CN216970025U - Be used for unmanned aerial vehicle to patrol and examine machine-mounted proprietary equipment - Google Patents
Be used for unmanned aerial vehicle to patrol and examine machine-mounted proprietary equipment Download PDFInfo
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- CN216970025U CN216970025U CN202220738759.XU CN202220738759U CN216970025U CN 216970025 U CN216970025 U CN 216970025U CN 202220738759 U CN202220738759 U CN 202220738759U CN 216970025 U CN216970025 U CN 216970025U
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- unmanned aerial
- aerial vehicle
- bracket component
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- equipment
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- 238000007689 inspection Methods 0.000 claims abstract description 21
- 238000012544 monitoring process Methods 0.000 claims abstract description 19
- 230000000694 effects Effects 0.000 abstract description 6
- 230000005484 gravity Effects 0.000 abstract description 4
- 230000002093 peripheral effect Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 10
- 230000003139 buffering effect Effects 0.000 description 3
- 230000004308 accommodation Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
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Abstract
The utility model provides onboard exclusive equipment for unmanned aerial vehicle inspection, which comprises an inspection equipment body and a frame, wherein the inspection equipment body comprises a support component and a buffer structure, a control cabin is installed at the top end of the frame, a base is installed at the bottom end of the frame, the top end of the support component is installed at the bottom of the base, an external monitoring system is installed at the top end of the support component, a built-in monitoring system is installed at the bottom end of the support component, a power component is installed at the top end of the support component, the external monitoring system is steered through the power component to realize peripheral monitoring, the center of gravity is set at the center of the unmanned aerial vehicle due to the use of balancing weights, the center of gravity is unchanged when the external monitoring system is steered, and the flight stability during inspection is improved, and the chassis surrounds the built-in monitoring system, so that the protection effect is improved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to onboard special equipment for unmanned aerial vehicle inspection.
Background
Unmanned aerial vehicle patrols and examines airborne exclusive equipment and can be patrolling and examining the in-process, to outer broken, mountain fire, real-time identification and early warning of circuit hidden danger such as fishing and wire foreign matter, current man-machine is patrolled and examined airborne exclusive equipment and is installed on unmanned aerial vehicle, scan analysis and transmission are carried out to the scene of below through the camera, but owing to patrol and examine in-process camera chance and carry out corresponding angle modulation, consequently can lead to the focus to change in the accommodation process, and then rock, stability is relatively poor, on the other hand, patrol and examine airborne exclusive equipment embeds multiple sensor, the cost is high, generally install in the fuselage bottom, in case take place signal loss of contact or control system trouble will lead to the bottom to suffer the impact when falling during consequently descending, structural strength is not enough, lack effectual descending protection architecture.
SUMMERY OF THE UTILITY MODEL
Aiming at the defects in the prior art, the utility model aims to provide the inspection onboard dedicated equipment for the unmanned aerial vehicle, so as to solve the problems in the background art, the inspection onboard dedicated equipment can avoid the condition of gravity center deviation in the angle adjusting process of a camera system, has higher flight stability, and has a corresponding anti-falling protection structure.
In order to realize the purpose, the utility model is realized by the following technical scheme: the utility model provides a be used for unmanned aerial vehicle to patrol and examine airborne exclusive equipment, includes equipment body and the frame of patrolling and examining, it includes bracket component and buffer structure to patrol and examine the equipment body, the control storehouse is installed on the top of frame, the base is installed to the bottom of frame, the bottom at the base is installed on the top of bracket component, external monitored control system is installed on the top of bracket component, built-in monitored control system is installed to the bottom of bracket component, power component is installed on the top of bracket component, the motor is installed on power component's top.
Furthermore, the bracket component mainly comprises a conical sleeve, the external monitoring system is fixed on the surface of the conical sleeve, a balancing weight is installed at the top end of the conical sleeve, and a chassis is arranged at the bottom end of the conical sleeve.
Furthermore, an air bag is arranged inside the chassis, the bottom end of the air bag is connected with a compressed air tank, an opening is formed in the surface of the chassis, and the buffer structure is arranged at the bottom end of the chassis.
Furthermore, the balancing weight is provided with three groups, and every balancing weight is the same with external monitored control system's shape, weight homogeneous, the balancing weight is fixed at the side at toper sleeve top with external monitored control system is even.
Further, buffer structure includes undercarriage and spring beam, the top of spring beam is provided with the ram, the spout of vertical structure is seted up to the inside on chassis, the inside of spout is all inserted to the top of spring beam and ram.
Further, spring beam, ram and compressed gas jar all are provided with four groups, and every spring beam, ram and compressed gas jar of group all install on same vertical axis, the rubber pad is equipped with in the bottom subsides of undercarriage.
Further, the power assembly is arranged in the middle of the bracket assembly and the base, the output shaft of the motor penetrates downwards from the surface of the base and is connected with the driving gear, and the driving gear is meshed with the driven gear.
Further, driven gear overlaps and establishes the surface at the pivot, the bottom and the bracket component fixed connection of pivot, driven gear's inboard and the fixed surface of pivot are connected, and driven gear's bottom and the top of bracket component are provided with the clearance.
The utility model has the beneficial effects that: the utility model discloses an onboard exclusive device for unmanned aerial vehicle inspection, which comprises an inspection device body, wherein the inspection device body comprises a rack, a control bin, a power assembly, a support assembly, a buffer structure, an external monitoring system, a motor, a rotating shaft, a driving gear, a driven gear, a base, a conical sleeve, an opening, a balancing weight, an air bag, a chassis, an undercarriage, a spring rod, a ram, an internal monitoring system and a compressed air tank.
1. This be used for unmanned aerial vehicle to patrol and examine airborne exclusive equipment adopts external and built-in two monitored control system, turns to external monitored control system through power component and realizes outlying control, and because the use of balancing weight sets the focus in this unmanned aerial vehicle's central point, and because balancing weight central symmetry distributes, therefore external monitored control system turns to the time focus position unchangeable, has improved the flight stability when patrolling and examining.
2. This be used for unmanned aerial vehicle to patrol and examine airborne exclusive equipment adds in the bottom of bracket component and is equipped with annular buffer structure, has improved buffering shock attenuation effect to surround built-in monitored control system through the chassis, improved the protection effect.
3. This be used for unmanned aerial vehicle to patrol and examine machine-carried exclusive equipment has air bag and compressor jar at chassis internally mounted, if unmanned aerial vehicle falls out of control or when the whereabouts impact force too big lead to the spring beam shrink excessively, can launch air bag through the ram striking compressor jar and form the expansion protection effect in the twinkling of an eye.
Drawings
Fig. 1 is a schematic structural diagram of the appearance of the onboard dedicated equipment for unmanned aerial vehicle inspection according to the utility model;
fig. 2 is a schematic structural diagram of a support assembly part of an onboard dedicated device for unmanned aerial vehicle inspection according to the utility model;
fig. 3 is a sectional view of a component part of an onboard dedicated equipment support for unmanned aerial vehicle inspection according to the utility model;
fig. 4 is a partial cross-sectional view of an inspection machine chassis for inspecting airborne equipment of an unmanned aerial vehicle according to the present invention;
in the figure: 1. a frame; 2. a control cabin; 3. a power assembly; 4. a bracket assembly; 5. a buffer structure; 6. an external monitoring system; 7. a motor; 8. a rotating shaft; 9. a driving gear; 10. a driven gear; 11. a base; 12. a tapered sleeve; 13. an opening; 14. a balancing weight; 15. an air bag; 16. a chassis; 17. a landing gear; 18. a spring lever; 19. a ram; 20. a monitoring system is arranged in the device; 21. a compressed gas tank.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the utility model easy to understand, the utility model is further described with the specific embodiments.
Referring to fig. 1 to 4, the present invention provides a technical solution: a patrol and examine airborne exclusive equipment for unmanned aerial vehicle, including patrolling and examining equipment body and frame 1, patrol and examine the equipment body and include bracket component 4 and buffer structure 5, control chamber 2 is installed on the top of frame 1, base 11 is installed to the bottom of frame 1, the top of bracket component 4 is installed in the bottom of base 11, external monitored control system 6 is installed on the top of bracket component 4, built-in monitored control system 20 is installed to the bottom of bracket component 4, power component 3 is installed to the top of bracket component 4, motor 7 is installed to the top of power component 3, the device installs base 11 part in the bottom of frame 1 through using the screw, and install bracket component 4 in the bottom of base 11 through pivot 8, whole bracket component 4 rotates around the central point of base 11 through pivot 8, and install external monitored control system 6 and built-in monitored control system 20 in the outside or inboard of bracket component 4, along with pivot 8 and bracket component 4 synchronous revolution, and 2 electric connection of control storehouse through electric wire and 1 top of frame, the information that can gather in the monitored control system sends to the outside through the inside wireless module in control storehouse 2, realize patrolling and examining the function, wherein built-in monitored control system 20 installs the bottom at bracket component 4, by the inside encirclement of bracket component 4 of coniform, mainly patrol and examine the circuit of bottom in the unmanned aerial vehicle flight state, external monitored control system 6 then patrols and examines the circuit in the remote position of side, it patrols and examines the region to have constituteed on a large scale jointly.
In this embodiment, the support assembly 4 mainly comprises a conical sleeve 12, the external monitoring system 6 is fixed on the surface of the conical sleeve 12, the top end of the conical sleeve 12 is provided with a balancing weight 14, the bottom end of the conical sleeve 12 is provided with a chassis 16, the balancing weights 14 are provided with three groups, each balancing weight 14 has the same shape and weight as the external monitoring system 6, the balancing weights 14 and the external monitoring system 6 are uniformly fixed on the side edge of the top of the conical sleeve 12, the external monitoring system 6 is mounted on the surface of the conical sleeve 12, a plurality of balancing weights 14 having the same shape and weight as the external monitoring system 6 are mounted on the surface of the conical sleeve 12, in this embodiment, the number of the balancing weights 14 is three groups, the balancing weights are symmetrically mounted on the periphery of the top of the conical sleeve 12, and the center of gravity of the unmanned aerial vehicle is adjusted by the balancing weights 14 and the external monitoring system 6, finally transfer the focus to bracket component 4's intermediate position, consequently when the power component 3 through the top rotates whole bracket component 4 around 8 parts of pivot, the focus is in pivot 8's axis department, even rotate angle regulation with external monitored control system 6, reconcile the focus position of whole frame 1 of in-process and do not change, consequently frame 1 part can not adjust because centrobaric change yet, the control angle accommodation process that makes whole external monitored control system 6 can not exert an influence to unmanned aerial vehicle's flight condition, the stability of flight has been improved.
This embodiment, buffer structure 5 includes undercarriage 17 and spring beam 18, the top of spring beam 18 is provided with ram 19, vertical structure's spout has been seted up to the inside on chassis 16, the inside of spout is all inserted to the top of spring beam 18 and ram 19, passes through spring beam 18 and is connected with buffer structure 5 in the bottom of bracket component 4, when descending, because buffer structure 5 is located whole unmanned aerial vehicle's least significant end, consequently can be through undercarriage 17 and the ground contact of buffer structure 5 bottom, the undercarriage 17 of loop configuration can provide more symmetrical holding power, consequently the in-process of descending can be even with the impact force dispersion to buffering on the spring beam 18 all around, the stability of descending has been improved.
In this embodiment, four sets of spring rods 18, rams 19 and compressed air tanks 21 are provided, each set of spring rods 18, rams 19 and compressed air tanks 21 is installed on the same vertical axis, a rubber pad is attached to the bottom end of the landing gear 17, an airbag 15 is installed inside the chassis 16, a compressed air tank 21 is connected to the bottom end of the airbag 15, an opening 13 is opened on the surface of the chassis 16, the buffer structure 5 is installed at the bottom end of the chassis 16, the top end of the spring rod 18 is inserted into the chassis 16 at the bottom end of the tapered sleeve 12, when the unmanned aerial vehicle falls or descends at a speed exceeding a safety threshold, the impact force is increased sharply, the impact force is visualized through contraction of springs on the surface of the spring rods 18, when the springs contract to a certain range, the spring rod 18 at the top end moves to a higher point of the chassis 16, until the impact force makes the ram 19 at the top end of the spring rod 18 touch the built-in compressed air tank 21, can trigger through impact force compression gas pitcher 21, inject into air bag 15's inside with inside compressed gas, outwards expand air bag 15 from opening 13, realize further buffering protection effect, avoid producing the damage to the whole equipment of patrolling and examining of bottom, this process only can appear going on under the condition that unmanned aerial vehicle takes place unusual descending, take place the last protective procedure when falling as unmanned aerial vehicle, wherein air bag 15 and compression gas pitcher 21 are current mature technique.
This embodiment, power component 3 installs the intermediate position at bracket component 4 and base 11, the output shaft of motor 7 is partly passed downwards from base 11 surface and is connected with driving gear 9, driving gear 9 meshes with driven gear 10 mutually, driven gear 10 cover is established on the surface of pivot 8, the bottom and the bracket component 4 fixed connection of pivot 8, the inboard of driven gear 10 is connected with the fixed surface of pivot 8, and the bottom of driven gear 10 and the top of bracket component 4 are provided with the clearance, and the built-in monitored control system 20 of bottom patrols the bottom in real time when patrolling and examining patrols and examines, and the external monitored control system 6 in the outside then drives whole bracket component 4 through the power component 3 on top and carries out the regulation of angle, and the motor 7 at the top fixed mounting of base 11 drives the driving gear 9 of bottom through the output shaft, can drive driven gear 10 through driving gear 9 meshes mutually with driven gear 10 and rotate, driven gear 10's inside and pivot 8 fixed connection can drive bracket component 4 realization synchronous revolution of bottom through pivot 8, and can patrol and examine the regulation and control of scope to the external monitored control system 6 on surface during rotatory.
While there have been shown and described what are at present considered the fundamental principles and essential features of the utility model and its advantages, it will be apparent to those skilled in the art that the utility model is not limited to the details of the foregoing exemplary embodiments, but is capable of other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (8)
1. The utility model provides a be used for unmanned aerial vehicle to patrol and examine airborne exclusive equipment, includes equipment body and frame (1) of patrolling and examining, its characterized in that: patrol and examine equipment body and include bracket component (4) and buffer structure (5), control storehouse (2) are installed on the top of frame (1), base (11) are installed to the bottom of frame (1), the bottom in base (11) is installed on the top of bracket component (4), external monitored control system (6) are installed on the top of bracket component (4), built-in monitored control system (20) are installed to the bottom of bracket component (4), power component (3) are installed on the top of bracket component (4), motor (7) are installed on the top of power component (3).
2. The special equipment for unmanned aerial vehicle inspection machine according to claim 1, wherein: bracket component (4) mainly comprise taper sleeve (12), the surface at taper sleeve (12) is fixed in external monitored control system (6), balancing weight (14) are installed on the top of taper sleeve (12), the bottom of taper sleeve (12) is provided with chassis (16).
3. The dedicated equipment for unmanned aerial vehicle inspection machine according to claim 2, wherein: the safety airbag device is characterized in that an air bag (15) is arranged inside the chassis (16), a compressed air tank (21) is connected to the bottom end of the air bag (15), an opening (13) is formed in the surface of the chassis (16), and the buffer structure (5) is arranged at the bottom end of the chassis (16).
4. The dedicated equipment for unmanned aerial vehicle inspection machine according to claim 2, wherein: the balancing weight (14) is provided with three groups, the shape and the weight of each balancing weight (14) are the same as those of the external monitoring system (6), and the balancing weights (14) and the external monitoring system (6) are uniformly fixed on the side edge of the top of the conical sleeve (12).
5. The special equipment for unmanned aerial vehicle inspection machine according to claim 3, wherein: buffer structure (5) include undercarriage (17) and spring beam (18), the top of spring beam (18) is provided with ram (19), the spout of vertical structure is seted up to the inside on chassis (16), the inside of spout is all inserted in the top of spring beam (18) and ram (19), the bottom of ram (19) is provided with the limiting plate structure of evagination.
6. The inspection machine for unmanned aerial vehicles is exclusively used in claim 5, and is characterized in that: the spring rods (18), the hammers (19) and the compressed air tanks (21) are all provided with four groups, each group of spring rods (18), the hammers (19) and the compressed air tanks (21) are all arranged on the same vertical axis, and rubber pads are attached to the bottom ends of the landing gears (17).
7. The special equipment for unmanned aerial vehicle inspection machine according to claim 1, wherein: the power assembly (3) is arranged in the middle of the bracket assembly (4) and the base (11), the output shaft of the motor (7) penetrates downwards from the surface of the base (11) and is connected with the driving gear (9), and the driving gear (9) is meshed with the driven gear (10).
8. The dedicated equipment for unmanned aerial vehicle inspection machine according to claim 7, wherein: driven gear (10) cover is established on the surface of pivot (8), the bottom and bracket component (4) fixed connection of pivot (8), the inboard of driven gear (10) is connected with the fixed surface of pivot (8), and is provided with the clearance between the bottom of driven gear (10) and the top of bracket component (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220738759.XU CN216970025U (en) | 2022-03-31 | 2022-03-31 | Be used for unmanned aerial vehicle to patrol and examine machine-mounted proprietary equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220738759.XU CN216970025U (en) | 2022-03-31 | 2022-03-31 | Be used for unmanned aerial vehicle to patrol and examine machine-mounted proprietary equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216970025U true CN216970025U (en) | 2022-07-15 |
Family
ID=82340220
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220738759.XU Expired - Fee Related CN216970025U (en) | 2022-03-31 | 2022-03-31 | Be used for unmanned aerial vehicle to patrol and examine machine-mounted proprietary equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216970025U (en) |
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2022
- 2022-03-31 CN CN202220738759.XU patent/CN216970025U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220715 |
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| CF01 | Termination of patent right due to non-payment of annual fee |