CN212872890U - Unmanned aerial vehicle machine carries ground penetrating radar device - Google Patents
Unmanned aerial vehicle machine carries ground penetrating radar device Download PDFInfo
- Publication number
- CN212872890U CN212872890U CN202021478977.1U CN202021478977U CN212872890U CN 212872890 U CN212872890 U CN 212872890U CN 202021478977 U CN202021478977 U CN 202021478977U CN 212872890 U CN212872890 U CN 212872890U
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- ground penetrating
- hanging
- penetrating radar
- radar
- unmanned aerial
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- 230000000149 penetrating effect Effects 0.000 title claims abstract description 55
- 238000009434 installation Methods 0.000 claims abstract description 18
- 238000003466 welding Methods 0.000 claims description 24
- 230000003139 buffering effect Effects 0.000 claims description 17
- 230000003014 reinforcing effect Effects 0.000 claims description 8
- 238000001514 detection method Methods 0.000 abstract description 9
- 230000000694 effects Effects 0.000 abstract description 5
- 239000011435 rock Substances 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 230000005489 elastic deformation Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- Radar Systems Or Details Thereof (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle carries ground penetrating radar device, including installation roof, installation otic placode, hitching component, alignment jig, regulation spout, radar box, fastening chassis, ground penetrating radar body, fastening component and radome, two regulation spouts have been seted up to the top terminal surface opposite side of installation roof, and the top of adjusting the spout is installed and is adjusted the frame, two pairs of installation otic placodes are all installed through welded fastening in the top of frame and the top terminal surface both sides of installation roof, and be provided with the hitching component between each pair of installation otic placode, the bottom terminal surface of installation roof has the radar box through welded fastening, the inboard top of radar box has the fastening chassis through bolt fixed mounting, this unmanned aerial vehicle carries ground penetrating radar device, and the installation is simple and convenient, and fixed effect is firm, when using, has good structural stability, the sway of the ground penetrating radar body can be effectively reduced, and the detection precision can be improved.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle equipment field specifically is an unmanned aerial vehicle machine carries ground penetrating radar device.
Background
In recent years, unmanned aerial vehicles have met the needs for detection and ranging in the fields of industry, shipping, air transportation, and the like, and have achieved wide application in these fields and industries. In order to better meet the detection and ranging requirements in the field or the detection and ranging requirements in other forms, the application range of the airborne radar of the unmanned aerial vehicle is generally greatly enlarged, so that the demand for the airborne radar is increased rapidly; unmanned aerial vehicle machine carries ground penetrating radar device among the prior art, when the installation, the installation is dismantled inconveniently, moreover, overall structure fastness is not good to it is great to lead to equipment to rock, influences the detection precision of equipment easily, consequently, designs an unmanned aerial vehicle machine and carries ground penetrating radar device and is very necessary.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle machine carries ground penetrating radar device, it is simple convenient to install, and fixed effect is firm, when using, has good structural stability, can effectively reduce rocking of ground penetrating radar body, is favorable to improving the detection precision.
The purpose of the utility model can be realized by the following technical scheme:
an airborne ground penetrating radar device of an unmanned aerial vehicle comprises a mounting top plate, a mounting ear plate, a hanging component, an adjusting bracket, adjusting chutes, a radar box, a fastening underframe, a ground penetrating radar body, a fastening component and a radar cover, wherein the other side of the top end surface of the mounting top plate is provided with two adjusting chutes, and the top of the adjusting chute is provided with an adjusting frame, the top of the adjusting frame and the two sides of the top end surface of the mounting top plate are fixedly provided with two pairs of mounting ear plates by welding, and a hanging component is arranged between each pair of mounting ear plates, the bottom end surface of the mounting top plate is fixedly provided with a radar box by welding, the top of the inner side of the radar box is fixedly provided with a fastening underframe through a bolt, the bottom of the fastening underframe is connected with a ground penetrating radar body, a fastening component is arranged on the outer side of the ground penetrating radar body, and a radar cover is fixedly arranged on the bottom end face of the radar box;
articulate the subassembly and include jib, articulate seat, first articulate groove, locking double-screw bolt, upset seat, second articulate groove and trip shaft, the jib is pegged graft and is installed between the installation otic placode, the top one end of jib is installed the articulate seat through welded fastening, the first groove of articulating has been seted up to the top terminal surface of articulate seat, one side of articulate seat is provided with the upset seat, the second articulates the groove has been seted up to the terminal surface of upset seat, the one end of upset seat is provided with the trip shaft, and the trip shaft grafting is installed in the inside both sides of articulate seat, the locking screw has all been seted up to the terminal surface both sides of articulate seat and the terminal surface both sides of upset seat, two locking double-screw bolts are installed in the terminal surface outside grafting of articulate seat, and the locking screw that the one end of locking double-screw bolt passed the articulate seat terminal surface passes through the screw fastening connection with the locking screw of upset seat terminal surface.
As a further aspect of the present invention: the bottom end face both sides of alignment jig all install adjusting block through welded fastening, and adjusting block pegs graft and installs the inside at adjusting the spout.
As a further aspect of the present invention: the adjusting frame is characterized in that positioning screw holes are formed in the end faces of the two sides of the adjusting frame, positioning screws are installed on one sides of the positioning screw holes through threaded connection, and one ends of the positioning screws penetrate through the positioning screw holes to be tightly connected with the end faces of the installation top plate.
As a further aspect of the present invention: the rotation through-hole has all been seted up to the terminal surface central authorities of installation otic placode and the bottom one end of jib, it installs the rotation bolt to rotate the interpolation of through-hole.
As a further aspect of the present invention: fastening components includes fixed frame, welding sill bar, buffering frame, limiting plate, buffering push rod and buffer spring, fixed frame has the outer wall of ground penetrating radar body all around through bolt fixed mounting, fixed frame's outer wall all installs the welding sill bar through welded fastening all around, and the other end of welding sill bar and the inner wall fixed connection of radar box, the buffering frame passes through welded fastening and installs inner wall one side at the radar box, the terminal surface of buffering frame has the limiting plate through welded fastening, the buffering push rod is installed in pegging graft of the terminal surface central authorities of limiting plate, and the other end of buffering push rod and the outer wall fixed connection of ground penetrating radar body, the buffer spring is installed in the outside cup jointing of buffering push rod, and buffer spring's both ends respectively with the outer wall fixed connection of limiting plate and ground penetrating radar body.
As a further aspect of the present invention: strengthening grooves are formed in two sides of the end face of the radar box, and strengthening plates are fixedly mounted inside the strengthening grooves.
The utility model has the advantages that: when the airborne ground penetrating radar device of the unmanned aerial vehicle is installed, the device can be hung and installed at the bottom of the unmanned aerial vehicle through the hanging component, the installation is simple and convenient, the fixing effect is firm, the disassembly is convenient, and the convenience in installation is improved; when the ground penetrating radar fixing device is used, ground penetrating detection is carried out through the ground penetrating radar body, good structural stability is achieved through the fastening assembly, shaking of the ground penetrating radar body can be effectively reduced, and detection precision is improved.
Drawings
In order to facilitate understanding for those skilled in the art, the present invention will be further described with reference to the accompanying drawings.
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic structural view of the hitch assembly of the present invention;
FIG. 3 is a cross-sectional view of the radar box of the present invention;
in the figure: 1. installing a top plate; 2. mounting an ear plate; 3. a hitch assembly; 4. an adjusting bracket; 5. adjusting the sliding chute; 6. a radar box; 7. fastening the underframe; 8. a ground penetrating radar body; 9. a fastening assembly; 10. a reinforcing plate; 11. A radome; 31. a boom; 32. a hanging seat; 33. a first hooking groove; 34. locking the stud; 35. a turning seat; 36. a second hanging groove; 37. a turning shaft; 91. a fixed frame; 92. welding a bottom rod; 93. a buffer frame; 94. a limiting plate; 95. a buffer push rod; 96. a buffer spring.
Detailed Description
The technical solution of the present invention will be described clearly and completely with reference to the following embodiments, and it should be understood that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
As shown in fig. 1-3, an airborne ground penetrating radar device of an unmanned aerial vehicle comprises a mounting top plate 1, a mounting ear plate 2, a hanging component 3, an adjusting frame 4, adjusting chutes 5, a radar box 6, a fastening underframe 7, a ground penetrating radar body 8, a fastening component 9 and a radar cover 11, wherein two adjusting chutes 5 are formed in the other side of the top end surface of the mounting top plate 1, the adjusting frame 4 is installed at the top of each adjusting chute 5, adjusting sliders are fixedly installed on two sides of the bottom end surface of each adjusting frame 4 through welding, and the adjusting sliders are installed in the adjusting chutes 5 in an inserted manner so as to facilitate movement of the adjusting frames 4; positioning screw holes are formed in the end faces of the two sides of the adjusting frame 4, positioning screws are installed on one sides of the positioning screw holes in a threaded connection mode, and one ends of the positioning screws penetrate through the positioning screw holes to be tightly connected with the end face of the installing top plate 1, so that the adjusting frame 4 can be fixed conveniently; two pairs of mounting lug plates 2 are fixedly mounted on the top of the adjusting frame 4 and two sides of the end surface of the top of the mounting top plate 1 through welding, a hanging component 3 is arranged between each pair of mounting lug plates 2, the hanging component 3 comprises a hanging rod 31, a hanging seat 32, a first hanging groove 33, a locking stud 34, a turning seat 35, a second hanging groove 36 and a turning shaft 37, the hanging rod 31 is installed between the mounting lug plates 2 in a plugging mode, a rotating through hole is formed in the center of the end surface of each mounting lug plate 2 and one end of the bottom of the hanging rod 31, and a rotating bolt is installed in the rotating through hole in a plugging mode, so that the position of the hanging rod 31 is fixed; a hanging seat 32 is fixedly installed at one end of the top of the hanging rod 31 through welding, a first hanging groove 33 is formed in the end face of the top of the hanging seat 32, an overturning seat 35 is arranged on one side of the hanging seat 32, a second hanging groove 36 is formed in the end face of the overturning seat 35, an overturning shaft 37 is arranged at one end of the overturning seat 35, the overturning shaft 37 is installed on two inner sides of the hanging seat 32 in an inserting mode, locking screw holes are formed in two sides of the end face of the hanging seat 32 and two sides of the end face of the overturning seat 35 respectively, two locking studs 34 are installed on the outer side of the end face of the hanging seat 32 in an inserting mode, and one end of each locking stud 34 penetrates through the locking screw hole in the end face of the hanging seat 32; the bottom end face of the installation top plate 1 is fixedly provided with a radar box 6 through welding, the top of the inner side of the radar box 6 is fixedly provided with a fastening underframe 7 through bolts, the bottom of the fastening underframe 7 is connected with a ground penetrating radar body 8, the outer side of the ground penetrating radar body 8 is provided with a fastening assembly 9, the fastening assembly 9 comprises a fixed frame 91, a welding bottom rod 92, a buffer frame 93, a limiting plate 94, a buffer push rod 95 and a buffer spring 96, the fixed frame 91 is fixedly provided with the periphery of the outer wall of the ground penetrating radar body 8 through bolts, the periphery of the outer wall of the fixed frame 91 is fixedly provided with the welding bottom rod 92 through welding, the other end of the welding bottom rod 92 is fixedly connected with the inner wall of the radar box 6, the buffer frame 93 is fixedly arranged on one side of the inner wall of the radar box 6 through welding, the limiting plate 94 is fixedly provided on the end face of, the other end of the buffer push rod 95 is fixedly connected with the outer wall of the ground penetrating radar body 8, a buffer spring 96 is sleeved on the outer side of the buffer push rod 95, and two ends of the buffer spring 96 are respectively fixedly connected with the limiting plate 94 and the outer wall of the ground penetrating radar body 8, so that the ground penetrating radar body 8 can be fixed, and the buffer effect is also achieved; reinforcing grooves are formed in the two sides of the end face of the radar box 6, and reinforcing plates 10 are fixedly arranged in the reinforcing grooves, so that the structural strength of the radar box 6 is improved; the bottom end face of the radar box 6 is fixedly provided with a radar cover 11.
The utility model discloses a theory of operation: when in use, the hanging component 3 is arranged at the top of the mounting top plate 1 and inside the mounting ear plate 2 at the top of the adjusting frame 4, the rotating through hole at the bottom of the suspender 31 is aligned with the rotating through hole at the end surface of the mounting ear plate 2, then a rotating bolt is used for penetrating through the rotating through hole, so that the suspender 31 is fixedly arranged between the mounting ear plates 2, the hanging component 3 at the top of the mounting top plate 1 is connected with the machine rod at one side of the bottom of the unmanned aerial vehicle frame, the first hanging groove 33 of the hanging seat 32 is positioned at one side of the machine rod, the overturning shaft 37 rotates inside the suspender 31, so that the overturning seat 35 rotates, the second hanging groove 36 is connected with the hanging seat 32 in a clamping way, then a locking stud 34 is used for penetrating through the locking screw hole of the hanging seat 32 to be in threaded fastening connection with the locking screw hole at the end surface of the overturning seat 35, after the two hanging components 3 at, the adjusting frame 4 is pushed, the adjusting frame 4 slides in the adjusting sliding groove 5 through the adjusting slide block, the hanging component 3 at the top of the adjusting frame 4 can move to the position of the machine rod on the other side of the bottom of the unmanned aerial vehicle frame, the positioning screw is screwed down, the positioning screw penetrates through the positioning screw hole to be tightly connected with the outer wall of the mounting top plate 1, so that the position of the adjusting frame 4 is fixed, then the two hanging components 3 at the top of the adjusting frame 4 are fixed with the machine rod, when the unmanned aerial vehicle takes off, the mounting top plate 1 and the radar box 6 can be hung up through the hanging components 3, the ground penetrating radar body 8 at the bottom of the fastening bottom frame 7 works, detection can be carried out through the radar cover 11, because the ground penetrating radar body 8 is mounted inside the radar box 6 through the fastening component 9, good mounting stability can be achieved on the ground penetrating radar body 8 through the fixing frame, when ground penetrating radar body 8 produces and rocks, in one side of ground penetrating radar body 8, the outer wall of ground penetrating radar body 8 can promote buffering push rod 95 and remove, under the effect of limiting plate 94 of buffering frame 93 terminal surface, can cause the extrusion to buffer spring 96, at the opposite side of ground penetrating radar body 8, ground penetrating radar body 8 can stimulate buffer spring 96, make buffer spring 96 take place to warp, elastic deformation through buffer spring 96, thereby reduce and rock, make ground penetrating radar body 8 can be stable, reinforcing plate 10 can improve the anti intensity of falling of radar case 6.
The preferred embodiments of the present invention disclosed above are intended only to help illustrate the present invention. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical applications, to thereby enable others skilled in the art to best understand the invention for and utilize the invention. The present invention is limited only by the claims and their full scope and equivalents.
Claims (6)
1. An airborne ground penetrating radar device of an unmanned aerial vehicle is characterized by comprising a mounting top plate (1), mounting ear plates (2), a hanging component (3), an adjusting frame (4), adjusting chutes (5), a radar box (6), a fastening underframe (7), a ground penetrating radar body (8), a fastening component (9) and a radar cover (11), wherein two adjusting chutes (5) are formed in the other side of the top end surface of the mounting top plate (1), the adjusting frame (4) is installed at the top of each adjusting chute (5), two pairs of mounting ear plates (2) are fixedly installed at the top of each adjusting frame (4) and the two sides of the top end surface of the mounting top plate (1) through welding, the hanging component (3) is arranged between every pair of mounting ear plates (2), the radar box (6) is installed at the bottom end surface of the mounting top plate (1) through welding, the fastening underframe (7) is fixedly installed at the top of the inner side of the radar box (6) through bolts, the bottom of the fastening underframe (7) is connected with a ground penetrating radar body (8), a fastening component (9) is arranged on the outer side of the ground penetrating radar body (8), and a radar cover (11) is fixedly arranged on the bottom end face of the radar box (6);
the hanging connection assembly (3) comprises a hanging rod (31), hanging seats (32), a first hanging groove (33), a locking stud (34), a turning seat (35), a second hanging groove (36) and a turning shaft (37), the hanging rod (31) is installed between the installation lug plates (2) in a plugging mode, the hanging seats (32) are fixedly installed at one end of the top of the hanging rod (31) through welding, the first hanging groove (33) is formed in the end face of the top of the hanging seats (32), the turning seat (35) is arranged on one side of the hanging seats (32), the second hanging groove (36) is formed in the end face of the turning seat (35), the turning shaft (37) is arranged at one end of the turning seat (35), the turning shaft (37) is installed on two sides of the inside of the hanging seats (32) in a plugging mode, locking screw holes are formed in two sides of the end faces of the hanging seats (32) and two sides of the end faces of the turning seats (35), two locking studs (34) are inserted and installed on the outer side of the end face of the hanging seat (32), and one ends of the locking studs (34) penetrate through locking screw holes in the end face of the hanging seat (32) and are fixedly connected with locking screw holes in the end face of the overturning seat (35) through threads.
2. The airborne ground penetrating radar device of the unmanned aerial vehicle of claim 1, wherein two sides of the bottom end surface of the adjusting frame (4) are fixedly provided with adjusting sliding blocks through welding, and the adjusting sliding blocks are inserted and installed inside the adjusting sliding grooves (5).
3. The airborne ground penetrating radar device of unmanned aerial vehicle of claim 1, wherein the both sides terminal surface of alignment jig (4) has all seted up the location screw, the one side of location screw is installed set screw through threaded connection, and set screw's one end passes the terminal surface top tight connection of location screw and installation roof (1).
4. The airborne ground penetrating radar device of unmanned aerial vehicle of claim 1, wherein the center of the end face of the mounting ear plate (2) and one end of the bottom of the hanger rod (31) are both provided with a rotating through hole, and a rotating bolt is inserted and installed in the rotating through hole.
5. The airborne ground penetrating radar device of the unmanned aerial vehicle of claim 1, wherein the fastening assembly (9) comprises a fixed frame (91), a welding bottom rod (92), a buffering frame (93), a limiting plate (94), a buffering push rod (95) and a buffering spring (96), the fixed frame (91) is fixedly installed around the outer wall of the ground penetrating radar body (8) through bolts, the welding bottom rod (92) is fixedly installed around the outer wall of the fixed frame (91) through welding, the other end of the welding bottom rod (92) is fixedly connected with the inner wall of the radar box (6), the buffering frame (93) is fixedly installed on one side of the inner wall of the radar box (6) through welding, the limiting plate (94) is fixedly installed on the end face of the buffering frame (93), the buffering push rod (95) is installed in the center of the end face of the limiting plate (94) in an inserting manner, and the other end of buffering push rod (95) and the outer wall fixed connection of ground penetrating radar body (8), buffer spring (96) are installed in the outside cup joint of buffering push rod (95), and the both ends of buffer spring (96) respectively with the outer wall fixed connection of limiting plate (94) and ground penetrating radar body (8).
6. The airborne ground penetrating radar device of the unmanned aerial vehicle of claim 1, wherein reinforcing grooves are formed in two sides of the end surface of the radar box (6), and reinforcing plates (10) are fixedly mounted inside the reinforcing grooves.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021478977.1U CN212872890U (en) | 2020-07-24 | 2020-07-24 | Unmanned aerial vehicle machine carries ground penetrating radar device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021478977.1U CN212872890U (en) | 2020-07-24 | 2020-07-24 | Unmanned aerial vehicle machine carries ground penetrating radar device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212872890U true CN212872890U (en) | 2021-04-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021478977.1U Expired - Fee Related CN212872890U (en) | 2020-07-24 | 2020-07-24 | Unmanned aerial vehicle machine carries ground penetrating radar device |
Country Status (1)
| Country | Link |
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| CN (1) | CN212872890U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113978374A (en) * | 2021-10-19 | 2022-01-28 | 华南农业大学 | Buffering connecting device based on all-terrain vehicle and ground penetrating radar instrument detection |
-
2020
- 2020-07-24 CN CN202021478977.1U patent/CN212872890U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113978374A (en) * | 2021-10-19 | 2022-01-28 | 华南农业大学 | Buffering connecting device based on all-terrain vehicle and ground penetrating radar instrument detection |
| CN113978374B (en) * | 2021-10-19 | 2023-08-04 | 华南农业大学 | Buffering connecting device based on all-terrain vehicle and ground penetrating radar instrument detection |
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| GR01 | Patent grant | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210402 |