CN215972127U - Deicing unmanned aerial vehicle's self stabilization adjustment mechanism - Google Patents
Deicing unmanned aerial vehicle's self stabilization adjustment mechanism Download PDFInfo
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- CN215972127U CN215972127U CN202122800115.7U CN202122800115U CN215972127U CN 215972127 U CN215972127 U CN 215972127U CN 202122800115 U CN202122800115 U CN 202122800115U CN 215972127 U CN215972127 U CN 215972127U
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- 230000007246 mechanism Effects 0.000 title claims abstract description 26
- 238000011105 stabilization Methods 0.000 title claims abstract description 12
- 230000006641 stabilisation Effects 0.000 title claims abstract description 4
- 239000007921 spray Substances 0.000 claims abstract description 34
- 230000005484 gravity Effects 0.000 claims abstract description 23
- 230000033001 locomotion Effects 0.000 claims description 4
- 238000009434 installation Methods 0.000 abstract description 8
- 230000000694 effects Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 abstract description 3
- 230000008569 process Effects 0.000 abstract description 3
- 230000008859 change Effects 0.000 abstract description 2
- 230000005540 biological transmission Effects 0.000 description 8
- 238000005507 spraying Methods 0.000 description 3
- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012212 insulator Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- 230000009467 reduction Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a self-stabilization adjusting mechanism of an deicing unmanned aerial vehicle, which is used for connecting the unmanned aerial vehicle and a spray gun, and comprises an installation seat and a hanging bracket, wherein the installation seat is arranged at the bottom of the unmanned aerial vehicle, the hanging bracket comprises a first connecting sleeve used for connecting the front part of the spray gun and a second connecting sleeve used for connecting the rear part of the spray gun, a fixed vertical rod is arranged at the bottom of the installation seat, the second connecting sleeve is hinged on the fixed vertical rod, a sliding mechanism which can move back and forth is arranged at the front position of the installation seat, a gravity center adjusting component is arranged at the moving end of the sliding mechanism, and the first connecting sleeve is connected with the gravity center adjusting component through a hinged connecting rod structure. The center of gravity adjusting component moves back and forth and can drive the spray gun to use the second connecting sleeve and the connecting point of fixed montant as the center and carry out angle modulation, and center of gravity adjusting component can balance the focus change that the spray gun leads to in angle modulation process again simultaneously, realizes the self stabilization effect.
Description
Technical Field
The utility model relates to the field of unmanned aerial vehicle accessories, in particular to a self-stabilization adjusting mechanism of a deicing unmanned aerial vehicle.
Background
The high-voltage transmission line is a main channel for electric energy transmission, the cable icing generated in severe cold weather in winter not only increases the whole weight of the transmission line, but also influences the electrical performance of the transmission line, and serious icing can cause line accidents such as transmission line galloping and disconnection, even pole tower collapse, insulator flashover and the like, which threaten the normal and stable operation of the transmission line. Therefore, ice coating removal for high voltage transmission line overhang is a routine and extremely difficult task for the power department.
Along with the development of science and technology, some transmission line defroster have been developed to relevant mechanism, deicing unmanned aerial vehicle is wherein the better one of effect promptly, deicing unmanned aerial vehicle carries ice-melt agent and rises to the high altitude, spray icing the point, easy operation, ice-melt is effectual, in order to improve the degree of accuracy of spraying ice-melt agent, utilize a longer spray gun as spraying tool usually, the spray gun is the snap-on in unmanned aerial vehicle bottom usually, also lead to the every single move angle of spray gun to be difficult to adjust, on the other hand is owing to the reaction force when spraying, lead to the stability reduction of unmanned aerial vehicle flight.
SUMMERY OF THE UTILITY MODEL
In view of this, the present invention aims to overcome the defects in the prior art, and provides a self-stabilization adjusting mechanism for a deicing unmanned aerial vehicle, which can adjust the angle of a spray gun of the deicing unmanned aerial vehicle and keep self-stabilization.
The self-stabilization adjusting mechanism of the deicing unmanned aerial vehicle is used for connecting the unmanned aerial vehicle and a spray gun, and comprises an installation seat and a hanging bracket, wherein the installation seat is arranged at the bottom of the unmanned aerial vehicle, the hanging bracket comprises a first connecting sleeve used for connecting the front part of the spray gun and a second connecting sleeve used for connecting the rear part of the spray gun, a fixed vertical rod is arranged at the bottom of the installation seat, the second connecting sleeve is hinged on the fixed vertical rod, a sliding mechanism which can move back and forth is arranged at the front position of the installation seat, a gravity center adjusting assembly is arranged at the moving end of the sliding mechanism, and the first connecting sleeve is connected with the gravity center adjusting assembly through a hinged connecting rod structure.
Further, the connecting rod structure comprises an upper connecting rod, a lower connecting rod and a central lever assembly, wherein a fulcrum part of the central lever assembly is connected to the mounting seat through a support, two ends of the upper connecting rod are respectively hinged with a force application end and a gravity center adjusting assembly of the central lever assembly, and two ends of the lower connecting rod are respectively hinged with a force bearing end and a first connecting sleeve of the central lever assembly.
Furthermore, the central lever assembly comprises a force applying arm, a force receiving arm and a buffer spring which are connected in a triangular mode, and the central lever assembly is connected to the support by taking a hinged point of the force applying arm and the force receiving arm as a fulcrum.
Further, the gravity center adjusting assembly comprises a connecting piece and a counterweight piece; the connecting piece is of a sheet structure, an upper connecting seat connected with the sliding mechanism is arranged on the upper surface of the connecting piece, a lower connecting seat connected with the connecting rod structure is arranged on the lower surface of the connecting piece, a plurality of connecting screw holes are formed in the front-back direction of the board surface of the connecting piece, and the counterweight piece is positioned at the connecting screw holes through bolts.
Furthermore, a connecting support is arranged between the first connecting sleeve and the second connecting sleeve, and an angle sensor is arranged on the connecting support.
The utility model has the beneficial effects that: the utility model discloses a self-stabilization adjusting mechanism of an deicing unmanned aerial vehicle, which comprises a mounting seat and a hanging bracket, wherein the hanging bracket is connected to a spray gun and comprises a first connecting sleeve and a second connecting sleeve, the first connecting sleeve is arranged at the front of the spray gun, the second connecting sleeve is arranged at the rear of the spray gun, the second connecting sleeve is hinged to the mounting seat through a fixed vertical rod, the first connecting sleeve is connected to a gravity center adjusting component capable of moving back and forth through a connecting rod structure, the gravity center adjusting component can drive the spray gun to carry out angle adjustment by taking a connecting point of the second connecting sleeve and the fixed vertical rod as a center when moving back and forth, and meanwhile, the gravity center adjusting component can balance gravity center change caused by the spray gun in the angle adjusting process, so that the self-stabilization effect is realized.
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The utility model is further described below with reference to the following figures and examples:
FIG. 1 is a schematic structural diagram of a first embodiment of the present invention;
FIG. 2 is a schematic structural diagram of a second embodiment of the present invention;
FIG. 3 is a schematic view of the construction of the center lever assembly of the present invention;
fig. 4 is a schematic structural view of the center of gravity adjusting assembly according to the present invention.
Description of reference numerals: unmanned aerial vehicle 1, spray gun 2, mounting base 3, hanger 4, first connecting sleeve 41, second connecting sleeve 42, fixed vertical rod 43, gravity center adjusting component 5, connecting piece 51, upper connecting base 511, lower connecting base 512, counterweight 52, connecting rod structure 6, upper connecting rod 61, lower connecting rod 62, central lever component 63, force applying arm 631, force applying arm 632, buffer spring 633, support 64, angle sensor 7, angle sensor 42,
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1, the self-stabilization adjusting mechanism of the deicing unmanned aerial vehicle in the present embodiment is connected between an unmanned aerial vehicle 1 and a spray gun 2, and includes a mounting base 3 and a hanger 4, wherein the mounting base 3 is arranged at the bottom of the unmanned aerial vehicle 1, and the hanger 4 is arranged on the spray gun 2; the gallows 4 divide into two parts, lean on the first adapter sleeve 41 of preceding part and be used for connecting spray gun 2 to lean on the second adapter sleeve 42 of back part including being used for connecting spray gun 2, 3 bottoms of mount pad are provided with a fixed montant 43, the second connector articulates on fixed montant 43, and fixed montant 43 can't be relative mount pad 3 rotates, but second adapter sleeve 42 can carry out certain angle's rotation for fixed montant 43, mount pad 3 leans on preceding position to be provided with the glide machanism of back-and-forth movement, for example screw rod mechanism or electric cylinder mechanism, glide machanism's removal end is provided with focus adjusting part 5, first adapter sleeve 41 through articulated link structure 6 with focus adjusting part 5 connects.
In an embodiment, the connecting rod structure 6 is a simple single connecting rod, the mounting base 3, the fixed vertical rod 43 and the spray gun 2 form a quadrilateral structure, and in the process of moving the center of gravity adjusting assembly 5 back and forth, the spray gun 2 is driven to perform angle adjustment in the pitching direction, preferably, the sliding mechanism only drives the part of the center of gravity adjusting assembly 5 before the spray gun 2 performs upward rotary motion to move, specifically, the center of gravity adjusting assembly 5 moves forward, the spray gun 2 is adjusted downward from a horizontal state, and the center of gravity shifting problem caused by angle adjustment of the spray gun 2 can be balanced by the movement of the center of gravity adjusting assembly 5.
As shown in fig. 2-3, in the present embodiment, the link structure 6 includes an upper link 61, a lower link 62 and a central lever assembly 63, a fulcrum portion of the central lever assembly 63 is connected to the mounting base 3 through a bracket 64, two ends of the upper link 61 are respectively hinged to the force applying end of the central lever assembly 63 and the center of gravity adjusting assembly 5, two ends of the lower link 62 are respectively hinged to the force receiving end of the central lever assembly 63 and the first connecting sleeve 41, and the driving power required by the sliding mechanism can be reduced through the lever structure.
In this embodiment, the central lever assembly 63 includes a force applying arm 631, a force receiving arm 632, and a buffer spring 633, and the central lever assembly 63 is connected to the bracket 64 with a hinge point of the force applying arm 631 and the force receiving arm 632 as a pivot. The buffer spring 633 can slow down the impact force on the unmanned aerial vehicle 1 when the spray gun 2 sprays.
In this embodiment, the center of gravity adjusting assembly 5 includes a connecting member 51 and a weight member 52; the connecting piece 51 is a sheet structure, the upper surface of the connecting piece is provided with an upper connecting seat 511 connected with a sliding mechanism, so that the connecting piece can move under the driving of the sliding mechanism, the lower surface of the connecting piece is provided with a lower connecting seat 512 connected with the connecting rod structure 6, the plate surface of the connecting piece 51 is provided with a plurality of connecting screw holes along the front-back direction, the counterweight piece 52 is positioned at the connecting screw holes through bolts, and the counterweight piece 52 can be adjusted in the front-back direction according to actual requirements.
In this embodiment, a connection bracket is arranged between the first connection sleeve 41 and the second connection sleeve 42, the connection bracket is provided with the angle sensor 7, an operator can adjust the angle data according to the angle data monitored by the angle sensor 7, and the first connection sleeve 41 and the second connection sleeve 42 are connected through the connection bracket, so that the fixing of the first connection sleeve 41 and the second connection sleeve to the spray gun 2 is firmer.
Finally, the above embodiments are only for illustrating the technical solutions of the present invention and not for limiting, although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made to the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, and all of them should be covered in the claims of the present invention.
Claims (5)
1. The utility model provides a deicing unmanned aerial vehicle's self stabilization adjustment mechanism for connect unmanned aerial vehicle and spray gun, its characterized in that: including mount pad and gallows, the mount pad sets up in the unmanned aerial vehicle bottom, the gallows is including being used for connecting the spray gun and leaning on the first adapter sleeve of preceding part and being used for connecting the spray gun and lean on the second adapter sleeve of back part, the mount pad bottom is provided with a fixed montant, the second adapter sleeve articulates on the fixed montant, the position that the mount pad leaned on the front is provided with the glide machanism of back-and-forth movement, glide machanism's removal end is provided with focus adjusting part, first adapter sleeve through articulated connecting rod structure with focus adjusting part connects.
2. Self-stabilizing adjustment mechanism of deicing unmanned aerial vehicle according to claim 1, characterized in that: the connecting rod structure comprises an upper connecting rod, a lower connecting rod and a central lever assembly, wherein the fulcrum part of the central lever assembly is connected to the mounting seat through a support, two ends of the upper connecting rod are respectively hinged with a force application end and a gravity center adjusting assembly of the central lever assembly, and two ends of the lower connecting rod are respectively hinged with a force bearing end and a first connecting sleeve of the central lever assembly.
3. Self-stabilizing adjustment mechanism of deicing unmanned aerial vehicle according to claim 2, characterized in that: the central lever assembly comprises a force applying arm, a force receiving arm and a buffer spring which are connected in a triangular mode, and the central lever assembly is connected to the support with a hinge point of the force applying arm and the force receiving arm as a fulcrum.
4. Self-stabilizing adjustment mechanism of deicing unmanned aerial vehicle according to claim 1, characterized in that: the gravity center adjusting assembly comprises a connecting piece and a counterweight piece; the connecting piece is of a sheet structure, an upper connecting seat connected with the sliding mechanism is arranged on the upper surface of the connecting piece, a lower connecting seat connected with the connecting rod structure is arranged on the lower surface of the connecting piece, a plurality of connecting screw holes are formed in the front-back direction of the board surface of the connecting piece, and the counterweight piece is positioned at the connecting screw holes through bolts.
5. Self-stabilizing adjustment mechanism of deicing unmanned aerial vehicle according to claim 1, characterized in that: a connecting support is arranged between the first connecting sleeve and the second connecting sleeve, and an angle sensor is arranged on the connecting support.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122800115.7U CN215972127U (en) | 2021-11-16 | 2021-11-16 | Deicing unmanned aerial vehicle's self stabilization adjustment mechanism |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122800115.7U CN215972127U (en) | 2021-11-16 | 2021-11-16 | Deicing unmanned aerial vehicle's self stabilization adjustment mechanism |
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| CN215972127U true CN215972127U (en) | 2022-03-08 |
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| CN202122800115.7U Active CN215972127U (en) | 2021-11-16 | 2021-11-16 | Deicing unmanned aerial vehicle's self stabilization adjustment mechanism |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114355986A (en) * | 2022-03-21 | 2022-04-15 | 山东天空之眼智能科技有限公司 | Unmanned aerial vehicle self-adaptation anti-interference control system |
-
2021
- 2021-11-16 CN CN202122800115.7U patent/CN215972127U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114355986A (en) * | 2022-03-21 | 2022-04-15 | 山东天空之眼智能科技有限公司 | Unmanned aerial vehicle self-adaptation anti-interference control system |
| CN114355986B (en) * | 2022-03-21 | 2022-06-03 | 山东天空之眼智能科技有限公司 | Unmanned aerial vehicle self-adaptation anti-interference control system |
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