CN216057074U - Online cloud monitoring and observing aircraft working state equipment - Google Patents
Online cloud monitoring and observing aircraft working state equipment Download PDFInfo
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- CN216057074U CN216057074U CN202121452204.0U CN202121452204U CN216057074U CN 216057074 U CN216057074 U CN 216057074U CN 202121452204 U CN202121452204 U CN 202121452204U CN 216057074 U CN216057074 U CN 216057074U
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 61
- 230000017525 heat dissipation Effects 0.000 claims abstract description 22
- 239000000428 dust Substances 0.000 claims description 11
- 238000013461 design Methods 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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Abstract
The utility model belongs to the field of monitoring, and particularly relates to an on-line cloud monitoring and observing aircraft working state device which comprises a shell, a storage protection mechanism, a heat dissipation mechanism, a handle and a base, wherein the storage protection mechanism is arranged on one side of the shell and comprises a cloud monitoring display screen, and a hinge is connected to one side of the cloud monitoring display screen; through the hinge, the base, the structural design of electric lift loop bar and operation mesa, realized folding convenient function of accomodating for cloud control display screen, solved when carrying the operation, because can't lead to occupation of land space big to cloud control display screen spin-fold, the condition of difficult carrying, thereby the problem of portability has been reduced, when carrying, it descends to start electric lift loop bar drive operation mesa, accomodate cloud control display screen through the hinge spin-fold again, thereby the carrying of observing aircraft operating condition equipment for this online cloud control has provided better guarantee, the practicality has been strengthened.
Description
Technical Field
The utility model relates to the field of monitoring, in particular to equipment for monitoring and observing the working state of an aircraft on line by cloud.
Background
The monitoring system is one of the most applied systems in the security system, the construction site monitoring system suitable for the market is a handheld video communication device, video monitoring is the mainstream at present, and changes in the world from the earliest analog monitoring to the digital monitoring in the past years to the current popular network video monitoring are caused, and monitoring methods are various, such as cloud monitoring.
Cloud monitoring is a hot issue of security industry, and most of the industry talks about the concept of smart cities, and the security cloud and IT cloud computing are classified into equal numbers, resource virtualization and cloud service, so that the monitoring industry at the present stage is in a transition stage from monitoring data concentration to virtualization and resource utilization.
But the effect that the aircraft operating condition equipment was observed in online cloud control that uses at present was accomodate for the majority and is carried is not good, when carrying the operation, because can't lead to the space occupation big to the rotatory folding condition that leads to of cloud control display screen, is difficult for carrying to reduced portability, so, propose online cloud control to observe aircraft operating condition equipment to above-mentioned problem.
SUMMERY OF THE UTILITY MODEL
In order to make up for the defects of the prior art and solve the problem that the aircraft cannot be conveniently carried and stored, the utility model provides equipment for monitoring and observing the working state of the aircraft on line through cloud.
The technical scheme adopted by the utility model for solving the technical problems is as follows: the utility model relates to an on-line cloud monitoring and observing aircraft working state device which comprises a shell, a storage protection mechanism, a heat dissipation mechanism, a handle and a base, wherein the storage protection mechanism is arranged on one side of the shell and comprises a cloud monitoring display screen, one side of the cloud monitoring display screen is connected with a hinge, a protection plate is arranged on the back surface of the cloud monitoring display screen, a plurality of fixing pieces are fixed on two sides of the protection plate, the heat dissipation mechanism is arranged on two sides of the shell and comprises heat dissipation fins, a plurality of fixing bolts are fixed on the peripheries of the heat dissipation fins, a dust screen is arranged on the inner sides of the heat dissipation fins, clamping blocks are arranged on two sides of the dust screen, and clamping grooves are formed in one side of each clamping block.
The handle is installed in one side of shell, the both sides of handle all are fixed with the screw rod, the surface of handle is provided with the rubber pad, the base sets up the inboard at the shell, the upper end of base is connected with the electric lift loop bar, the other end of electric lift loop bar is connected with the operation mesa, the surface of operation mesa is provided with the protection pad.
Preferably, the cloud monitoring display screen is movably connected with the shell through hinges, and the hinges are distributed on the cloud monitoring display screen at equal intervals.
Preferably, the guard plate passes through stationary blade and cloud control display screen swing joint, and the stationary blade is equidistant distribution on cloud control display screen.
Preferably, the radiating fins are in threaded connection with the shell through fixing bolts, and the fixing bolts are distributed on the radiating fins at equal intervals.
Preferably, the dustproof net passes through the fixture block, the clamping groove and the radiating fin to form a detachable structure, and the fixture block is arranged by a vertical middle axis symmetry axis of the dustproof net.
Preferably, the handle is movably connected with the shell through a screw rod, and the rubber pad is tightly attached to the handle.
Preferably, the operation table top, the electric lifting sleeve rod and the base form a lifting structure, and the electric lifting sleeve rod and the base are vertically distributed.
Preferably, the protection pad is tightly attached to the operation table top, and the size of the protection pad is matched with that of the operation table top.
The utility model has the advantages that:
1. according to the portable cloud monitoring and observing aircraft working state equipment, the function of folding and conveniently accommodating the cloud monitoring display screen is achieved through the structural design of the hinge, the base, the electric lifting sleeve rod and the operating table board, the problem that the cloud monitoring display screen occupies a large space and is not easy to carry due to the fact that the cloud monitoring display screen cannot be rotated and folded during carrying operation is solved, and therefore the problem of portability is solved;
2. according to the utility model, through the structural design of the radiating fin, the fixing bolt, the dustproof net, the clamping block and the clamping groove, the radiating function of the device for monitoring and observing the working state of the aircraft on line is improved, the problem that the device fails due to the fact that the internal temperature is too high and cannot be discharged because of continuous long-time work is solved, the dustproof net is clamped into the clamping groove through the clamping block and is installed on the inner side of the radiating fin, and then the radiating fin is installed on two sides of the shell through the fixing bolt, so that better guarantee is provided for the radiating dustproof performance of the device for monitoring and observing the working state of the aircraft on line.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.
FIG. 1 is a schematic front view of an embodiment;
FIG. 2 is a schematic structural diagram of an embodiment in a front view;
FIG. 3 is a schematic structural view of a storage protection mechanism according to an embodiment;
FIG. 4 is a schematic structural diagram of a heat dissipation mechanism according to an embodiment;
FIG. 5 is an enlarged view of the structure at A in FIG. 3 according to the present invention.
In the figure: 1. a housing; 2. a storage protection mechanism; 201. a cloud monitoring display screen; 202. a hinge; 203. a protection plate; 204. a fixing sheet; 3. a heat dissipation mechanism; 301. a heat sink; 302. fixing the bolt; 303. a dust screen; 304. a clamping block; 305. a card slot; 4. a handle; 5. a screw; 6. a rubber pad; 7. a base; 8. an electric lifting loop bar; 9. an operation table top; 10. and (6) a protective pad.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the 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.
Referring to fig. 1-5, an on-line cloud monitoring and observing aircraft working state device comprises a housing 1, a storage protection mechanism 2, a heat dissipation mechanism 3, a handle 4 and a base 7, wherein the storage protection mechanism 2 is arranged on one side of the housing 1, the storage protection mechanism 2 comprises a cloud monitoring display screen 201, a hinge 202 is connected to one side of the cloud monitoring display screen 201, a protection plate 203 is mounted on the back of the cloud monitoring display screen 201, a plurality of fixing plates 204 are fixed to two sides of the protection plate 203, the heat dissipation mechanism 3 is arranged on two sides of the housing 1, the heat dissipation mechanism 3 comprises a heat dissipation fin 301, a plurality of fixing bolts 302 are fixed to the periphery of the heat dissipation fin 301, a dust screen 303 is mounted on the inner side of the heat dissipation fin 301, fixture blocks 304 are arranged on two sides of the dust screen 303, and a clamping groove 305 is formed in one side of the fixture blocks 304.
Preferably, the cloud monitoring display screen 201 is movably connected with the housing 1 through hinges 202, and the hinges 202 are distributed on the cloud monitoring display screen 201 at equal intervals.
Preferably, the protection plate 203 is movably connected with the cloud monitoring display screen 201 through the fixing plates 204, and the fixing plates 204 are distributed on the cloud monitoring display screen 201 at equal intervals.
Preferably, the heat sink 301 is screwed to the housing 1 by fixing bolts 302, and the fixing bolts 302 are equally spaced on the heat sink 301.
Preferably, the dust screen 303 is detachably arranged between the clamping block 304, the clamping groove 305 and the heat sink 301, and the clamping block 304 is arranged around a vertical central axis of the dust screen 303.
Preferably, the handle 4 is movably connected with the housing 1 through a screw 5, and the rubber pad 6 is tightly attached to the handle 4.
Preferably, the operation table top 9, the electric lifting sleeve rod 8 and the base 7 form a lifting structure, and the electric lifting sleeve rod 8 and the base 7 are vertically distributed.
Preferably, the protection pad 10 is closely attached to the operation table 9, and the size of the protection pad 10 is matched with the size of the operation table 9.
The electrical components presented in the document are all electrically connected with an external master controller and 220V mains, and the master controller can be a conventional known device controlled by a computer or the like.
When the working state of the aircraft needs to be monitored and observed, the dust screen 303 is clamped into the clamping groove 305 through the clamping block 304 and is installed on the inner side of the radiating fin 301, then the radiating fin 301 is installed on the two sides of the shell 1 through the fixing bolt 302, after the work is finished, the electric lifting sleeve rod 8 is started to drive the operation table top 9 to descend, then the cloud monitoring display screen 201 is rotatably folded and stored through the hinges 202, and the cloud monitoring display screen is released and carried through the handle 4, wherein the electric lifting sleeve rod 8 is started to be YS-NZ100-12A, and the working principle of the device for monitoring and observing the working state of the aircraft is the online cloud monitoring and observing.
In conclusion, the on-line cloud monitoring and observing aircraft working state equipment realizes the function of folding and conveniently storing the cloud monitoring display screen 201 through the structural design of the hinge 202, the base 7, the electric lifting sleeve rod 8 and the operation table board 9, solves the problem that the cloud monitoring display screen 201 cannot be folded in a rotating way to cause large occupied space and is not easy to carry during carrying operation, thereby reducing the portability, when in carrying, the electric lifting sleeve rod 8 is started to drive the operation table board 9 to descend, and then the cloud monitoring display screen 201 is folded and stored in a rotating way through the hinge 202, thereby providing better guarantee for the carrying and storing performance of the on-line cloud monitoring and observing aircraft working state equipment, enhancing the practicability, and through the structural design of the radiating fins 301, the fixing bolts 302, the dustproof net 303, the clamping blocks 304 and the clamping grooves 305, the heat dissipation function of the on-line cloud monitoring and observing aircraft working state equipment is improved, the problem of continuous long-time work cause inside high temperature can not discharge and lead to equipment to break down is solved, go into card slot 305 inboard with dust screen 303 through fixture block 304 and install it to fin 301 inboard, install fin 301 the both sides of shell 1 through fixing bolt 302 again to the heat dissipation dirt proofness of this online cloud control observation aircraft operating condition equipment provides better guarantee.
In the description herein, references to the description of "one embodiment," "an example," "a specific example" or the like are intended to mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the utility model. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The foregoing shows and describes the general principles, essential features, and advantages of the utility model. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the utility model as claimed.
Claims (8)
1. On-line cloud control observation aircraft operating condition equipment, its characterized in that: the novel solar heat collector comprises a shell (1), a storage protection mechanism (2), a heat dissipation mechanism (3), a handle (4) and a base (7), wherein the storage protection mechanism (2) is arranged on one side of the shell (1), the storage protection mechanism (2) comprises a cloud monitoring display screen (201), a hinge (202) is connected to one side of the cloud monitoring display screen (201), a protection plate (203) is installed on the back surface of the cloud monitoring display screen (201), a plurality of fixing plates (204) are fixed to two sides of the protection plate (203), the heat dissipation mechanism (3) is arranged on two sides of the shell (1), the heat dissipation mechanism (3) comprises heat dissipation fins (301), a plurality of fixing bolts (302) are fixed to the periphery of each heat dissipation fin (301), a dust screen (303) is installed on the inner side of each heat dissipation fin (301), clamping blocks (304) are arranged on two sides of each dust screen (303), a clamping groove (305) is formed in one side of the clamping block (304);
handle (4) are installed in one side of shell (1), the both sides of handle (4) all are fixed with screw rod (5), the surface of handle (4) is provided with rubber pad (6), base (7) set up the inboard at shell (1), the upper end of base (7) is connected with electric lift loop bar (8), the other end of electric lift loop bar (8) is connected with operation mesa (9), the surface of operation mesa (9) is provided with protection pad (10).
2. The on-line cloud monitoring and observing aircraft working state device of claim 1, characterized in that: cloud control display screen (201) are through hinge (202) and shell (1) swing joint, and hinge (202) are equidistant distribution on cloud control display screen (201).
3. The on-line cloud monitoring and observing aircraft working state device of claim 1, characterized in that: protection plate (203) are through stationary blade (204) and cloud control display screen (201) swing joint, and stationary blade (204) are equidistant distribution on cloud control display screen (201).
4. The on-line cloud monitoring and observing aircraft working state device of claim 1, characterized in that: the radiating fins (301) are in threaded connection with the shell (1) through fixing bolts (302), and the fixing bolts (302) are distributed on the radiating fins (301) at equal intervals.
5. The on-line cloud monitoring and observing aircraft working state device of claim 1, characterized in that: the dustproof net (303) forms a detachable structure through the clamping blocks (304), the clamping grooves (305) and the radiating fins (301), and the clamping blocks (304) are arranged in a mode of being symmetrical to the vertical middle axis of the dustproof net (303).
6. The on-line cloud monitoring and observing aircraft working state device of claim 1, characterized in that: the handle (4) is movably connected with the shell (1) through the screw rod (5), and the rubber pad (6) is tightly attached to the handle (4).
7. The on-line cloud monitoring and observing aircraft working state device of claim 1, characterized in that: the operation table top (9), the electric lifting sleeve rod (8) and the base (7) form a lifting structure, and the electric lifting sleeve rod (8) and the base (7) are vertically distributed.
8. The on-line cloud monitoring and observing aircraft working state device of claim 1, characterized in that: the protection pad (10) is tightly attached to the operation table top (9), and the size of the protection pad (10) is matched with that of the operation table top (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121452204.0U CN216057074U (en) | 2021-06-28 | 2021-06-28 | Online cloud monitoring and observing aircraft working state equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121452204.0U CN216057074U (en) | 2021-06-28 | 2021-06-28 | Online cloud monitoring and observing aircraft working state equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216057074U true CN216057074U (en) | 2022-03-15 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121452204.0U Expired - Fee Related CN216057074U (en) | 2021-06-28 | 2021-06-28 | Online cloud monitoring and observing aircraft working state equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216057074U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115711643A (en) * | 2022-10-27 | 2023-02-24 | 广州清迈电子有限公司 | Environment monitoring instrument |
-
2021
- 2021-06-28 CN CN202121452204.0U patent/CN216057074U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115711643A (en) * | 2022-10-27 | 2023-02-24 | 广州清迈电子有限公司 | Environment monitoring instrument |
| CN115711643B (en) * | 2022-10-27 | 2023-10-31 | 广州清迈电子有限公司 | Environment monitoring instrument |
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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: 20220315 |