CN214649093U - Unmanned aerial vehicle aerial survey of stable installation is with hanging cabin structure - Google Patents

Unmanned aerial vehicle aerial survey of stable installation is with hanging cabin structure Download PDF

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Publication number
CN214649093U
CN214649093U CN202120922572.0U CN202120922572U CN214649093U CN 214649093 U CN214649093 U CN 214649093U CN 202120922572 U CN202120922572 U CN 202120922572U CN 214649093 U CN214649093 U CN 214649093U
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mounting bracket
block
unmanned aerial
aerial vehicle
lifter
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曹俊
杨昕
庄国钦
刘世霄
李阳
周传海
韩亚臣
罗建军
梁智勇
吴卓霖
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Liuzhou Xuntian Technology Development Co ltd
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Liuzhou Xuntian Technology Development Co ltd
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Abstract

The utility model discloses an unmanned aerial vehicle for aerial survey nacelle structure of stable installation, including mounting bracket, fixed establishment and adjustment mechanism, sealing mechanism is installed to the mounting bracket top, fixed establishment all installs in the mounting bracket both sides, adjustment mechanism installs in the mounting bracket below, the support has all been welded to adjustment mechanism below both sides, damper is installed to the support below, the third connecting block is installed to the damper below. This unmanned aerial vehicle for aerial survey of stable installation hangs cabin structure, through being provided with the lifter, spacing hole, gag lever post and fixing bolt, the pulling lifter makes the lifter at the inside both sides round trip movement of mounting bracket to suitable position, push into spacing downthehole portion with the gag lever post again, then fix in unmanned aerial vehicle one side with fixing bolt screws up the lifter, can be convenient for carry out fixed mounting to the mounting bracket of device more, the lifter can be convenient for adjust the size of mounting bracket more, so that adapt to the unmanned aerial vehicle of different models.

Description

Unmanned aerial vehicle aerial survey of stable installation is with hanging cabin structure
Technical Field
The utility model relates to an unmanned aerial vehicle air survey correlation technique field specifically is an unmanned aerial vehicle air survey of stable installation is with hanging cabin structure.
Background
Unmanned aerial vehicle aerial survey is the powerful supplement of traditional aerial photogrammetry means, have flexible, high-efficient quick, meticulous accuracy, the operating cost is low, application scope is wide, characteristics such as production cycle is short, have obvious advantage in the aspect of the quick acquisition of small region and flight difficulty area high resolution image, along with the development of unmanned aerial vehicle and digital camera technique, digital aerial photography technique based on unmanned aerial vehicle platform has shown its unique advantage, unmanned aerial vehicle need use nacelle structure in the aerial survey process, it is fixed to install the camera, but the nacelle structure that uses at present, can't more stable installation usually when using, take place to shake when unmanned aerial vehicle and make and lead to nacelle structure to take place to rock, influence the effect of aerial survey, thereby greatly reduced the device's result of use.
But nacelle structure that uses at present often can't be more stable when using installs, takes place to shake when unmanned aerial vehicle and makes and lead to nacelle structure to take place to rock, influences the effect of aerial survey to greatly reduced the device's result of use.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle nacelle structure for aerial survey of stable installation to what provide in solving above-mentioned background art generally can't more stable install when using, take place to shake when unmanned aerial vehicle and make and can lead to the nacelle structure to take place to rock, influence the effect of aerial survey, thereby greatly reduced the device's result of use problem.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle aerial survey of stable installation is with hanging cabin structure, includes mounting bracket, fixed establishment and adjustment mechanism, sealing mechanism is installed to the mounting bracket top, fixed establishment all installs in the mounting bracket both sides, adjustment mechanism installs in the mounting bracket below, the support has all been welded to adjustment mechanism below both sides, damper is installed to the support below, the third connecting block is installed to the damper below, the electronic rotatory piece of second is installed to third connecting block inboard, the electronic rotatory piece inboard installation organism of second, the camera lens is installed to the organism inboard, camera lens surface mounting has clearance mechanism.
Preferably, sealing mechanism includes wiring mouth, movable block, movable hook and sealing washer, the wiring mouth is seted up in mounting bracket one side, the movable block has all been welded to wiring mouth outer wall both sides, assorted movable hook is installed with it to the movable block inboard, the sealing washer is installed to movable hook one side.
Preferably, the fixing mechanism comprises a lifting rod, a limiting hole, a limiting rod and a fixing bolt, the lifting rod is installed on two sides of the inner wall of the installation frame, the limiting hole is formed in one side of the lifting rod, the limiting rod is installed on the inner side of the limiting hole, and the fixing bolt penetrates through one side of the lifting rod.
Preferably, adjustment mechanism includes electric lift loop bar, first connecting block, draw-in groove, fixture block, second connecting block and the rotatory piece of first electronic, the electric lift loop bar is installed in the mounting bracket below, the welding of electric lift loop bar below has first connecting block, the draw-in groove has been seted up to first connecting block one side, assorted fixture block with it is installed to the draw-in groove inboard, the welding of fixture block one side has the second connecting block, first electronic rotatory piece is installed to second connecting block one side.
Preferably, damper includes telescopic sleeve, fixed block, expanding spring and mount, telescopic sleeve welds in support below both sides, telescopic sleeve inner weld has the fixed block, the welding of fixed block one side has expanding spring, the welding of expanding spring one side has the mount.
Preferably, the second electric rotating blocks are symmetrically distributed on the central axis of the machine body.
Preferably, clearance mechanism includes the electronic rotatory piece of third, clearance scraper blade, slider and slide rail, the electronic rotatory piece of third is installed in camera lens outer wall one side, the clearance scraper blade is installed to the electronic rotatory piece one side of third, the welding of clearance scraper blade one side has the slider, the slider is installed at the slide rail inboardly, the slide rail is installed in camera lens one side.
Compared with the prior art, the beneficial effects of the utility model are that: the hanging cabin structure for the aerial survey of the stably installed unmanned aerial vehicle pulls the lifting rod to enable the lifting rod to move back and forth to a proper position on two sides in the mounting rack by arranging the lifting rod, the limiting hole, the limiting rod and the fixing bolt, then the limiting rod is pushed into the limiting hole, then the lifting rod is screwed and fixed on one side of the unmanned aerial vehicle by a fixing bolt, so that the mounting frame of the device can be more conveniently fixed and installed, the size of the mounting frame can be more conveniently adjusted by the lifting rod, so as to be convenient for adapting to unmanned aerial vehicles of different models, meanwhile, when the unmanned aerial vehicle shakes, the fixing frame drives the telescopic spring to move up and down in the telescopic sleeve, thereby make expanding spring drive organism reciprocate, can be convenient for more stabilize the shock attenuation to the organism, avoid the organism to rock and exert an influence to the picture of aerial survey, make the use of device more stable to the effectual result of use that has promoted the device.
Drawings
Fig. 1 is a schematic view of the front cross-sectional structure of the present invention;
FIG. 2 is a schematic view of the front view of the present invention;
FIG. 3 is a schematic view of the structure of the third electric rotating block and the cleaning scraper of the present invention;
fig. 4 is the structural schematic diagram of the utility model with the mutually matched mounting rack and the lifting rod.
In the figure: 1. a mounting frame; 2. a sealing mechanism; 201. a wiring port; 202. a movable block; 203. a movable hook; 204. a seal ring; 3. a fixing mechanism; 301. a lifting rod; 302. a limiting hole; 303. a limiting rod; 304. fixing the bolt; 4. an adjustment mechanism; 401. an electric lifting loop bar; 402. a first connection block; 403. A card slot; 404. a clamping block; 405. a second connecting block; 406. a first motorized rotating block; 5. a support; 6. A damping mechanism; 601. a telescopic sleeve; 602. a fixed block; 603. a tension spring; 604. a fixed mount; 7. A third connecting block; 8. a second electric rotating block; 9. a body; 10. a lens; 11. a cleaning mechanism; 1101. A third electric rotating block; 1102. cleaning a scraper; 1103. a slider; 1104. a slide rail.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle nacelle structure for aerial survey of stable installation, including mounting bracket 1, fixed establishment 3 and adjustment mechanism 4, sealing mechanism 2 is installed to 1 top of mounting bracket, fixed establishment 3 all installs in 1 both sides of mounting bracket, adjustment mechanism 4 installs in 1 below of mounting bracket, support 5 has all been welded to 4 below both sides of adjustment mechanism, damper 6 is installed to support 5 below, third connecting block 7 is installed to damper 6 below, the electronic rotatory piece 8 of second is installed to 7 inboard of third connecting block, organism 9 is installed to the electronic rotatory piece 8 inboard of second, camera lens 10 is installed to organism 9 inboard, camera lens 10 surface mounting has clearance mechanism 11.
Further, sealing mechanism 2 includes wiring mouth 201, movable block 202, activity hook 203 and sealing washer 204, wiring mouth 201 is seted up in mounting bracket 1 one side, all welded in wiring mouth 201 outer wall both sides has movable block 202, assorted activity hook 203 with it is installed to movable block 202 inboard, sealing washer 204 is installed to activity hook 203 one side, through being provided with wiring mouth 201, movable block 202, activity hook 203 and sealing washer 204, can be convenient for more seal the wiring mouth 201 of device, prevent that there is moisture to get into inside wiring mouth 201 when using, lead to organism 9's short circuit, influence subsequent use.
Further, fixed establishment 3 includes lifter 301, spacing hole 302, gag lever post 303 and fixing bolt 304, lifter 301 installs in 1 inner wall both sides of mounting bracket, spacing hole 302 has been seted up to lifter 301 one side, gag lever post 303 is installed to spacing hole 302 inboard, fixing bolt 304 all runs through in lifter 301 one side, through being provided with lifter 301, spacing hole 302, gag lever post 303 and fixing bolt 304, can be convenient for carry out fixed mounting to the mounting bracket 1 of device more, lifter 301 can be convenient for adjust the size of mounting bracket 1 more, so that adapt to the unmanned aerial vehicle of different models.
Further, adjustment mechanism 4 includes electric lift loop bar 401, first connecting block 402, draw-in groove 403, fixture block 404, second connecting block 405 and first electric rotating block 406, electric lift loop bar 401 is installed in mounting bracket 1 below, the welding of electric lift loop bar 401 below has first connecting block 402, draw-in groove 403 has been seted up to first connecting block 402 one side, assorted fixture block 404 is installed to draw-in groove 403 inboard, the welding of fixture block 404 one side has second connecting block 405, first electric rotating block 406 is installed to second connecting block 405 one side, through being provided with electric lift loop bar 401, first connecting block 402, draw-in groove 403, fixture block 404, second connecting block 405 and first electric rotating block 406, can be convenient for carry out the regulation of upper and lower position and left and right angle to the organism 9 of device more, make the shooting scope of organism 9 wider, use more intelligence.
Further, damper 6 includes telescopic sleeve 601, fixed block 602, expanding spring 603 and mount 604, telescopic sleeve 601 welds in support 5 below both sides, telescopic sleeve 601 internal weld has fixed block 602, fixed block 602 one side welding has expanding spring 603, expanding spring 603 one side welding has mount 604, through being provided with telescopic sleeve 601, fixed block 602, expanding spring 603 and mount 604, can be convenient for stabilize the shock attenuation to organism 9 more, avoid organism 9 to rock and produce the influence to the picture of aerial survey, make the use of device more stable, thereby the effectual result of use that has promoted the device.
Further, the second electric rotating block 8 is symmetrically distributed along the axis of the machine body 9, the second electric rotating block 8 can adjust the upper and lower angles of the machine body 9, and the third connecting block 7 and the second electric rotating block 8 are arranged, so that the machine body 9 of the device can be adjusted in the upper and lower angles, the shooting range of the machine body 9 is wider, no dead angle exists, and the use is more convenient.
Further, the cleaning mechanism 11 includes a third electric rotating block 1101, a cleaning scraper 1102, a slider 1103 and a sliding rail 1104, the third electric rotating block 1101 is installed on one side of the outer wall of the lens 10, the cleaning scraper 1102 is installed on one side of the third electric rotating block 1101, the slider 1103 is welded on one side of the cleaning scraper 1102, the slider 1103 is installed on the inner side of the sliding rail 1104, the sliding rail 1104 is installed on one side of the lens 10, through the third electric rotating block 1101, the cleaning scraper 1102, the slider 1103 and the sliding rail 1104, dust or water stains on the surface of the lens 10 can be cleaned in time in the using process, the shooting definition is prevented from being influenced, and meanwhile, the slider 1103 and the sliding rail 1104 are arranged, so that the cleaning scraper 1102 is more stable.
The working principle is as follows: firstly, an external power supply is switched on, the sealing ring 204 is pushed to drive the sealing ring 204 to drive the movable hook 203 to be fixedly connected with the movable block 202, so that the sealing ring 204 is fixed above the wiring port 201, then the lifting rod 301 is pulled to make the lifting rod 301 move back and forth to a proper position at two sides in the mounting rack 1, then the limiting rod 303 is pushed into the limiting hole 302, then the electric lifting loop bar 401 is opened to make the electric lifting loop bar 401 drive the machine body 9 to move up and down, then the second electric rotating block 8 is opened to make the first electric rotating block 406 drive the machine body 9 to move back and forth, when the unmanned aerial vehicle shakes, the fixing rack 604 drives the telescopic spring 603 to move up and down in the telescopic sleeve 601, so that the telescopic spring 603 drives the machine body 9 to move up and down, so that the machine body 9 can be more conveniently and stably damped, and when the unmanned aerial vehicle is used, the second electric rotating block 8 is opened to make the second electric rotating block 8 drive the machine body 9 to move up and down, finally, the third electric rotating block 1101 is opened to enable the third electric rotating block 1101 to drive the cleaning scraper 1102 to move back and forth on the surface of the lens 10, and meanwhile, the cleaning scraper 1102 drives the slider 1103 to move back and forth on the inner side of the sliding rail 1104, wherein the type of the electric lifting loop bar 401 is as follows: YS-NZ100-12A, the first motorized rotation block 406 is of the type: DG60-5, the model of the second electric rotating block 8 is: DG60-5, the model of the third electric rotating block 1101 is: y200RA60, so as to complete the use process of the whole stable-installation pod structure for aerial survey of unmanned aerial vehicles.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. The utility model provides an unmanned aerial vehicle of stable installation hanging cabin structure for aerial survey, includes mounting bracket (1), fixed establishment (3) and adjustment mechanism (4), its characterized in that: sealing mechanism (2) are installed to mounting bracket (1) top, mounting bracket (1) both sides are all installed in fixed establishment (3), adjustment mechanism (4) are installed in mounting bracket (1) below, support (5) have all been welded to adjustment mechanism (4) below both sides, damper (6) are installed to support (5) below, third connecting block (7) are installed to damper (6) below, the electronic rotatory piece of second (8) are installed to third connecting block (7) inboard, the electronic rotatory piece of second (8) inboard installation organism (9), camera lens (10) are installed to organism (9) inboard, camera lens (10) surface mounting has clearance mechanism (11).
2. The nacelle structure for unmanned aerial vehicle aerial survey of stable installation of claim 1, wherein: sealing mechanism (2) are including wiring mouth (201), movable block (202), movable hook (203) and sealing washer (204), wiring mouth (201) are seted up in mounting bracket (1) one side, wiring mouth (201) outer wall both sides all weld movable block (202), assorted movable hook (203) with it is installed to movable block (202) inboard, sealing washer (204) are installed to movable hook (203) one side.
3. The nacelle structure for unmanned aerial vehicle aerial survey of stable installation of claim 1, wherein: fixed establishment (3) include lifter (301), spacing hole (302), gag lever post (303) and fixing bolt (304), install in mounting bracket (1) inner wall both sides lifter (301), spacing hole (302) have been seted up to lifter (301) one side, gag lever post (303) are installed to spacing hole (302) inboard, fixing bolt (304) all run through in lifter (301) one side.
4. The nacelle structure for unmanned aerial vehicle aerial survey of stable installation of claim 1, wherein: adjustment mechanism (4) include electric lift loop bar (401), first connecting block (402), draw-in groove (403), fixture block (404), second connecting block (405) and first electronic rotatory piece (406), install in mounting bracket (1) below electric lift loop bar (401), the welding of electric lift loop bar (401) below has first connecting block (402), draw-in groove (403) have been seted up to first connecting block (402) one side, assorted fixture block (404) with it is installed to draw-in groove (403) inboard, the welding of fixture block (404) one side has second connecting block (405), first electronic rotatory piece (406) are installed to second connecting block (405) one side.
5. The nacelle structure for unmanned aerial vehicle aerial survey of stable installation of claim 1, wherein: damper (6) are including flexible cover (601), fixed block (602), expanding spring (603) and mount (604), flexible cover (601) welding is in support (5) below both sides, flexible cover (601) internal weld has fixed block (602), fixed block (602) one side welding has expanding spring (603), expanding spring (603) one side welding has mount (604).
6. The nacelle structure for unmanned aerial vehicle aerial survey of stable installation of claim 1, wherein: the second electric rotating blocks (8) are symmetrically distributed on the central axis of the machine body (9).
7. The nacelle structure for unmanned aerial vehicle aerial survey of stable installation of claim 1, wherein: the cleaning mechanism (11) comprises a third electric rotating block (1101), a cleaning scraper (1102), a slider (1103) and a sliding rail (1104), the third electric rotating block (1101) is installed on one side of the outer wall of the lens (10), the cleaning scraper (1102) is installed on one side of the third electric rotating block (1101), the slider (1103) is welded on one side of the cleaning scraper (1102), the slider (1103) is installed on the inner side of the sliding rail (1104), and the sliding rail (1104) is installed on one side of the lens (10).
CN202120922572.0U 2021-04-30 2021-04-30 Unmanned aerial vehicle aerial survey of stable installation is with hanging cabin structure Active CN214649093U (en)

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CN202120922572.0U CN214649093U (en) 2021-04-30 2021-04-30 Unmanned aerial vehicle aerial survey of stable installation is with hanging cabin structure

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Application Number Priority Date Filing Date Title
CN202120922572.0U CN214649093U (en) 2021-04-30 2021-04-30 Unmanned aerial vehicle aerial survey of stable installation is with hanging cabin structure

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115382801A (en) * 2022-08-29 2022-11-25 焦作市黄河华龙工程有限公司 Remote video water conservancy patrols dyke and checks out dangerous equipment

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115382801A (en) * 2022-08-29 2022-11-25 焦作市黄河华龙工程有限公司 Remote video water conservancy patrols dyke and checks out dangerous equipment
CN115382801B (en) * 2022-08-29 2023-12-19 焦作市黄河华龙工程有限公司 Remote video water conservancy dyke inspection equipment

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