CN207689673U - A kind of aircraft safety monitoring system and ADS-B receivers - Google Patents
A kind of aircraft safety monitoring system and ADS-B receivers Download PDFInfo
- Publication number
- CN207689673U CN207689673U CN201820064121.6U CN201820064121U CN207689673U CN 207689673 U CN207689673 U CN 207689673U CN 201820064121 U CN201820064121 U CN 201820064121U CN 207689673 U CN207689673 U CN 207689673U
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- Prior art keywords
- ads
- receivers
- connecting rod
- pedestal
- translot
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 19
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 25
- 238000009434 installation Methods 0.000 abstract description 4
- 230000000694 effects Effects 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 5
- 230000001419 dependent effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000007774 longterm Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model discloses a kind of aircraft safety monitoring system and ADS B receivers, it is characterized by comprising GPS antenna, GPS positioning module, airborne sending device, ADS B receivers, display screens, the ADS B receivers include machine box, antenna, pedestal, it is vertically arranged with mounting hole on the pedestal, the connecting rod is mounted in mounting hole, the connecting rod is connect by key-bolt with pedestal, the key-bolt sequentially passes through screw hole, pilot hole, pin hole, translot, and the top of key-bolt is mounted in translot, and magnet is equipped in the translot.Antenna is connect by connecting rod with pedestal, and locating piece is mounted in locating slot, connecting rod rotation and longitudinal direction can be prevented to move down, key-bolt can prevent connecting rod from moving longitudinally upward, and the installation between connecting rod, antenna and pedestal is very firm as a result,.
Description
Technical field
The utility model is related to aircraft technical field, especially a kind of aircraft safety monitoring system and ADS-B are received
Machine.
Background technology
Automatic dependent surveillance broadcast（ADS-B）Be the aircraft operation monitoring technology based on global position system ground/
Empty, sky/air data link.1090MHzES ADS-B (Automatic dependent surveillance broadcast) are a kind of ADS- based on S mode data-link
B technologies, the maximum data bandwidth provided are 1M Bits/s.ADS-B technologies can make to fly in the air for ground-air collaboration monitoring
There is good anticipation between capable aircraft, can find position, course of each aircraft etc. in time, operator can
Make correct judgement in time according to real-time condition.ADS-B technologies can realize ground flying device activity feelings with the cost of very little
The monitoring of condition.ADS-B signal receivers can also be realized other more other than it can realize air to air monitoring, air to surface monitoring
The function of aspect, such as：Aerospace plane can automatic identification mutual alignment, keep personal distance；Ground ATC can be to receiving
Terminal and Route reform aircraft implementing monitoring command；Personal distance is kept between the aircraft of airport surface movement, vehicle, is risen
It is acted on to ground surveillance.And in receiver apparatus, the stability of reception antenna is particularly significant, and shaking, which occurs, in reception antenna then can
Influence the reception of signal.
Utility model content
Purpose of the utility model is to solve the above problem, a kind of aircraft safety monitoring system and ADS- are devised
B receivers, it is characterised in that including GPS antenna, GPS positioning module, airborne sending device, ADS-B receivers, display screen, institute
It states GPS antenna to connect with GPS positioning module, the GPS positioning module is connect with airborne sending device, the airborne sending device
Signal is sent by the ADS-B receivers of digital data chain earthward, the ADS-B receivers are connect with display screen, described
ADS-B receivers include machine box, antenna, pedestal, and the antenna is mounted on the base by connecting rod, is set vertically on the pedestal
It is equipped with mounting hole, mounting hole both sides horizontal symmetrical is equipped with locating slot, and the connecting rod both sides are equipped with locating piece, described fixed
Position block is mounted in locating slot, and the connecting rod is mounted in mounting hole, and the connecting rod is connect by key-bolt with pedestal, institute
It states and is transversely provided with screw hole on pedestal, pin hole is transversely provided in the connecting rod, the connecting rod is equipped with pilot hole, the guiding
Hole is located at one end of pin hole, and the pedestal is equipped with translot, and the translot is located at the other end of pin hole, and the key-bolt is worn successively
Screw hole, pilot hole, pin hole, translot are crossed, and the top of key-bolt is mounted in translot, and flat thin magnet, institute are equipped in the translot
The side for stating flat thin magnet and translot is attracted.
The pilot hole is funnel structure.
It is threadedly coupled between the key-bolt and screw hole.
The base end face is equipped with rubber pad, and the antenna is connect by conducting wire with machine box.
Advantageous effect：
1 the utility model can realize the monitoring to aircraft activity condition；
2 antennas are connect by connecting rod with pedestal, and locating piece is mounted in locating slot, and connecting rod can be prevented to rotate and indulge
To moving down, key-bolt can prevent connecting rod from moving longitudinally upward, as a result, the installation ten between connecting rod, antenna and pedestal
Divide firm；
3 connecting rod tops are attracted with the flat thin magnet in translot, effectively can prevent key-bolt from loosening, long-term holding antenna
It is firm；
The design of 4 pilot holes allows key-bolt more easily to pass through pilot hole and positioning pin, installs more square
Just.
5 rubber pads play the role of anti-skidding and protection and place desktop not by seat wear.
Description of the drawings
Fig. 1 is utility model diagram；
Fig. 2 is the utility model ADS-B receiver schematic diagrames；
In figure, GPS antenna -1, airborne sending device -3, ADS-B receivers -4, antenna -4-1, connects GPS positioning module -2
Extension bar -4-2, pedestal -4-3, mounting hole -4-4, locating slot -4-5, locating piece -4-6, key-bolt -4-7, screw hole -4-8, pin hole -
4-9, pilot hole -4-10, translot -4-11, flat thin magnet -4-12, rubber pad -4-13, machine box -4-14, display screen -5.
Specific implementation mode
Root according to the figure, is further described the utility model：
Embodiment 1
A kind of aircraft safety monitoring system and ADS-B receivers, it is characterised in that including GPS antenna 1, GPS positioning mould
Block 2, airborne sending device 3, ADS-B receivers 4, display screen 5, GPS antenna 1 are connect with GPS positioning module 2, GPS positioning module
2 connect with airborne sending device 3, and airborne sending device 3 sends letter by the ADS-B receivers 4 of digital data chain earthward
Number, ADS-B receivers 4 are connect with display screen 5, and ADS-B receivers 4 include machine box 4-14, antenna 4-1, pedestal 4-3, antenna 4-1
It is connect with machine box 4-14 by conducting wire, antenna 4-1 is mounted on by connecting rod 4-2 on pedestal 4-3, and peace is vertically arranged on pedestal
Hole 4-4 is filled, mounting hole both sides horizontal symmetrical is equipped with locating slot 4-5, and connecting rod both sides are equipped with locating piece 4-6, locating piece installation
In locating slot, connecting rod is mounted in mounting hole, and connecting rod is connect by key-bolt 4-7 with pedestal, is transversely provided on pedestal
Screw hole 4-8 is transversely provided with pin hole 4-9 in connecting rod, and connecting rod is equipped with pilot hole 4-10, and pilot hole is funnel structure, is oriented to
Hole is located at one end of pin hole, and pedestal is equipped with translot 4-11, and translot is located at the other end of pin hole, key-bolt sequentially pass through screw hole,
Pilot hole, pin hole, translot, and the top of key-bolt is mounted in translot, and flat thin magnet 4-12, flat thin magnet and cross are equipped in translot
The side of slot is attracted, and is threadedly coupled between key-bolt and screw hole, base end face is equipped with rubber pad 4-13.
Embodiment 2
When real time monitoring, the signal of the satellite launch received is transmitted to GPS positioning module 2, locating module 2 by GPS antenna 1
Again the position belonging to aircraft is transmitted to airborne sending device 3, airborne sending device 3 by digital data chain earthward
The case where ADS-B receivers 4 send signal, and ADS-B receivers 4 will monitor includes on display screen 5, to realize to aircraft
The monitoring of activity condition.
During use, locating piece 4-6 is mounted in locating slot 4-5 ADS-B receivers, and connecting rod can be prevented to turn
It is dynamic and it is longitudinal move down, key-bolt then can prevent connecting rod 4-2 from moving longitudinally upward, as a result, connecting rod, antenna and pedestal it
Between installation it is very firm, avoid antenna 4-1 from shaking, the flat thin magnet 4-12 in connecting rod top and translot 4-11 is attracted, and can be had
Effect prevents key-bolt from loosening, long-term to keep the firm of antenna.
Finally it should be noted that：The above descriptions are merely preferred embodiments of the present invention, is not limited to this
Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art
For, it still can be with technical scheme described in the above embodiments is modified, or to which part technical characteristic
Equivalent replacement is carried out, within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on,
It should be included within the scope of protection of this utility model.
Claims (4)
1. a kind of aircraft safety monitoring system and ADS-B receivers, it is characterised in that including GPS antenna, GPS positioning module,
Airborne sending device, ADS-B receivers, display screen, the GPS antenna are connect with GPS positioning module, the GPS positioning module
It is connect with airborne sending device, the airborne sending device sends letter by the ADS-B receivers of digital data chain earthward
Number, the ADS-B receivers are connect with display screen, and the ADS-B receivers include machine box, antenna, pedestal, and the antenna passes through
Connecting rod is mounted on the base, and mounting hole is vertically arranged on the pedestal, and mounting hole both sides horizontal symmetrical is equipped with positioning
Slot, the connecting rod both sides are equipped with locating piece, and the locating piece is mounted in locating slot, and the connecting rod is mounted on mounting hole
Interior, the connecting rod is connect by key-bolt with pedestal, and screw hole is transversely provided on the pedestal, is transversely provided in the connecting rod
Pin hole, the connecting rod are equipped with pilot hole, and the pilot hole is located at one end of pin hole, and the pedestal is equipped with translot, described
Translot is located at the other end of pin hole, and the key-bolt sequentially passes through screw hole, pilot hole, pin hole, translot, and the top peace of key-bolt
In translot, flat thin magnet, the side actuation of the flat thin magnet and translot are installed in the translot.
2. a kind of aircraft safety monitoring system according to claim 1 and ADS-B receivers, it is characterised in that：It is described
Pilot hole is funnel structure.
3. a kind of aircraft safety monitoring system according to claim 1 and ADS-B receivers, it is characterised in that：It is described
It is threadedly coupled between key-bolt and screw hole.
4. a kind of aircraft safety monitoring system according to claim 1 and ADS-B receivers, it is characterised in that：It is described
Base end face is equipped with rubber pad, and the antenna is connect by conducting wire with machine box.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820064121.6U CN207689673U (en) | 2018-01-16 | 2018-01-16 | A kind of aircraft safety monitoring system and ADS-B receivers |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820064121.6U CN207689673U (en) | 2018-01-16 | 2018-01-16 | A kind of aircraft safety monitoring system and ADS-B receivers |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207689673U true CN207689673U (en) | 2018-08-03 |
Family
ID=62990875
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820064121.6U Expired - Fee Related CN207689673U (en) | 2018-01-16 | 2018-01-16 | A kind of aircraft safety monitoring system and ADS-B receivers |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207689673U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111121769A (en) * | 2019-12-30 | 2020-05-08 | 中国人民解放军93209部队 | Mechanical scanning portable cooperative target air monitoring equipment and autonomous north correcting method |
| CN111641023A (en) * | 2020-06-10 | 2020-09-08 | 西安电子工程研究所 | A installation base for ADS-B receiving antenna |
-
2018
- 2018-01-16 CN CN201820064121.6U patent/CN207689673U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111121769A (en) * | 2019-12-30 | 2020-05-08 | 中国人民解放军93209部队 | Mechanical scanning portable cooperative target air monitoring equipment and autonomous north correcting method |
| CN111121769B (en) * | 2019-12-30 | 2021-11-16 | 中国人民解放军93209部队 | Mechanical scanning portable cooperative target air monitoring equipment and autonomous north correcting method |
| CN111641023A (en) * | 2020-06-10 | 2020-09-08 | 西安电子工程研究所 | A installation base for ADS-B receiving antenna |
| CN111641023B (en) * | 2020-06-10 | 2021-09-07 | 西安电子工程研究所 | A installation base for ADS-B receiving antenna |
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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: 20180803 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |