CN109058702A - A kind of road in airport monitoring system - Google Patents
A kind of road in airport monitoring system Download PDFInfo
- Publication number
- CN109058702A CN109058702A CN201810982197.1A CN201810982197A CN109058702A CN 109058702 A CN109058702 A CN 109058702A CN 201810982197 A CN201810982197 A CN 201810982197A CN 109058702 A CN109058702 A CN 109058702A
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- Prior art keywords
- shaft
- gear
- groove
- support column
- monitoring system
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 37
- 238000009510 drug design Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 5
- 238000012423 maintenance Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003331 infrared imaging Methods 0.000 description 1
- 239000013307 optical fiber Substances 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/06—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
- F16M11/08—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting around a vertical axis, e.g. panoramic heads
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/18—Heads with mechanism for moving the apparatus relatively to the stand
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/20—Undercarriages with or without wheels
- F16M11/2085—Undercarriages with or without wheels comprising means allowing sideward adjustment, i.e. left-right translation of the head relatively to the undercarriage
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/20—Undercarriages with or without wheels
- F16M11/2092—Undercarriages with or without wheels comprising means allowing depth adjustment, i.e. forward-backward translation of the head relatively to the undercarriage
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/183—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
- H04N7/185—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source from a mobile camera, e.g. for remote control
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Studio Devices (AREA)
Abstract
The invention belongs to monitoring system technical fields, in particular a kind of road in airport monitoring system, including fixing seat, signal input module, voice module, control unit, power supply module and alarm module, signal input module, voice module, power supply module and alarm module are connected with control unit, sliding slot is offered at the top of the fixing seat, support column is slidably fitted in sliding slot, and it is extended to outside sliding slot at the top of support column, sliding slot offers first rotating shaft slot on the inner wall of support column side, sliding slot offers the second rotary axis groove on the inner wall far from support column side, the same first rotating shaft is rotatably equipped in first rotating shaft slot and the second rotary axis groove, gear grooved is offered at the top of fixing seat.The present invention has rational design, easy to use, and camera is easy to remove and rotates, and can effectively drop to the cost of monitoring system erection, while avoiding monitor damage bring risk, reduces blind area of monitoring, ensures aircraft Normal Take-Off And Landing.
Description
Technical field
The present invention relates to monitoring system technical field more particularly to a kind of road in airport monitoring systems.
Background technique
Typical TV monitor system is mainly by front end supervision equipment, transmission device, rear end storage, control and display equipment
This five most of composition, wherein rear end equipment can be further divided into central control equipment and sub-control control equipment, and front and back ends equipment has
A variety of constituted modes, the connection between them can be realized by various ways such as cable, optical fiber, microwaves.
Application No. is CN201210294093.4 to disclose a kind of airport monitoring system of cradle head control, including video terminal
Equipment, demultplexer, GIS map control system, radar, radar fix coordinated control system, alarm system and monitor terminal,
The radar is connect with the radar fix coordinated control system, the video frequency terminal apparatus respectively with the demultplexer and
The monitor terminal connection, the monitor terminal are sat with the GIS map control system, the radar respectively by communication network
Mark coordinated control system is connected with the alarm system, and the video monitoring equipment includes holder, CCD camera and infrared imaging
Instrument, the CCD camera and the infrared thermoviewer are separately positioned on the holder, and infrared thermoviewer and CCD camera are handed over
Video monitoring is realized for control, and the use of infrared thermoviewer avoids the external boisterous influence to monitor video, also real
The normal monitoring for having showed night ensure that the safety and validity of monitoring system, still, monitor in the prior art to field road logical
Often road in airport is monitored by the way that multiple monitors are arranged, monitoring system construction cost is high, and later maintenance cost is high, and its
There is monitor damage in if, blind area of monitoring will be formed, there are greater risk, monitoring is not easy to be moved, and camera is also inconvenient
In being rotated, with the progress of science and technology, social development, more stringent requirements are proposed to monitoring system by people, for this purpose,
It is proposed a kind of road in airport monitoring system.
Summary of the invention
The purpose of the present invention is to provide a kind of road in airport monitoring systems, to solve original mentioned above in the background art
Some is in the prior art usually monitored the monitoring of field road by the way that multiple monitors are arranged to road in airport, monitoring system building
At high cost, later maintenance cost is high, and if wherein have monitor damage, blind area of monitoring will be formed, there are greater risks, and monitoring is not
It is convenient for moving, camera is also not easy to be rotated.
To achieve the goals above, present invention employs following technical solutions: a kind of road in airport monitoring system, including solid
Reservation, signal input module, voice module, control unit, power supply module and alarm module, signal input module, voice module,
Power supply module and alarm module are connected with control unit, and sliding slot is offered at the top of the fixing seat, sliding peace in sliding slot
It is extended to outside sliding slot equipped with support column, and at the top of support column, sliding slot offers first turn on the inner wall of support column side
Axial trough, sliding slot offer the second rotary axis groove, rotation in first rotating shaft slot and the second rotary axis groove on the inner wall far from support column side
The same first rotating shaft is installed, gear grooved is offered at the top of fixing seat, and gear grooved is connected with the second rotary axis groove, first
Shaft is located at one end fixing sleeve in gear grooved and is equipped with first gear, is fixedly installed with first servo motor at the top of fixing seat,
It is fixedly installed with second gear on the output shaft of first servo motor, second gear and first gear are wound with same the jointly
One belt, opens up at the top of support column fluted, and support rod is rotatably equipped in groove, is fixedly installed with and takes the photograph at the top of support rod
As head, the second rotary axis groove is offered on the inner wall of groove bottom side, the second shaft, and second turn are rotatably equipped in the second rotary axis groove
It is extended at the top of axis outside the second rotary axis groove, top and the support rod of the second shaft are welded and fixed, and fixation is arranged in the second shaft
There is the first angular wheel, rotary shaft through hole is offered on the inner wall of groove side, third shaft is rotatably equipped in rotary shaft through hole, and
The both ends of third shaft all extend to outside rotary shaft through hole, and one end that third shaft is located in groove is fixedly installed with the second conical tooth
Wheel, the second angular wheel, the second angular wheel is meshed with the first angular wheel, third shaft far from the second angular wheel one
End is fixedly installed with third gear, and support column is fixedly installed with the second servo motor, the second servo close to the side of third gear
The 4th gear is fixedly installed on the output shaft of motor, the 4th gear and third gear are wound with same second belt jointly.
Preferably, it is fixedly installed with kelly in the sliding slot, support column is slidably located on kelly.
Preferably, through-hole is offered on the support column, the inner wall of through-hole is equipped with internal screw thread, and first rotating shaft is equipped with outer
Screw thread, through-hole are threadedly coupled with first rotating shaft.
Preferably, annular groove is offered in the rotary shaft through hole, fixing sleeve is equipped with annular fixture block, annular snap in third shaft
Block and annular groove are rotatablely connected.
Preferably, it is arranged with first bearing in the first rotating shaft slot, first bearing is fixedly mounted in first rotating shaft.
Preferably, annular spacing groove is offered on the groove, limited block is welded on support rod, and limited block and annular limit
Position slot rotation connection.
Preferably, it is arranged with second bearing in second rotary axis groove, second bearing is fixedly mounted in the second shaft.
Preferably, motor slot is offered at the top of the fixing seat, first servo motor is fixedly mounted in motor slot.
Compared with prior art, the beneficial effects of the present invention are: by fixing seat, sliding slot, support base, first rotating shaft slot,
Second rotary axis groove, first rotating shaft, gear grooved, first gear, first servo motor, second gear, the first belt, groove, support
Bar, camera, the second rotary axis groove, the second shaft, the first angular wheel, rotary shaft through hole, third shaft, the second angular wheel,
The cooperation of three gears, the second servo motor, the 4th gear, the second belt, kelly, through-hole, annular groove and annular fixture block, works as needs
When dollying head, firstly, starting first servo motor, the output shaft of first servo motor drives second gear to rotate, and second
Gear drives the rotation of the first belt, and the first belt drives first gear rotation, and first gear drives first rotating shaft rotation, due to branch
On dagger through-hole be with first rotating shaft be threadedly coupled, and support column is slidably located on kelly again, so, first rotating shaft
Rotation will drive support column and slide in sliding slot, and support column drives camera to be moved；
When needing to rotate camera, firstly, the second servo motor of starting, the output shaft of the second servo motor drives the 4th
Gear rotation, the 4th gear drive the rotation of the second belt, and the second belt drives the rotation of third gear, and third gear drives third to turn
Axis rotation, third shaft drive the rotation of the second angular wheel, and the second angular wheel drives the rotation of the first angular wheel, the first taper
Gear drives the second shaft to rotate in the second rotary axis groove, and the second shaft drives support rod rotation, and support rod drives camera to turn
It is dynamic, so as to complete the rotation work of camera；
The present invention has rational design, easy to use, and camera is easy to remove and rotates, and can effectively drop to monitoring system frame
If cost, while avoid monitor damage bring risk, reduce blind area of monitoring, ensure aircraft Normal Take-Off And Landing.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the structural schematic diagram of part A in the present invention；
Fig. 3 is the structural schematic diagram of part B in the present invention；
Fig. 4 is the structural schematic diagram of C portion in the present invention；
Fig. 5 is side view of the invention；
Fig. 6 is the principle of the present invention block diagram；
In figure: 1, fixing seat；2, sliding slot；3, support base；4, first rotating shaft slot；5, the second rotary axis groove；6, first rotating shaft；7,
Gear grooved；8, first gear；9, first servo motor；10, second gear；11, the first belt；12, groove；13, support rod；
14, camera；15, the second rotary axis groove；16, the second shaft；17, the first angular wheel；18, rotary shaft through hole；19, third shaft；
20, the second angular wheel；21, third gear；22, the second servo motor；23, the 4th gear；24, the second belt；25, kelly；
26, through-hole；27, annular groove；28, annular fixture block.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-6 is please referred to, the present invention provides a kind of technical solution: a kind of road in airport monitoring system, including fixing seat 1,
Signal input module, voice module, control unit, power supply module and alarm module, signal input module, voice module, power supply
Module and alarm module are connected with control unit, and the top of fixing seat 1 offers sliding slot 2, and branch is slidably fitted in sliding slot 2
Dagger 3, and the top of support column 3 extends to outside sliding slot 2, sliding slot 2 offers first rotating shaft on the inner wall of 3 side of support column
Slot 4, sliding slot 2 offer the second rotary axis groove 5 on the inner wall far from 3 side of support column, in first rotating shaft slot 4 and the second rotary axis groove 5
It is rotatably equipped with the same first rotating shaft 6, the top of fixing seat 1 offers gear grooved 7, and gear grooved 7 and 5 phase of the second rotary axis groove
Connection, first rotating shaft 6 are located at one end fixing sleeve in gear grooved 7 equipped with first gear 8, and the top of fixing seat 1 is fixedly installed with
First servo motor 9 is fixedly installed with second gear 10, second gear 10 and the first tooth on the output shaft of first servo motor 9
Wheel 8 is wound with same first belt 11 jointly, and the top of support column 3 opens up fluted 12, branch is rotatably equipped in groove 12
Strut 13, the top of support rod 13 are fixedly installed with camera 14, the second rotary axis groove 15 are offered on the inner wall of 12 bottom side of groove,
The second shaft 16 is rotatably equipped in second rotary axis groove 15, and the top of the second shaft 16 extends to outside the second rotary axis groove 15, the
The top of two shafts 16 is welded and fixed with support rod 13, and fixing sleeve is equipped with the first angular wheel 17, groove 12 in the second shaft 16
Rotary shaft through hole 18 is offered on the inner wall of side, is rotatably equipped with third shaft 19 in rotary shaft through hole 18, and third shaft 19
Both ends all extend to outside rotary shaft through hole 18, and one end that third shaft 19 is located in groove 12 is fixedly installed with the second angular wheel
20, the second angular wheel 20, the second angular wheel 20 is meshed with the first angular wheel 17, and third shaft 19 is far from the second taper
One end of gear 20 is fixedly installed with third gear 21, and support column 3 is fixedly installed with second close to the side of third gear 21 and watches
Motor 22 is taken, the 4th gear 23, the 4th gear 23 and third gear 21 are fixedly installed on the output shaft of the second servo motor 22
It is wound with same second belt 24 jointly；
Kelly 25 is fixedly installed in sliding slot 2, support column 3 is slidably located on kelly 25, offers through-hole on support column 3
26, the inner wall of through-hole 26 is equipped with internal screw thread, and first rotating shaft 6 is equipped with external screw thread, and through-hole 26 is threadedly coupled with first rotating shaft 6,
Annular groove 27 is offered in rotary shaft through hole 18, fixing sleeve is equipped with annular fixture block 28, annular fixture block 28 and annular in third shaft 19
Slot 27 is rotatablely connected, and is arranged with first bearing in first rotating shaft slot 4, first bearing is fixedly mounted in first rotating shaft 6, groove 12
On offer annular spacing groove, be welded with limited block on support rod 13, limited block and annular spacing groove are rotatablely connected, the second shaft
Second bearing is arranged in slot 15, second bearing is fixedly mounted in the second shaft 16, and the top of fixing seat 1 offers motor
Slot, first servo motor 9 are fixedly mounted in motor slot, pass through fixing seat 1, sliding slot 2, support base 3, first rotating shaft slot 4, second
Rotary axis groove 5, first rotating shaft 6, gear grooved 7, first gear 8, first servo motor 9, second gear 10, the first belt 11, groove
12, support rod 13, camera 14, the second rotary axis groove 15, the second shaft 16, the first angular wheel 17, rotary shaft through hole 18, third turn
Axis 19, third gear 21, the second servo motor 22, the 4th gear 23, the second belt 24, kelly 25, leads to second angular wheel 20
The cooperation in hole 26, annular groove 27 and annular fixture block 28, when needing dollying head 14, firstly, starting first servo motor 9,
The output shaft of first servo motor 9 drives second gear 10 to rotate, and second gear 10 drives the rotation of the first belt 11, the first belt
11 drive first gear 8 to rotate, and first gear 8 drives first rotating shaft 6 to rotate, due to through-hole 26 on support column 3 and first rotating shaft 6
It is threaded connection, and support column 3 is slidably located on kelly 25 again, so, the rotation of first rotating shaft 6 will drive support column
3 slide in sliding slot 2, and support column 3 drives camera 14 to be moved；When needing to rotate camera 14, firstly, starting second
Servo motor 22, the output shaft of the second servo motor 22 drive the rotation of the 4th gear 23, and the 4th gear 23 drives the second belt 24
Rotation, the second belt 24 drive third gear 21 to rotate, and third gear 21 drives third shaft 19 to rotate, and third shaft 19 drives
The rotation of second angular wheel 20, the second angular wheel 20 drive the rotation of the first angular wheel 17, and the first angular wheel 17 drives the
Two shafts 16 rotate in the second rotary axis groove 15, and the second shaft 16 drives support rod 13 to rotate, and support rod 13 drives camera 14
Rotation, so as to complete the rotation work of camera 14；The present invention has rational design, easy to use, camera 14 it is easy to remove and
Rotation, can effectively drop to the cost of monitoring system erection, while avoid monitor damage bring risk, reduce monitoring
Blind area ensures aircraft Normal Take-Off And Landing.
Working principle: in use, signal input module transmits a signal to control unit, power supply module to control unit into
Row power supply, voice module send a signal to control unit, and control unit judges after signal analysis and processing, and control is single
Member control alarm module is alarmed, when needing dollying head 14, firstly, starting first servo motor 9, the first servo electricity
The output shaft of machine 9 drives second gear 10 to rotate, and second gear 10 drives the rotation of the first belt 11, and the first belt 11 drives first
Gear 8 rotates, and first gear 8 drives first rotating shaft 6 to rotate, since through-hole 26 on support column 3 and first rotating shaft 6 are that screw thread connects
It connects, and support column 3 is slidably located on kelly 25 again, so, the rotation of first rotating shaft 6 will drive support column 3 in sliding slot 2
Interior sliding, support column 3 drives camera 14 to be moved, when needing to rotate camera 14, firstly, the second servo motor of starting
22, the output shaft of the second servo motor 22 drives the rotation of the 4th gear 23, and the 4th gear 23 drives the second belt 24 to rotate, and second
Belt 24 drives third gear 21 to rotate, and third gear 21 drives third shaft 19 to rotate, and third shaft 19 drives the second taper
Gear 20 rotates, and the second angular wheel 20 drives the rotation of the first angular wheel 17, and the first angular wheel 17 drives the second shaft 16
It being rotated in the second rotary axis groove 15, the second shaft 16 drives support rod 13 to rotate, and support rod 13 drives camera 14 to rotate, thus
Complete the rotation work of camera 14.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Anyone skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (8)
1. a kind of road in airport monitoring system, including fixing seat (1), signal input module, voice module, control unit, power supply
Module and alarm module, signal input module, voice module, power supply module and alarm module are connected with control unit,
It is characterized in that: being offered sliding slot (2) at the top of the fixing seat (1), is slidably fitted with support column (3) in sliding slot (2), and support
Sliding slot (2) is extended at the top of column (3) outside, sliding slot (2) offers first rotating shaft slot on the inner wall of support column (3) side
(4), sliding slot (2) far from support column (3) side inner wall on offer the second rotary axis groove (5), first rotating shaft slot (4) with second turn
It is rotatably equipped with the same first rotating shaft (6), is offered at the top of fixing seat (1) gear grooved (7), and gear grooved in axial trough (5)
(7) it is connected with the second rotary axis groove (5), first rotating shaft (6) is located at one end fixing sleeve in gear grooved (7) equipped with first gear
(8), it is fixedly installed with first servo motor (9) at the top of fixing seat (1), fixed peace on the output shaft of first servo motor (9)
Equipped with second gear (10), second gear (10) and first gear (8) are wound with same first belt (11), support column jointly
(3) it opens up at the top of fluted (12), is rotatably equipped with support rod (13) in groove (12), the fixed peace in the top of support rod (13)
It equipped with camera (14), is offered the second rotary axis groove (15) on the inner wall of groove (12) bottom side, rotation in the second rotary axis groove (15)
It is equipped with the second shaft (16), and extends to the second rotary axis groove (15) outside at the top of the second shaft (16), the second shaft (16)
Top is welded and fixed with support rod (13), and fixing sleeve is equipped with the first angular wheel (17) in the second shaft (16), groove (12) one
It offers rotary shaft through hole (18), is rotatably equipped with third shaft (19) in rotary shaft through hole (18), and third shaft on the inner wall of side
(19) both ends all extend to rotary shaft through hole (18) outside, and one end that third shaft (19) is located in groove (12) is fixedly installed with
Two angular wheels (20), the second angular wheel (20), the second angular wheel (20) are meshed with the first angular wheel (17), third
Shaft (19) is fixedly installed with third gear (21) far from the one end of the second angular wheel (20), and support column (3) is close to third tooth
The side of wheel (21) is fixedly installed with the second servo motor (22), and the is fixedly installed on the output shaft of the second servo motor (22)
Four gears (23), the 4th gear (23) and third gear (21) are wound with same second belt (24) jointly.
2. a kind of road in airport monitoring system according to claim 1, it is characterised in that: fixed peace in the sliding slot (2)
Equipped with kelly (25), support column (3) is slidably located on kelly (25).
3. a kind of road in airport monitoring system according to claim 1, it is characterised in that: opened up on the support column (3)
Have through-hole (26), the inner wall of through-hole (26) is equipped with internal screw thread, and first rotating shaft (6) is equipped with external screw thread, through-hole (26) and first
Shaft (6) is threadedly coupled.
4. a kind of road in airport monitoring system according to claim 1, it is characterised in that: opened on the rotary shaft through hole (18)
Equipped with annular groove (27), fixing sleeve is equipped with annular fixture block (28) in third shaft (19), annular fixture block (28) and annular groove (27)
Rotation connection.
5. a kind of road in airport monitoring system according to claim 1, it is characterised in that: in the first rotating shaft slot (4)
It is arranged with first bearing, first bearing is fixedly mounted on first rotating shaft (6).
6. a kind of road in airport monitoring system according to claim 1, it is characterised in that: offered on the groove (12)
Annular spacing groove, limited block is welded on support rod (13), and limited block and annular spacing groove are rotatablely connected.
7. a kind of road in airport monitoring system according to claim 1, it is characterised in that: in second rotary axis groove (15)
It is arranged with second bearing, second bearing is fixedly mounted on the second shaft (16).
8. a kind of road in airport monitoring system according to claim 1, it is characterised in that: the top of the fixing seat (1)
Motor slot is offered, first servo motor (9) is fixedly mounted in motor slot.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810982197.1A CN109058702A (en) | 2018-08-27 | 2018-08-27 | A kind of road in airport monitoring system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810982197.1A CN109058702A (en) | 2018-08-27 | 2018-08-27 | A kind of road in airport monitoring system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109058702A true CN109058702A (en) | 2018-12-21 |
Family
ID=64756240
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810982197.1A Pending CN109058702A (en) | 2018-08-27 | 2018-08-27 | A kind of road in airport monitoring system |
Country Status (1)
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| CN (1) | CN109058702A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109140155A (en) * | 2018-10-09 | 2019-01-04 | 郑州森之林电子科技有限公司 | A kind of multi-direction adjustable projection arrangement |
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| WO2018013510A1 (en) * | 2016-07-11 | 2018-01-18 | Dyno Equipment, Inc. | Modular motorized slider system |
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Application publication date: 20181221 |