CN211419177U - Staying unmanned aerial vehicle's receipts line control mechanism - Google Patents
Staying unmanned aerial vehicle's receipts line control mechanism Download PDFInfo
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- CN211419177U CN211419177U CN201921813107.2U CN201921813107U CN211419177U CN 211419177 U CN211419177 U CN 211419177U CN 201921813107 U CN201921813107 U CN 201921813107U CN 211419177 U CN211419177 U CN 211419177U
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Abstract
The utility model discloses a staying unmanned aerial vehicle's receipts line control mechanism, its structure includes the receipts line box, the cable, staying unmanned aerial vehicle, the receipts line box is located subaerially, the cable cooperation is installed in receipts line box one side, staying unmanned aerial vehicle inlays in the cable end, the receipts chamber is installed to the receipts line box internally, the receipts chamber is equipped with the support column, the top board, the paying out machine, the unwrapping wire area, the lower locating plate, the admission machine, receive the line area, the wall inlays and is equipped with the outlet in the receipts chamber, the outlet is equipped with guide rail, cable pipe, the wire reel is installed to the support column inboard, the wire reel is equipped with wire winding groove, wire releasing groove, wire receiving groove, baffle, receipts line box one side is equipped with the intake plate, the intake plate is equipped with limiting plate, spacing groove, proximity switch, when staying unmanned aerial vehicle ascends, it rises to drive the cable, when the cable is, the pay-off belt drives the pay-off groove to rotate, the wire spool rotates to enable the cable to extend, and the phenomenon that the cable is pulled due to tight tightening is avoided.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle and specifically relates to a staying unmanned aerial vehicle's receipts line control mechanism is related to.
Background
Mooring unmanned aerial vehicle is a novel unmanned aerial vehicle system, through using the ground power supply, sacrifices the journey and enables the carrier to reach the long-time purpose that stagnates and hover, and the mooring cable of power supply is accomodate on the capstan winch, is dragged out the cable by operating personnel when the carrier rises, is withdrawed the cable by hand or motor drive capstan winch when the carrier descends.
But current mooring unmanned aerial vehicle's receipts line control mechanism, the unable regulation of speed of receiving and releasing the line appears the cable easily and causes the phenomenon of dragging to mooring unmanned aerial vehicle, leads to the emergence of crash accident, and the winding phenomenon appears easily in the cable overlength of release.
SUMMERY OF THE UTILITY MODEL
Receive line control mechanism to current mooring unmanned aerial vehicle, the unable regulation of speed of receiving and releasing line appears the cable easily and causes to moor unmanned aerial vehicle and drags the phenomenon, leads to the emergence of crash accident, and the cable overlength of release appears winding phenomenon easily not enough, the utility model provides a mooring unmanned aerial vehicle's receiving line control mechanism solves above-mentioned technical problem.
The utility model discloses a realize through following technical scheme: the utility model provides a staying unmanned aerial vehicle's receipts line control mechanism, its structure includes receipts line box, cable, staying unmanned aerial vehicle, receive the line box and locate subaerially, the cable cooperation is installed in receipts line box one side, staying unmanned aerial vehicle inlays admittedly in the cable end, it has the chamber of accomodating to receive line box internally mounted.
Further say, accomodate the chamber and be equipped with support column, top board, admission machine, receive the line area, lower locating plate, paying out machine, pay off tape, the support column passes through welded connection and accomodates the intracavity wall, top board and lower locating plate inlay admittedly in accomodating the chamber with one side, the admission machine passes through bolted connection inside the top board, it installs around the admission machine to receive the line area cooperation, the paying out machine passes through bolted connection inside the lower locating plate, the cooperation of pay off tape is installed around the paying out machine.
Furthermore, a wire outlet is embedded in the inner wall of the accommodating cavity, a guide rail and a cable tube are arranged at the wire outlet, the guide rail is embedded in the wire outlet, and the cable tube is arranged between the two guide rails.
Furthermore, the wire spool is installed to the support column inboard, the wire spool is equipped with wire winding groove, wire releasing groove, receipts wire casing, baffle, the wire winding groove inlays to be located around the wire spool, wire releasing groove inlays respectively in the wire spool both sides with receiving the wire casing, two baffles are respectively through welded connection in the wire releasing groove with receive the wire outside of groove.
Furthermore, take-up box one side is equipped with the storage plate, the storage plate is equipped with limiting plate, spacing groove, proximity switch, the limiting plate passes through welded connection in storage plate surface, the spacing groove inlays and locates limiting plate one side, proximity switch inlays admittedly in spacing inslot wall.
Advantageous effects
The utility model relates to a staying unmanned aerial vehicle's receipts line control mechanism compares with prior art and has following advantage:
1. the utility model winds the cable around the winding groove through the winding groove on the winding disc, and the end of the cable is connected to the bottom of the mooring unmanned aerial vehicle, so that the mooring unmanned aerial vehicle can hover for a long time in the air;
2. when the mooring unmanned aerial vehicle ascends, the cable is driven to ascend, and when the cable is close to and tightened, the cable contacts with the proximity switch above, so that the paying-off machine in the upper positioning plate is started, the paying-off belt drives the paying-off groove to rotate, the wire spool rotates to stretch out the cable, the phenomenon that the cable is tightened and pulled is avoided, and the occurrence of crash accidents is avoided;
3. the utility model discloses when the cable overlength that emits, the proximity switch of flagging cable below for the admission machine in the locating plate starts down, makes the take-up belt drive receipts wire casing and rotates, makes wire reel opposite direction rotate and makes the cable withdraw, avoids the cable overlength to take place winding phenomenon.
Drawings
Other features, objects and advantages of the invention will become more apparent upon reading of the detailed description of non-limiting embodiments with reference to the following drawings:
fig. 1 is the utility model relates to a stay unmanned aerial vehicle's receipts line control mechanism's schematic structure diagram.
Fig. 2 is the schematic diagram of the internal amplification structure of the wire-rewinding box of the present invention.
Fig. 3 is a schematic side view of the wire spool according to the present invention.
Fig. 4 is the side-view enlarged structure schematic diagram of the take-up box of the utility model.
In the figure: the wire winding box comprises a wire winding box 1, a cable 2, a mooring unmanned aerial vehicle 3, a storage cavity a, a support column a1, an upper positioning plate a2, a wire paying out machine a3, a wire paying out belt a4, a lower positioning plate a5, a wire winding machine a6, a wire winding belt a7, a wire outlet b, a guide rail b1, a cable pipe b2, a wire winding disc c, a wire winding groove c1, a wire paying out groove c2, a wire winding groove c3, a baffle c4, a storage plate d, a limit plate d1, a limit groove d2 and a proximity switch d 3.
Detailed Description
In order to make the technical means, the creation features, the achievement purposes and the functions of the present invention easy to understand, the following description is combined with the detailed description and the accompanying drawings to further explain the preferred embodiments of the present invention.
Examples
Please refer to fig. 1-4, the utility model provides a staying unmanned aerial vehicle's receipts line control mechanism, its structure includes receipts line box 1, cable 2, staying unmanned aerial vehicle 3, receive line box 1 and locate subaerially, 2 cooperation installations in receipts line box 1 one side of cable, staying unmanned aerial vehicle 3 inlays admittedly in 2 ends of cable, receive 1 internally mounted of line box and accomodate chamber an.
Accomodate chamber a and be equipped with support column a1, go up locating plate a2, admission machine a3, receive line area a4, lower locating plate a5, paying out machine a6, unwrapping wire area a7, support column a1 is through welding connection in accomodating chamber an inner wall, go up locating plate a2 and lower locating plate a5 and inlay in accomodating chamber a same side, admission machine a3 passes through bolted connection inside last locating plate a2, receive line area a4 cooperation and install around admission machine a3, paying out machine a6 passes through bolted connection inside lower locating plate a5, unwrapping wire area a7 cooperation is installed around paying out machine a 6.
An outlet b is embedded in the inner wall of the accommodating cavity a, a guide rail b1 and a cable tube b2 are arranged at the outlet b, the guide rail b1 is embedded inside the outlet b, and the cable tube b2 is installed between the two guide rails b 1.
Wire reel c is installed to support column a1 inboard, wire reel c is equipped with wire winding groove c1, unwrapping wire groove c2, receives wire winding groove c3, baffle c4, wire winding groove c1 inlays and locates around the wire winding groove c, wire winding groove c2 inlays respectively in wire winding c both sides with receiving wire groove c3, two baffle c4 are respectively through welded connection in wire winding groove c2 and receive the wire winding groove c3 outside.
The principle of the utility model is as follows: one end of a cable 2 is placed on a winding groove c1 of a winding disc c in a take-up box 1, the cable 2 passes through a cable tube b2 and passes through a guide rail b1 on a wire outlet b, the other end of the cable 2 is connected to the bottom of a tethered unmanned aerial vehicle 3, so that the tethered unmanned aerial vehicle 3 achieves the purpose of long-time hovering, when the tethered unmanned aerial vehicle 3 works, the tethered unmanned aerial vehicle 3 ascends to enable the cable 2 to be gradually tightened, when the cable 2 approaches a limiting groove d2 at the bottom of an upper limiting plate d1, a corresponding approach switch d3 is triggered, a paying-off machine a3 inside an upper locating plate a2 is started, the paying-off machine a3 rotates to enable a paying-off belt a4 to drive a winding groove c2 to rotate, the winding disc c is paid off, the cable 2 extends out of the take-up box 1, the phenomenon of pulling is avoided, the accident caused, the unmanned aerial vehicle 3 descends to enable the cable 2 to be gradually loosened, when the cable 2 approaches, trigger corresponding proximity switch d3 for the inside admission machine a6 of lower locating plate a5 starts, and admission machine a6 rotates and makes receipts line area a7 drive receipts line groove c3 and rotate, makes wire reel c receive the line, makes cable 2 retrieve and receive line box 1, avoids the cable overlength to take place winding phenomenon.
The technical features of the embodiments described above may be arbitrarily combined, and for the sake of brevity, all possible combinations of the technical features in the embodiments described above are not described, but should be considered as being within the scope of the present specification as long as there is no contradiction between the combinations of the technical features.
Claims (5)
1. The utility model provides a staying unmanned aerial vehicle's receipts line control mechanism, its structure is including receiving line box (1), cable (2), staying unmanned aerial vehicle (3), its characterized in that:
receive line box (1) and locate subaerially, cable (2) cooperation is installed in receiving line box (1) one side, mooring unmanned aerial vehicle (3) are embedded in cable (2) end, receive line box (1) internally mounted and accomodate chamber (a).
2. The line-winding control mechanism of a tethered drone of claim 1, wherein: accomodate chamber (a) and be equipped with support column (a1), go up locating plate (a2), admission machine (a3), receive line area (a4), lower locating plate (a5), paying out machine (a6), unwrapping wire area (a7), support column (a1) are through welded connection in accomodating chamber (a) inner wall, go up locating plate (a2) and lower locating plate (a5) and inlay in accomodating chamber (a) same side, admission machine (a3) are inside through bolted connection in last locating plate (a2), receive line area (a4) cooperation and install around admission machine (a3), paying out machine (a6) are inside through bolted connection in lower locating plate (a5), unwrapping wire area (a7) cooperation is installed around paying out machine (a 6).
3. The line-winding control mechanism of a tethered drone of claim 2, wherein: accomodate chamber (a) inner wall and inlay and be equipped with outlet (b), outlet (b) is equipped with guide rail (b1), cable pipe (b2), inside outlet (b) was inlayed and is located in guide rail (b1), cable pipe (b2) are installed between two guide rails (b 1).
4. The line-winding control mechanism of a tethered drone of claim 2, wherein: wire reel (c) are installed to support column (a1) inboard, wire reel (c) are equipped with wire winding groove (c1), unwrapping wire groove (c2), receive wire winding groove (c3), baffle (c4), wire winding groove (c1) are inlayed and are located around wire reel (c), wire winding groove (c2) and receipts wire casing (c3) are inlayed respectively and are fixed in wire reel (c) both sides, two baffle (c4) are respectively through welded connection in wire winding groove (c2) and receipts wire casing (c3) outside.
5. The line-winding control mechanism of a tethered drone of claim 1, wherein: receive line box (1) one side and be equipped with storage plate (d), storage plate (d) is equipped with limiting plate (d1), spacing groove (d2), proximity switch (d3), limiting plate (d1) are through welded connection in storage plate (d) surface, limiting groove (d2) are inlayed and are located limiting plate (d1) one side, proximity switch (d3) are inlayed and are fixed in spacing groove (d2) inner wall.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201921813107.2U CN211419177U (en) | 2019-10-25 | 2019-10-25 | Staying unmanned aerial vehicle's receipts line control mechanism |
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CN201921813107.2U CN211419177U (en) | 2019-10-25 | 2019-10-25 | Staying unmanned aerial vehicle's receipts line control mechanism |
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CN211419177U true CN211419177U (en) | 2020-09-04 |
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CN201921813107.2U Active CN211419177U (en) | 2019-10-25 | 2019-10-25 | Staying unmanned aerial vehicle's receipts line control mechanism |
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2019
- 2019-10-25 CN CN201921813107.2U patent/CN211419177U/en active Active
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Effective date of registration: 20210409 Address after: 417100 building 3, poverty alleviation Industrial Park, Loudi hi tech Industrial Development Zone, Lianyuan City, Loudi City, Hunan Province Patentee after: HUNAN JINGFEI INTELLIGENT TECHNOLOGY Co.,Ltd. Address before: 530004, 100 East University Road, the Guangxi Zhuang Autonomous Region, Nanning Patentee before: Wei Jianjing |