CN218751465U

CN218751465U - But unmanned aerial vehicle of split

Info

Publication number: CN218751465U
Application number: CN202223358030.9U
Authority: CN
Inventors: 曹元园; 宋懿帆
Original assignee: Henan Qiwei Intelligent Flight Technology Co ltd
Current assignee: Henan Qiwei Intelligent Flight Technology Co ltd
Priority date: 2022-12-14
Filing date: 2022-12-14
Publication date: 2023-03-28
Anticipated expiration: 2032-12-14

Abstract

The utility model relates to an unmanned aerial vehicle electric power inspection technical field specifically is an unmanned aerial vehicle of split, which comprises a bod, probe and constraint device, the fixed surface of probe and fuselage is connected, the surface butt of fuselage has actuating mechanism, the constraint device sets up in fuselage and actuating mechanism's linking department, the constraint device includes the locating rack, the fixed surface of locating rack and fuselage is connected, the fixed surface of locating rack is connected with spacing post, the surface cover of spacing post is equipped with the knot frame, the thread groove has been seted up on the surface of spacing post, the inner wall threaded connection that spacing post is located the thread groove has the gim peg, the fixed surface of gim peg is connected with adjust knob, the surface cover of gim peg is equipped with the damping gasket. The utility model discloses, through setting up the constraint device for unmanned aerial vehicle's actuating mechanism can dismantle fast, has reduced then that unmanned aerial vehicle is difficult to the problem of in time maintenance after the field damage, has improved unmanned aerial vehicle maintenance efficiency under the field environment, has improved unmanned aerial vehicle's result of use.

Description

But unmanned aerial vehicle of split

Technical Field

The utility model relates to an unmanned aerial vehicle electric power patrols and examines technical field, especially relates to an unmanned aerial vehicle of removable branch.

Background

At the in-process that electric power was patrolled and examined, often need use unmanned aerial vehicle to inspect cable run to improve electric power and patrol and examine personnel's work efficiency, patrol and examine personnel through operation unmanned aerial vehicle alright inspect the operation to the cable run of eminence.

In the prior art, such as a utility model with publication number CN212605804U, the patent discloses an unmanned aerial vehicle convenient to disassemble and assemble, the patent adopts a bottom unmanned machine shell and a top unmanned machine shell, and the left and right sides of the bottom unmanned machine shell and the top unmanned machine shell are both provided with disassembling and assembling mechanisms; the disassembly and assembly mechanism comprises a fixing ring, a threaded hole, an L-shaped rod body, a motor shaft, an unmanned aerial vehicle fan blade, a threaded wall, a T-shaped plate, a first damping block, a second damping block and a spring; the top of the bottom unmanned machine shell is attached with a top unmanned machine shell, and fixing rings are integrally formed on the left side and the right side of the bottom unmanned machine shell and the top unmanned machine shell; the utility model discloses a solid fixed ring and the intra-annular L type body of rod of stationary ring on the unmanned aerial vehicle casing, not only can utilize L type body of rod, convenient dismouting motor and flabellum, and when L type body of rod is fixed, can fix unmanned casing and top unmanned casing at the bottom simultaneously, equally behind the dismouting L type body of rod, unmanned casing and top unmanned casing also can break away from the split voluntarily at the bottom, independent dismouting part has been saved, carry out the dismouting of wholeization and connect, the structure that uses is comparatively complicated in order to solve the unmanned aerial vehicle that has the dismouting function now, at practical application's in-process, because the step of operation assembly structure is loaded down with trivial details, lead to the problem of the dismouting operational difficulty of equipment.

The inventor discovers in daily work, the in-process of patrolling and examining at in-service use unmanned aerial vehicle, the structure that has current unmanned aerial vehicle is mostly the integral type, at the in-process that uses in the field, unmanned aerial vehicle's actuating mechanism easily collides with external production, the fault probability that leads to unmanned aerial vehicle's actuating mechanism is higher, when unmanned aerial vehicle's actuating mechanism breaks down, be difficult to maintain the operation because of the field environment, make the unmanned aerial vehicle of trouble can't maintain fast and put into operation again, lead to patrolling and examining personnel's the problem that work of patrolling and examining received the restriction.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving and having the field environment among the prior art and be difficult to maintain the operation for the unmanned aerial vehicle of trouble can't maintain fast and put into use again, leads to patrolling and examining personnel's the shortcoming that the work of patrolling and examining received the restriction, and the unmanned aerial vehicle of a removable division that proposes.

In order to achieve the above purpose, the utility model adopts the following technical scheme: the utility model provides an unmanned aerial vehicle of split, includes fuselage, probe and constraint device, the fixed surface of probe and fuselage is connected, the surface butt of fuselage has had actuating mechanism, the constraint device sets up the linking department at fuselage and actuating mechanism, the constraint device includes the locating rack, the fixed surface of locating rack and fuselage is connected, the fixed surface of locating rack is connected with spacing post, the surface cover of spacing post is equipped with detains the frame.

Preferably, the thread groove has been seted up on the surface of spacing post, the inner wall threaded connection that spacing post is located the thread groove has the gim peg, the fixed surface of gim peg is connected with adjust knob, the surface cover of gim peg is equipped with the damping gasket, sets up spacing post, through mutually supporting of spacing post and locating rack, can tentatively restrict actuating mechanism's position.

Preferably, the slot has been seted up on actuating mechanism's surface, the locating rack is pegged graft mutually with the inner wall of slot, the locating rack is with actuating mechanism's surperficial looks butt, spacing post runs through the actuating mechanism setting, the draw-in groove has been seted up on the surface of spacing post, detain the inner wall looks butt of frame and draw-in groove, detain the surface looks butt of frame and actuating mechanism, set up and detain the frame, through detaining the frame under damping gasket, gim peg and adjust knob's restriction, can fix actuating mechanism's position on the locating rack.

Preferably, the adjusting knob is abutted with the surface of a damping gasket, the damping gasket is abutted with the surface of the limiting column, the damping gasket is abutted with the surface of the buckling frame, the damping gasket is arranged, and the position of the buckling frame can be fixed under the limitation of the adjusting knob and the fixing bolt through the damping gasket.

Preferably, actuating mechanism's surface is provided with securing device, securing device includes the mounting bracket, the mounting bracket is connected with actuating mechanism's fixed surface, the inner wall of mounting bracket articulates there is the connecting block, the fixed surface of connecting block is connected with the guide post, sets up the mounting bracket, can restrict the position of connecting block through the mounting bracket to realize the supporting effect of connecting block.

Preferably, the surface of the guide column is fixedly connected with a connecting block, the surface of the connecting block is fixedly connected with a load spring, the surface of the connecting block is fixedly connected with a support, the connecting block is arranged, and the support position of the support can be supported and fixed under the support limit of the connecting frame and the guide column through the connecting block.

Preferably, the quantity of guide post is two, two the guide post is bilateral symmetry setting about the connecting block, the power-carrying spring is articulated mutually with the surface of connecting block, the power-carrying spring cup joints mutually with the surface of guide post, support frame and actuating mechanism's inner wall looks butt, set up the power-carrying spring, can absorb the stress that actuating mechanism produced through the power-carrying spring to reduce the load of actuating mechanism body.

Compared with the prior art, the utility model discloses an advantage lies in with positive effect:

in the utility model, through the arrangement of the binding device, when the electric power inspection is carried out, an operator operates the unmanned aerial vehicle to lift off, operates the unmanned aerial vehicle to approach the electric power cable, then the lens of the unmanned aerial vehicle can be opened, the state of the cable shot by the lens can be checked on the operation terminal, and then the cable can be inspected and checked step by step; when unmanned aerial vehicle's actuating mechanism takes place to damage, the knob is adjusted in rotation, adjust knob drive gim peg rotates, fixed commentaries on classics gradually breaks away from the thread groove at the in-process that changes, when the gim peg breaks away from the thread groove completely, the restraint of gim peg and adjust knob is lost to the damping gasket, simultaneously the damping gasket loses the restriction to detaining the frame, after detaining the frame and losing the restriction, the frame is detained in the downward pulling, detain and break away from actuating mechanism at the in-process that is pulled, actuating mechanism loses the restriction of detaining the frame, alright dismantle the operation to the actuating mechanism who damages immediately, thereby realize the change to actuating mechanism, through setting up the constraint device, make unmanned aerial vehicle's actuating mechanism can carry out quick dismantlement, then reduced the problem that unmanned aerial vehicle is difficult to in time maintenance after the field damage, the maintenance efficiency of unmanned aerial vehicle under the field environment is improved, unmanned aerial vehicle's result of use has been improved.

Drawings

Fig. 1 is a schematic perspective view of the detachable unmanned aerial vehicle according to the present invention;

fig. 2 is a schematic view of the detachable unmanned aerial vehicle in a bottom view;

fig. 3 is a schematic structural view of a detachable binding device of an unmanned aerial vehicle according to the present invention;

fig. 4 is a schematic structural view of the detachable stabilizing device of the unmanned aerial vehicle according to the present invention;

fig. 5 is a schematic structural diagram of a position a in fig. 4 of the detachable unmanned aerial vehicle according to the present invention.

Illustration of the drawings:

1. a body; 2. a probe; 3. a drive mechanism; 4. a restraint device; 41. a positioning frame; 42. a limiting post; 43. buckling frames; 44. a fixing bolt; 45. adjusting a knob; 46. a damping shim; 5. a securing device; 51. a mounting frame; 52. connecting blocks; 53. a guide post; 54. a joining block; 55. a load spring; 56. and (7) supporting.

Detailed Description

Referring to fig. 1-5, the present invention provides a technical solution: the utility model provides a but unmanned aerial vehicle of split, includes fuselage 1, probe 2 and constraint device 4, and the fixed surface of probe 2 and fuselage 1 is connected, and the surperficial butt of fuselage 1 has actuating mechanism 3, and constraint device 4 sets up in the linking department of fuselage 1 and actuating mechanism 3, and actuating mechanism 3's surface is provided with securing device 5.

The specific arrangement and function of the binding means 4 and the stabilising means 5 will be described in detail below.

In this embodiment: the binding device 4 comprises a positioning frame 41, the positioning frame 41 is fixedly connected with the surface of the machine body 1, a limiting column 42 is fixedly connected with the surface of the positioning frame 41, and a buckling frame 43 is sleeved on the surface of the limiting column 42.

Specifically, the thread groove has been seted up on spacing post 42's surface, and the inner wall threaded connection that spacing post 42 is located the thread groove has gim peg 44, and the fixed surface of gim peg 44 is connected with adjust knob 45, and the surface cover of gim peg 44 is equipped with damping shim 46, sets up spacing post 42, through mutually supporting of spacing post 42 and locating rack 41, can tentatively restrict actuating mechanism 3's position.

Specifically, a slot is formed in the surface of the driving mechanism 3, the positioning frame 41 is inserted into the inner wall of the slot, the positioning frame 41 abuts against the surface of the driving mechanism 3, the limiting column 42 penetrates through the driving mechanism 3, a clamping groove is formed in the surface of the limiting column 42, the buckling frame 43 is clamped against the inner wall of the clamping groove, and the buckling frame 43 abuts against the surface of the driving mechanism 3.

In this embodiment: a buckle frame 43 is provided, and the position of the driving mechanism 3 can be fixed on the positioning frame 41 through the buckle frame 43 under the restriction of the damping gasket 46, the fixing bolt 44 and the adjusting knob 45.

Specifically, the adjusting knob 45 abuts against the surface of the damping gasket 46, the damping gasket 46 abuts against the surface of the limiting column 42, the damping gasket 46 abuts against the surface of the buckle 43, the damping gasket 46 is arranged, and the position of the buckle 43 can be fixed under the limit of the adjusting knob 45 and the fixing bolt 44 through the damping gasket 46.

In this embodiment: the stabilizing device 5 comprises a mounting frame 51, the mounting frame 51 is fixedly connected with the surface of the driving mechanism 3, the inner wall of the mounting frame 51 is hinged with a connecting block 52, and the surface of the connecting block 52 is fixedly connected with a guide column 53.

In this embodiment: the mounting frame 51 is provided, and the position of the connecting block 52 can be limited through the mounting frame 51, so that the supporting effect of the connecting block 52 is realized.

Specifically, the surface of the guiding column 53 is fixedly connected with a connecting block 54, the surface of the connecting block 54 is fixedly connected with a load spring 55, the surface of the connecting block 54 is fixedly connected with a support frame 56, the connecting block 54 is arranged, and the support frame 56 can be supported and fixed by the connecting block 54 under the support limit of the connecting frame and the guiding column 53.

Specifically, the number of guide post 53 is two, and two guide posts 53 are bilateral symmetry setting about connecting block 52, and year power spring 55 is articulated mutually with the surface of connecting block 52, and year power spring 55 cup joints mutually with the surface of guide post 53, supports frame 56 and actuating mechanism 3's inner wall looks butt.

In this embodiment: the load spring 55 is provided, and the load of the main body of the drive mechanism 3 can be reduced by absorbing the stress generated in the drive mechanism 3 by the load spring 55.

The working principle is as follows: when power inspection is carried out, an operator operates the unmanned aerial vehicle to lift off, operates the unmanned aerial vehicle to approach a power cable, then can open a lens of the unmanned aerial vehicle, and check the state of the cable shot by the lens on an operation terminal, and then can carry out inspection and inspection on the cable gradually; when unmanned aerial vehicle's actuating mechanism 3 takes place to damage, adjust knob 45 is rotated, adjust knob 45 drive gim peg 44 rotates, fixed commentaries on classics gradually breaks away from the thread groove at the in-process that changes, when gim peg 44 breaks away from the thread groove completely, damping gasket 46 loses the restraint of gim peg 44 and adjust knob 45, damping gasket 46 loses the restriction to detaining frame 43 simultaneously, after detaining frame 43 loses the restriction, downwards pulling detains frame 43, detain frame 43 and break away from actuating mechanism 3 at the in-process that is pulled, actuating mechanism 3 loses the restriction of detaining frame 43, alright dismantle the operation to the actuating mechanism 3 that damages immediately, thereby realize the change to actuating mechanism 3, through setting up constraint device 4, make unmanned aerial vehicle's actuating mechanism 3 can carry out quick dismantlement, and then reduced the problem that unmanned aerial vehicle is difficult to in time to maintain after the field damage, the maintenance efficiency of unmanned aerial vehicle under the field environment has been improved, unmanned aerial vehicle's result of use has been improved. In addition, by arranging the stabilizing device 5, when the equipment descends, the driving mechanism 3 is in contact with the ground, the driving mechanism 3 generates impact at the moment of contacting the ground, so that acting force is formed, the driving mechanism 3 guides the acting force generated by the driving mechanism 3 to the mounting frame 51, the mounting frame 51 guides the acting force to the connecting block 52, the connecting block 52 transmits the acting force to the guide column 53, meanwhile, the connecting block 52 applies the acting force to the load bearing spring 55, the load bearing spring 55 absorbs the acting force exerted by the load bearing spring 55, the guide column 53 guides the acting force to the connecting block 54, the connecting block 54 guides the acting force to the abutting frame 56, the abutting frame 56 absorbs the acting force exerted by the connecting block 54, and the acting force bearing frame 56 and the load bearing spring 55 are matched, so that the structural strength of the driving mechanism 3 is improved, the load borne by the driving mechanism 3 during the equipment is reduced, and the stability of the driving mechanism 3 is further improved.

Claims

1. The utility model provides a but unmanned aerial vehicle of split, includes fuselage (1), probe (2) and constraint device (4), its characterized in that: the utility model discloses a safety belt conveyor, including probe (2), the fixed surface of fuselage (1) is connected, the surperficial butt of fuselage (1) has actuating mechanism (3), constraint device (4) set up the linking department at fuselage (1) and actuating mechanism (3), constraint device (4) are including locating rack (41), the fixed surface of locating rack (41) and fuselage (1) is connected, the fixed surface of locating rack (41) is connected with spacing post (42), the surface cover of spacing post (42) is equipped with detains frame (43).

2. A detachable unmanned aerial vehicle according to claim 1, wherein: the utility model discloses a damping spacer, including spacing post (42), inner wall threaded connection that spacing post (42) are located the thread groove has gim peg (44), the fixed surface of gim peg (44) is connected with adjust knob (45), the surface cover of gim peg (44) is equipped with damping gasket (46).

3. A detachable unmanned aerial vehicle according to claim 1, wherein: the slot has been seted up on the surface of actuating mechanism (3), locating rack (41) are pegged graft with the inner wall of slot mutually, the surperficial looks butt of locating rack (41) and actuating mechanism (3), actuating mechanism (3) setting is run through in spacing post (42), the draw-in groove has been seted up on the surface of spacing post (42), detain the inner wall looks butt of frame (43) and draw-in groove, detain the surface looks butt of frame (43) and actuating mechanism (3).

4. A detachable unmanned aerial vehicle according to claim 2, wherein: the adjusting knob (45) is abutted with the surface of a damping gasket (46), the damping gasket (46) is abutted with the surface of the limiting column (42), and the damping gasket (46) is abutted with the surface of the buckling frame (43).

5. A detachable unmanned aerial vehicle according to claim 1, wherein: the surface of actuating mechanism (3) is provided with securing device (5), securing device (5) include mounting bracket (51), mounting bracket (51) are connected with the fixed surface of actuating mechanism (3), the inner wall of mounting bracket (51) articulates there is connecting block (52), the fixed surface of connecting block (52) is connected with guide post (53).

6. A detachable unmanned aerial vehicle according to claim 5, wherein: the surface of the guide column (53) is fixedly connected with a connecting block (54), the surface of the connecting block (54) is fixedly connected with a load spring (55), and the surface of the connecting block (54) is fixedly connected with a support frame (56).

7. A detachable unmanned aerial vehicle according to claim 6, wherein: the quantity of guide post (53) is two, two guide post (53) are bilateral symmetry setting about connecting block (52), carry power spring (55) and hinge mutually with the surface of connecting block (52), carry power spring (55) and cup joint mutually with the surface of guide post (53), support the inner wall looks butt of frame (56) and actuating mechanism (3).