landing leg, the total station is installed in the bottom of mount, the connecting plate is installed to the bottom of total station, the bottom of connecting plate has the mounting box through bolted connection, be provided with the injection molding lid on the mounting box, install quick-inflating subassembly and buffering gasbag in the mounting box, quick-inflating subassembly is located buffering gasbag, be provided with annular seal receptacle in the mounting box, be provided with annular closing plate on the opening of buffering gasbag, annular closing plate passes through the fix with screw on annular seal receptacle, install a distance sensor on four landing legs of unmanned aerial vehicle respectively, distance sensor and quick-inflating subassembly are connected with unmanned aerial vehicle flight attitude controller respectively; the utility model discloses simple structure, reasonable in design can carry out abundant protection to the total powerstation, avoids falling and causes the damage.
Description
Technical Field
The utility model relates to a total powerstation device based on unmanned aerial vehicle belongs to the mapping technology field.
Background
The total station is a short for total station type electronic tacheometer, is an optoelectronic instrument combining an electronic theodolite, an optoelectronic distance meter and a microprocessor, and can be almost used in all measurement fields. With the continuous development and application of computer technology, special requirements of users and application of other industrial technologies, carrying a total station by an unmanned aerial vehicle becomes a hotspot in the market.
For example, the publication number is CN214372476U, and the patent name is a topographic map mapping device that unmanned aerial vehicle carried on total powerstation, and it is through effectively combining unmanned aerial vehicle and total powerstation, through set up shock attenuation buffer gear between unmanned aerial vehicle and total powerstation, avoids the influence of the vibrations that produce when unmanned aerial vehicle takes off and land the in-process to the total powerstation. But because the phenomenon that unmanned aerial vehicle appears falling easily at the flight in-process, the total powerstation is expensive, falls and can cause the damage to the total powerstation, leads to unable the use, and current unmanned aerial vehicle equipment who carries on the total powerstation lacks reliable means of protection.
SUMMERY OF THE UTILITY MODEL
For solving the technical problem that prior art exists, the utility model provides a simple structure, reasonable in design can carry out abundant protection to the total powerstation, avoids falling the total powerstation device based on unmanned aerial vehicle that causes the damage.
In order to realize the purpose, the technical proposal adopted by the utility model is a total station device based on an unmanned aerial vehicle, which comprises the unmanned aerial vehicle, the total station and an unmanned aerial vehicle flight attitude controller, a fixing frame is arranged between the supporting legs of the unmanned aerial vehicle, the total station is arranged at the bottom of the fixing frame, the bottom of the total station is provided with a connecting plate, the bottom of the connecting plate is connected with a mounting box through a bolt, the mounting box is provided with an injection molding cover, the mounting box is internally provided with a quick inflation assembly and a buffer air bag, the quick inflation component is positioned in the buffer air bag, an annular sealing seat is arranged in the mounting box, an annular sealing plate is arranged on an opening of the buffering air bag and is fixed on an annular sealing seat through a screw, the four support legs of the unmanned aerial vehicle are respectively provided with a distance sensor, and the distance sensors and the quick inflation assembly are respectively connected with the unmanned aerial vehicle flight attitude controller;
the quick inflation assembly is used for quickly inflating the buffering air bag; the distance sensor is used for detecting the distance between the unmanned aerial vehicle and the bottom surface and sending a trigger signal to the unmanned aerial vehicle flight attitude controller when the unmanned aerial vehicle falls; unmanned aerial vehicle flight attitude controller is used for detecting unmanned aerial vehicle's flight gesture to start the quick aerate subassembly when unmanned aerial vehicle falls and receives distance sensor's trigger signal.
Preferably, the quick charge subassembly is including aerifing box, fixed lid and some firearm, it installs on the mounting box to aerify the box, it is fixed with fixed lid on the box to aerify, some firearm are installed at the center of box to aerify, the externally mounted of some firearm has the cylinder of moulding plastics, the both sides of the cylinder of moulding plastics are provided with the air guide hole, the both sides of box of aerifing are provided with the venthole respectively, the both sides of box of aerifing still are provided with the filter screen fixed slot, install the filter screen in the filter screen fixed slot, the filter screen is located the inboard of venthole, it has the medicament to fill respectively in the cavity between box of aerifing and the cylinder of moulding plastics.
Preferably, the inflatable box is further provided with a cushion block, the cushion block is positioned in the injection separation cylinder, and the medicament of the injection separation cylinder is wrapped by an isolation film.
Preferably, a plurality of supporting bulges are further arranged between the filter screen and the inner wall of the inflating box, and the supporting bulges are arranged on the inner wall of the inflating box.
Preferably, the buffer air bag comprises an annular ring and a hemispherical structure arranged at the lower part of the annular ring.
Compared with the prior art, the utility model discloses following technological effect has: the utility model discloses simple structure, reasonable in design adopts and installs the buffering gasbag subassembly that can explode automatically in the bottom of total powerstation, and when unmanned aerial vehicle appeared falling, unmanned aerial vehicle flight attitude controller can detect the unmanned aerial vehicle signal of falling, controls distance sensor simultaneously and carries out the range finding to receive distance sensor's distance data signal in real time; when distance sensor's distance signal reached the setting value, unmanned aerial vehicle flight attitude controller control quick aerate subassembly is detonating fast to carry out quick aerate to the buffering gasbag, the buffering gasbag is opened rapidly, makes the impact force that buffering gasbag and bottom surface contact buffering unmanned aerial vehicle and total powerstation fallen to the ground, and then avoids unmanned aerial vehicle and total powerstation to damage.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a schematic structural view of the middle buffer airbag of the present invention after being opened.
Fig. 3 is a schematic structural view of the middle quick inflation assembly of the present invention.
Fig. 4 is a bottom view of the middle buffer airbag of the present invention after it is opened.
Detailed Description
In order to make the technical problem, technical solution and advantageous effects to be solved by the present invention more clearly understood, the following description is given in conjunction with the accompanying drawings and embodiments to illustrate the present invention in further detail. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
As shown in fig. 1-4, a total station based on unmanned aerial vehicles, comprising an unmanned aerial vehicle 1, the total station 2 and the unmanned aerial vehicle flight attitude controller, a fixing frame 3 is installed between supporting legs of the unmanned aerial vehicle 1, the total station 2 is installed at the bottom of the fixing frame 3, a connecting plate 4 is installed at the bottom of the total station 2, the bottom of the connecting plate 4 is connected with a mounting box 5 through a bolt, an injection molding cover 6 is arranged on the mounting box 5, a quick inflation assembly 7 and a buffering air bag 8 are installed in the mounting box 5, the quick inflation assembly 7 is located in the buffering air bag 8, an annular sealing seat 9 is arranged in the mounting box 5, an annular sealing plate 10 is arranged on an opening of the buffering air bag 8, the annular sealing plate 10 is fixed on the annular sealing seat 9 through a screw, a distance sensor 11 is respectively installed on each of the four supporting legs of the unmanned aerial vehicle 1, and the distance sensor 11 and the quick inflation assembly 7 are respectively connected with the unmanned aerial vehicle flight attitude controller;
the quick inflation assembly 7 is used for quickly inflating the buffering air bag; the distance sensor 11 is used for detecting the distance between the unmanned aerial vehicle and the bottom surface and sending a trigger signal to the unmanned aerial vehicle flight attitude controller when the unmanned aerial vehicle falls; unmanned aerial vehicle flight attitude controller is used for detecting unmanned aerial vehicle's flight gesture to start the quick aerate subassembly when unmanned aerial vehicle falls and receives distance sensor's trigger signal.
The utility model discloses in adopt and install the gasbag subassembly in the bottom of total powerstation, the gasbag subassembly can appear when falling at unmanned aerial vehicle, opens the buffering gasbag, and then cushion the impact that unmanned aerial vehicle and total powerstation fall to the ground, avoids buffering unmanned aerial vehicle and total powerstation to appear damaging. When the unmanned aerial vehicle normally flies, the unmanned aerial vehicle flight attitude controller detects that the flight attitude of the unmanned aerial vehicle is normal. When the unmanned aerial vehicle falls to cause abnormal flight attitude, controlling the distance sensor to start, and acquiring a distance signal between the unmanned aerial vehicle and the bottom surface in real time through the distance sensor; when the distance reaches a set value, the distance is generally 1-1.5m away from the ground, the distance sensor generates a trigger signal, the unmanned aerial vehicle flight attitude controller controls the quick inflation assembly to be started quickly, the buffering air bag is inflated, the buffering air bag is opened quickly, impact of landing of the unmanned aerial vehicle and the total station is buffered, and further the unmanned aerial vehicle and the total station are protected.
Wherein, quick charge subassembly 7 is including aerifing box 12, fixed lid 13 and some firearm 14, it installs on mounting box 5 to aerify box 12, it is fixed with fixed lid 13 on the box 12 to aerify, it installs some firearm 14 to aerify the center of box 12, the externally mounted of some firearm 14 has the knockout drum 16 of moulding plastics, the both sides of knockout drum 16 of moulding plastics are provided with air guide hole 17, the both sides of aerifing box 12 are provided with venthole 18 respectively, the both sides of aerifing box 12 still are provided with filter screen fixed slot 19, install filter screen 20 in the filter screen fixed slot 19, filter screen 20 is located the inboard of venthole 18, it fills medicament 21 respectively in the cavity between box 12 and the knockout drum 16 of moulding plastics and the knockout drum 16. Quick inflation assembly embeds some firearm and medicament, aerifys as needs, and unmanned aerial vehicle flight attitude control ware control point firearm starts, and some firearm light the medicament, and the medicament violent reaction produces gas and aerifys buffering gasbag. The amount of the medicament is matched with the volume of the buffer air bag, the inflated volume is ensured to be smaller than the volume of the buffer air bag, the buffer air bag is further prevented from being inflated too fully, and the gas above 1/2 can be filled. The inflatable box 12 is also provided with a cushion block 22, the cushion block 22 is positioned in the injection separation cylinder 16, and the medicament of the injection separation cylinder 16 is wrapped by an isolating film 23. The cushion can extrude the medicament and guarantee closely knit degree, and the isolating film can avoid the medicament of the knockout drum of moulding plastics and the medicament contact in the gas cell simultaneously, can break through the isolating film fast again when lighting, lights the medicament in the gas cell. A plurality of supporting protrusions 24 are further provided between the filter screen 20 and the inner wall of the air-filled box 12, and the supporting protrusions 24 are installed on the inner wall of the air-filled box 12. The supporting bulge can ensure that the filter screen has enough filtering area and increase the ventilation capacity.
In addition, buffering gasbag 8 includes annular ring 25 and sets up hemispherical structure 15 in annular ring lower part, adopts this kind of structure, can make buffering gasbag can cushion the impact force in, can also support through the annular ring, and then further avoid equipment to damage.
The above description is only exemplary of the present invention and should not be construed as limiting the present invention, and any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (5)
1. Total powerstation device based on unmanned aerial vehicle, including unmanned aerial vehicle, total powerstation and unmanned aerial vehicle flight attitude control ware, its characterized in that: the unmanned aerial vehicle flight attitude control system comprises an unmanned aerial vehicle, a total station, a mounting frame, a connecting plate, a mounting box, an injection molding cover, a quick inflation assembly and a buffering air bag, wherein the mounting frame is arranged between supporting legs of the unmanned aerial vehicle, the total station is arranged at the bottom of the mounting frame, the bottom of the total station is provided with the connecting plate, the bottom of the connecting plate is connected with the mounting box through a bolt, the mounting box is provided with the injection molding cover, the mounting box is internally provided with the quick inflation assembly and the buffering air bag, the quick inflation assembly is positioned in the buffering air bag, an annular sealing seat is arranged in the mounting box, an opening of the buffering air bag is provided with an annular sealing plate, the annular sealing plate is fixed on the annular sealing seat through a screw, four supporting legs of the unmanned aerial vehicle are respectively provided with a distance sensor, and the distance sensors and the quick inflation assembly are respectively connected with an unmanned aerial vehicle flight attitude controller;
the quick inflation assembly is used for quickly inflating the buffering air bag; the distance sensor is used for detecting the distance between the unmanned aerial vehicle and the bottom surface and sending a trigger signal to the unmanned aerial vehicle flight attitude controller when the unmanned aerial vehicle falls; unmanned aerial vehicle flight attitude controller is used for detecting unmanned aerial vehicle's flight gesture to start the quick aerate subassembly when unmanned aerial vehicle falls and receives distance sensor's trigger signal.
2. The unmanned-based total station apparatus of claim 1, wherein: the quick inflation subassembly is including aerifing box, fixed lid and some firearm, it installs on the mounting box to aerify the box, it is fixed with fixed lid on the box to aerify, some firearm is installed at the center of the box of aerifing, the externally mounted of some firearm has the cylinder of moulding plastics, the both sides of the cylinder of moulding plastics are provided with the air guide hole, the both sides of the box of aerifing are provided with the venthole respectively, the both sides of the box of aerifing still are provided with the filter screen fixed slot, install the filter screen in the filter screen fixed slot, the filter screen is located the inboard of venthole, it has the medicament to fill respectively in the cavity between box of aerifing and the cylinder of moulding plastics between the cylinder of moulding plastics and the cylinder of moulding plastics.
3. The unmanned aerial vehicle-based total station apparatus of claim 2, wherein: the inflatable box is further provided with a cushion block, the cushion block is located in the injection separation cylinder, and an isolating film wraps the injection separation cylinder.
4. The unmanned aerial vehicle-based total station apparatus of claim 2, wherein: still be provided with a plurality of support archs between the filter screen and the inner wall of aerifing the box, support the arch and install on the inner wall of aerifing the box.
5. The unmanned aerial vehicle-based total station apparatus of any one of claims 1-4, wherein: the buffer air bag comprises an annular ring and a hemispherical structure arranged at the lower part of the annular ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220936244.0U CN217110943U (en) | 2022-04-22 | 2022-04-22 | Total powerstation device based on unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220936244.0U CN217110943U (en) | 2022-04-22 | 2022-04-22 | Total powerstation device based on unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217110943U true CN217110943U (en) | 2022-08-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220936244.0U Active CN217110943U (en) | 2022-04-22 | 2022-04-22 | Total powerstation device based on unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217110943U (en) |
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2022
- 2022-04-22 CN CN202220936244.0U patent/CN217110943U/en active Active
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