CN212313867U - Engineering geographic information surveys unmanned aerial vehicle - Google Patents
Engineering geographic information surveys unmanned aerial vehicle Download PDFInfo
- Publication number
- CN212313867U CN212313867U CN202020520154.4U CN202020520154U CN212313867U CN 212313867 U CN212313867 U CN 212313867U CN 202020520154 U CN202020520154 U CN 202020520154U CN 212313867 U CN212313867 U CN 212313867U
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- China
- Prior art keywords
- baffle
- air bag
- shell
- unmanned aerial
- connecting rod
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- 238000000034 method Methods 0.000 description 3
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Abstract
The utility model provides an engineering geographic information surveying unmanned aerial vehicle, which is characterized by comprising a shell, a connecting rod, a propeller, an air bag A baffle, a parachute baffle, a supporting rod, a camera, an air bag B baffle and an air bag C baffle, the upper part of the shell is of a flat-topped pyramid structure, the lower part of the shell is of an octagonal prism structure, the four sides of the pyramid structure above the shell are respectively provided with an air bag A baffle plate, the connecting rod is embedded in the groove, the tail end of the connecting rod is provided with a propeller, the round bulge is embedded into the round groove, the convex block is attached to the shell, the left side and the right side of the bottom surface of the shell are respectively provided with a support bar, the side surface of the support bar is provided with an air bag B baffle plate, an air bag B is arranged above the air bag B baffle, air bag C baffles are respectively arranged on the front side and the rear side of the bottom surface of the shell, and an air bag C is arranged above the air bag C baffles.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field especially relates to engineering geographic information surveys unmanned aerial vehicle.
Background
The unmanned aerial vehicle is a whole-course unmanned aerial vehicle, is a various remote control aircraft which does not need a driver to board and drive in a broad sense, and is generally particularly an unmanned reconnaissance aircraft of the military. The first unmanned aerial vehicle was used in the military field first, and developed gradually to civilian use later. To date, unmanned aerial vehicles have played an important role in many areas. In the aspect of engineering geography survey, the unmanned aerial vehicle has the advantages of higher visual field and lower cost, and can help the engineering team to better complete the geography survey. Because carry out the geographical survey time measuring of adverse circumstances and have various proruption situation, if the view of controlling personnel suddenly is obstructed, unmanned aerial vehicle's camera trouble etc. cause unmanned aerial vehicle to lose and control, then can cause unmanned aerial vehicle's damage, cause great loss to the enterprise, so an urgent need can implement the engineering geographical survey unmanned aerial vehicle of protection under emergency.
SUMMERY OF THE UTILITY MODEL
According to the technical problems, the utility model provides an engineering geographic information surveys unmanned aerial vehicle, which is characterized by comprising a shell, a connecting rod, a propeller, an air bag A baffle, a parachute baffle, a support rod, a camera, an air bag B baffle and an air bag C baffle, wherein the upper part of the shell is a flat-top pyramid structure, the lower part of the shell is an eight-prism structure, the four sides of the pyramid structure above the shell are respectively provided with the air bag A baffle, the lower part of the air bag A baffle is provided with the air bag A, the top surface of the pyramid structure above the shell is provided with the parachute baffle, the lower part of the parachute baffle is provided with a parachute, the inclined side surface of the eight-prism structure below the shell is provided with a groove, the upper and lower sides of the groove are provided with circular grooves, the upper and lower sides of the top end of the connecting rod are provided with circular, the screw is installed to the connecting rod end, structure as an organic whole is protruding, lug and connecting rod, the connecting rod embedding sets up inside the recess, protruding embedding circular slot, the tight shell is pasted to the lug, the left and right sides of shell bottom surface is provided with the bracing piece respectively, the side of bracing piece is provided with gasbag B baffle, the top of gasbag B baffle is provided with gasbag B, both sides are provided with gasbag C baffle respectively around the shell bottom surface, the top of gasbag C baffle is provided with gasbag C.
The utility model has the advantages that:
1. when the utility model is used, if the emergency situation is met, such as the damage of the camera of the unmanned aerial vehicle and the rapid reduction of the visual field of the unmanned aerial vehicle due to external factors, the emergency button on the remote controller can be pressed to pop out the air bag A, the air bag B and the air bag C, the utility model can slowly land, and the parachute pops out at the moment, if the utility model falls on the ground, the air bag B and the air bag C can provide buffering to protect the safety of the utility model; if the momentum is great or the gasbag B, C can bounce after falling down when the whereabouts, the utility model discloses, gasbag A, gasbag B, gasbag C protect jointly this moment the utility model discloses a safety. Do the utility model provides a good durability and protectiveness have protected the utility model discloses a complete, has more protected the utility model discloses the complete of inside data.
2. The utility model discloses during the use, if meet emergency, can make gasbag A, gasbag B, gasbag C pop out through pressing the emergency button on the remote controller, the screw slowly loses power, the utility model discloses can slow descending, the parachute pops out this moment, if the utility model discloses at the in-process of whereabouts, the cliff is touched to screw and bracing piece, and the round bulge follows the circular slot roll-off, and the inside circuit of bracing piece is pulled apart, and screw and bracing piece break away from the shell, and the parachute provides the buffering, makes the utility model discloses slowly descend. Through design round bulge and circular slot, can make screw and bracing piece break away from the shell, prevented to make the cracked condition of shell when suffering the impact owing to indelible bracing piece, increased the utility model discloses a whereabouts stability has protected the utility model discloses a complete, has more protected the utility model discloses the complete of inside data.
Drawings
Fig. 1 is a schematic front structural view of the present invention;
fig. 2 is a schematic top view of the present invention;
fig. 3 is a schematic bottom view of the present invention;
FIG. 4 is a schematic view of the unfolding structure of the air bag A, the air bag B and the air bag C of the present invention;
FIG. 5 is a schematic view of the structure of the support rod embedded in the housing of the present invention;
FIG. 6 is a schematic view of the circular groove structure of the present invention;
fig. 7 is a schematic view of the structure of the round protrusion of the present invention.
In the figure: 1-shell, 101-circular groove, 2-connecting rod, 201-circular protrusion, 202-bump, 3-propeller, 4-air bag A baffle, 401-air bag A, 5-parachute baffle, 501-parachute, 6-air bag B baffle, 601-air bag B, 7-air bag C baffle. 701-air bag C, 8-support rod, 9-camera.
Detailed Description
Example 1
The utility model provides an engineering geographic information surveys unmanned aerial vehicle, which is characterized by comprising a shell 1, a connecting rod 2, a propeller 3, an air bag A baffle 4, a parachute baffle 5, a support rod 8, a camera 9, an air bag B baffle 6 and an air bag C baffle 7, wherein the upper part of the shell 1 is of a flat-topped pyramid structure, the lower part of the shell 1 is of an eight-prism structure, the four sides of the pyramid structure above the shell 1 are respectively provided with the air bag A baffle 4, the lower part of the air bag A baffle 4 is provided with an air bag A401, the top surface of the pyramid structure above the shell 1 is provided with the parachute baffle 5, the lower part of the parachute baffle 5 is provided with a parachute 501, the inclined side surface of the eight-prism structure below the shell 1 is provided with a groove, the upper and lower sides of the groove are provided with circular grooves 101, the upper and lower sides of the, the left front side and the left back side of connecting rod 2 are provided with lug 202 respectively, protruding 201, lug 202 and connecting rod 2 structure as an organic whole, the embedding of connecting rod 2 sets up inside the recess, protruding 201 embedding circular slot 101, lug 202 pastes tight shell 1, the left and right sides of shell 1 bottom surface is provided with bracing piece 8 respectively, the side of bracing piece 8 is provided with gasbag B baffle 6, the top of gasbag B baffle 6 is provided with gasbag B601, both sides are provided with gasbag C baffle 7 respectively around the shell 1 bottom surface, the top of gasbag C baffle 7 is provided with gasbag C701.
Example 2
When the utility model is used, if the emergency situation occurs, the air bag A401, the air bag B601 and the air bag C701 can be popped out by pressing the emergency button on the remote controller, the propeller 3 slowly loses power, the utility model can slowly land, the parachute 501 pops out at the moment, if the utility model falls on the ground, the air bag B601 and the air bag C701 can provide buffer to protect the safety of the utility model; if the momentum is large when falling or the airbag B601 and the airbag C701 roll after falling, the airbag B601 and the airbag C701 can bounce, and the airbag A401, the airbag B601 and the airbag C701 protect the safety of the utility model together; if the utility model discloses at the in-process of whereabouts, screw 3 and bracing piece 8 touch the cliff, and protruding 201 slips out from circular slot 101, and the inside circuit of bracing piece 8 is pulled apart, and screw 3 and bracing piece 8 break away from shell 1, and parachute 501 provides the buffering, makes the utility model discloses slowly descend.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. The utility model discloses each part that mentions is the common technique in prior art, and the technical personnel of this trade should understand, the utility model discloses do not receive the restriction of above-mentioned embodiment, the description only is the explanation in above-mentioned embodiment and the description the principle of the utility model, under the prerequisite that does not deviate from the spirit and the scope of the utility model, the utility model discloses still can have various changes and improvement, these changes and improvement all fall into the protection of claim the utility model is within the scope. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. Engineering geographic information surveys unmanned aerial vehicle, its characterized in that includes shell, connecting rod, screw, gasbag A baffle, parachute baffle, bracing piece, camera, gasbag B baffle, gasbag C baffle, the top of shell is the pyramid structure of flat top, the below of shell is eight prismatic structure, the four sides of pyramid structure above the shell are provided with gasbag A baffle respectively, the below of gasbag A baffle is provided with gasbag A, the top surface of pyramid structure above the shell is provided with the parachute baffle, parachute baffle below is provided with, the oblique side of eight prismatic structure below the shell is seted up flutedly, the upper and lower both sides of recess are seted up the circular slot, the upper and lower both sides of connecting rod top are provided with the dome, the screw is installed to the connecting rod end, the left front and back both sides of connecting rod are provided with the lug respectively, the round convex, the convex block and the connecting rod are of an integrated structure, the connecting rod is embedded into the groove, the round convex is embedded into the round groove, the convex block is attached to the shell tightly, the left side and the right side of the bottom surface of the shell are provided with the supporting rods respectively, the side faces of the supporting rods are provided with the air bag B baffle, the air bag B is arranged above the air bag B baffle, the air bag C baffle is arranged on the front side and the rear side of the bottom surface of the shell respectively, and the air bag C is arranged above the air bag C baffle.
2. The unmanned aerial vehicle for engineering geographic information survey of claim 1, wherein the lines inside the support rods pass through the support rods to be connected with the lines inside the housing.
3. The drone of claim 1, wherein the circuitry inside the support rod is independent of the circuitry inside the housing.
4. The unmanned aerial vehicle for engineering geographic information survey of claim 1, wherein the propeller, the trigger device of air bag a, the trigger device of air bag B, the trigger device of air bag C, and the trigger device of parachute are connected by an internal circuit.
5. The unmanned aerial vehicle for engineering geographic information survey of claim 1, wherein an emergency button is provided on the unmanned aerial vehicle remote control.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020520154.4U CN212313867U (en) | 2020-04-10 | 2020-04-10 | Engineering geographic information surveys unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020520154.4U CN212313867U (en) | 2020-04-10 | 2020-04-10 | Engineering geographic information surveys unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212313867U true CN212313867U (en) | 2021-01-08 |
Family
ID=74020592
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020520154.4U Expired - Fee Related CN212313867U (en) | 2020-04-10 | 2020-04-10 | Engineering geographic information surveys unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212313867U (en) |
-
2020
- 2020-04-10 CN CN202020520154.4U patent/CN212313867U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210108 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |