CN204641507U - A kind of low latitude early warning detection self-propelled vehicle - Google Patents
A kind of low latitude early warning detection self-propelled vehicle Download PDFInfo
- Publication number
- CN204641507U CN204641507U CN201520242768.XU CN201520242768U CN204641507U CN 204641507 U CN204641507 U CN 204641507U CN 201520242768 U CN201520242768 U CN 201520242768U CN 204641507 U CN204641507 U CN 204641507U
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- China
- Prior art keywords
- hatchcover
- assembly
- low latitude
- early warning
- propelled vehicle
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Abstract
Be badly in need of for field, low latitude the problem being applicable to civilian mobile monitoring platform, the utility model provides a kind of low latitude early warning detection self-propelled vehicle, comprises probe assembly, chassis vehicle and equipment shelter; Described equipment shelter is arranged on chassis vehicle; Probe assembly is located in equipment shelter; In addition, equipment shelter is also provided with hatchcover sliding assembly and lifting assembly; During this low latitude early warning detection self-propelled vehicle work, hatchcover sliding assembly is opened, and expose the window at equipment shelter top, probe assembly together stretches out from the window at equipment shelter top with the movable end of lifting assembly subsequently; When this low latitude early warning detection self-propelled vehicle quits work, probe assembly together declines with the movable end of lifting assembly, and hatchcover sliding assembly closes subsequently.Useful technique effect: the utility model can fill up low latitude monitoring dynamics that is that cause is inadequate because existing, civilian low latitude monitoring fixed station is a not enough difficult problem, serves the effect strengthened low latitude early warning detection and ensure flight safety.
Description
Technical field
The utility model belongs to radar equipment technical field, is specifically related to a kind of low latitude early warning detection self-propelled vehicle.
Background technology
At present, country opens gradually the field, low latitude in territorial limits just according to plan.Can predict, the aircraft in field, low latitude will be increasing, ensures low-latitude flying safety, the work of prevention low-latitude flying hidden danger will be day by day serious.In order to strengthen low latitude early warning detection and ensure flight safety, relevant departments have carried out mapping out the work of low latitude early warning detection, but the supervision at fixed test station will be planned and progressively implements, the gathering of the information collected, upload, comprehensive treatment also needs the time to implement and perfect.
For this reason, the mobile monitoring platform that can carry out effective monitoring to field, low latitude is continued on the market, as the useful supplement at fixed test station.
Utility model content
Be badly in need of for field, low latitude the problem being applicable to civilian mobile monitoring platform, the utility model provides a kind of low latitude early warning detection self-propelled vehicle, and its concrete structure is as follows:
A kind of low latitude early warning detection self-propelled vehicle, comprises probe assembly, chassis vehicle 101 and equipment shelter 102; Described equipment shelter 102 is arranged on chassis vehicle 101; Probe assembly is located in equipment shelter 102; In addition, equipment shelter 102 is also provided with hatchcover sliding assembly and lifting assembly;
Have window at the top of equipment shelter 102 and be furnished with hatchcover sliding assembly; Described hatchcover sliding assembly can opening and closing in the horizontal direction;
Lifting assembly is provided with in equipment shelter 102 below hatchcover sliding assembly; Described lifting assembly can vertically be elevated;
Described probe assembly is connected with the movable end of lifting assembly;
During this low latitude early warning detection self-propelled vehicle work, hatchcover sliding assembly is opened, and expose the window at equipment shelter 102 top, probe assembly together stretches out from the window at equipment shelter 102 top with the movable end of lifting assembly subsequently; When this low latitude early warning detection self-propelled vehicle quits work, probe assembly together declines with the movable end of lifting assembly, and hatchcover sliding assembly closes subsequently.
useful technique effect
The utility model can fill up the difficult problem that low latitude monitoring dynamics that is that cause is inadequate because existing, civilian low latitude monitoring fixed station is not enough, serves the effect strengthened low latitude early warning detection and ensure flight safety.
The utility model not only has the basic function of radar monitoring, also has the ability of optoelectronic monitoring concurrently, is the mobile platform simultaneously providing radar monitoring and photoelectric monitor, thus greatly improves the promptness of low latitude early warning detection, reliability, convenience and high efficiency.
Accompanying drawing explanation
Fig. 1 is the part sectional view of the utility model rounding state.
Fig. 2 is the part sectional view of the utility model deployed condition.
Fig. 3 is the structural representation of hatchcover sliding assembly in Fig. 1.
Fig. 4 is the structural representation of radar equipment Lift Part 105 in Fig. 1.
Fig. 5 is the birds-eye view of Fig. 4.
Detailed description of the invention
Now be described with reference to the accompanying drawings constructional feature of the present utility model.
See Fig. 1, a kind of low latitude early warning detection self-propelled vehicle, comprises probe assembly, chassis vehicle 101 and equipment shelter 102; Described equipment shelter 102 is arranged on chassis vehicle 101; Probe assembly is located in equipment shelter 102; In addition, equipment shelter 102 is also provided with hatchcover sliding assembly and lifting assembly;
Have window at the top of equipment shelter 102 and be furnished with hatchcover sliding assembly; Described hatchcover sliding assembly can opening and closing in the horizontal direction;
Lifting assembly is provided with in equipment shelter 102 below hatchcover sliding assembly; Described lifting assembly can vertically be elevated;
Described probe assembly is connected with the movable end of lifting assembly;
During this low latitude early warning detection self-propelled vehicle work, hatchcover sliding assembly is opened, and expose the window at equipment shelter 102 top, probe assembly together stretches out from the window at equipment shelter 102 top with the movable end of lifting assembly subsequently, as shown in Figure 2; When this low latitude early warning detection self-propelled vehicle quits work, probe assembly together declines with the movable end of lifting assembly, and hatchcover sliding assembly closes subsequently, as shown in Figure 1.
See Fig. 1, be respectively provided with 2 in the both sides of chassis vehicle 101 and support leveling assembly; Described support leveling assembly can vertically be elevated; By supporting the levelness of leveling assembly adjustment chassis vehicle 101.
Furtherly, described support leveling assembly is electronic supporting leg 301.
Furtherly, each electronic supporting leg 301 is equipped with level sensor.
See Fig. 2, be provided with supporting leg chock 111 in the bottom of electronic supporting leg 301.
See Fig. 1 and Fig. 2, have 2 windows at the top of equipment shelter 102;
A hatchcover sliding assembly is furnished with at each window place; Wherein, the hatchcover sliding assembly near headstock place is designated as radar equipment cabin hatchcover slippage parts 104, and the hatchcover sliding assembly near tailstock place is designated as optoelectronic monitoring and follows the tracks of cabin hatchcover slippage parts 107;
A lifting assembly is provided with in each beneath window; Wherein, the lifting assembly corresponding with radar equipment cabin hatchcover slippage parts 104 is designated as radar equipment Lift Part 105, is designated as optoelectronic device Lift Part 108 with the lifting assembly that optoelectronic monitoring follows the tracks of cabin hatchcover slippage parts 107 corresponding;
Described probe assembly comprises low latitude early warning radar 106 and optoelectronic monitoring tracking equipment 109; Wherein, low latitude early warning radar 106 is arranged on radar equipment Lift Part 105, and optoelectronic monitoring tracking equipment 109 is arranged on optoelectronic device Lift Part 108.
See Fig. 3, described hatchcover sliding assembly comprises slide rail 401, hatchcover 402 and electric pushrod 403; Wherein, be provided with slide rail 401 at the window place of equipment shelter 102, slide rail 401 is furnished with hatchcover 402; Described hatchcover 402 is connected with one end of electric pushrod 403, and the other end of electric pushrod 403 is connected with equipment shelter 102; Drive hatchcover 402 along slide rail 401 closure or openness by electric pushrod 403.
See Fig. 1, be provided with 2 hatchcover limit switches at each window place of equipment shelter 102, detect hatchcover 402 by hatchcover limit switch and be in open and close state.
See Fig. 4, lifting assembly comprises spiral lift 501 and bearing base 502; Described spiral lift 501 is the frame body of rectangle, as shown in Figure 5; Bearing base 502 is movably connected in spiral lift 501, and moves up and down along the vertical bar of spiral lift 501; Probe assembly is arranged on the top of bearing base 502.
Furtherly, the vertical bar direction along spiral lift 501 is provided with 2 base limit switches, is detected the jacking condition of bearing base 502 by base limit switch.
Claims (10)
1. a low latitude early warning detection self-propelled vehicle, comprises probe assembly, chassis vehicle (101) and equipment shelter (102); Described equipment shelter (102) is arranged on chassis vehicle (101); Probe assembly is located in equipment shelter (102); It is characterized in that: on equipment shelter (102), be also provided with hatchcover sliding assembly and lifting assembly;
Have window at the top of equipment shelter (102) and be furnished with hatchcover sliding assembly; Described hatchcover sliding assembly can opening and closing in the horizontal direction;
Lifting assembly is provided with in equipment shelter (102) below hatchcover sliding assembly; Described lifting assembly can vertically be elevated;
Described probe assembly is connected with the movable end of lifting assembly;
During this low latitude early warning detection self-propelled vehicle work, hatchcover sliding assembly is opened, and expose the window at equipment shelter (102) top, probe assembly together stretches out from the window at equipment shelter (102) top with the movable end of lifting assembly subsequently; When this low latitude early warning detection self-propelled vehicle quits work, probe assembly together declines with the movable end of lifting assembly, and hatchcover sliding assembly closes subsequently.
2. a kind of low latitude according to claim 1 early warning detection self-propelled vehicle, is characterized in that: be respectively provided with 2 in the both sides of chassis vehicle (101) and support leveling assembly; Described support leveling assembly can vertically be elevated; By supporting the levelness of leveling assembly adjustment chassis vehicle (101).
3. a kind of low latitude according to claim 2 early warning detection self-propelled vehicle, is characterized in that: described support leveling assembly is electronic supporting leg (301).
4. a kind of low latitude according to claim 3 early warning detection self-propelled vehicle, is characterized in that: on each electronic supporting leg (301), be equipped with level sensor.
5. a kind of low latitude according to claim 3 early warning detection self-propelled vehicle, is characterized in that: be provided with supporting leg chock (111) in the bottom of electronic supporting leg (301).
6. a kind of low latitude according to claim 1 early warning detection self-propelled vehicle, is characterized in that:
2 windows are had at the top of equipment shelter (102);
A hatchcover sliding assembly is furnished with at each window place; Wherein, the hatchcover sliding assembly near headstock place is designated as radar equipment cabin hatchcover slippage parts (104), and the hatchcover sliding assembly near tailstock place is designated as optoelectronic monitoring and follows the tracks of cabin hatchcover slippage parts (107);
A lifting assembly is provided with in each beneath window; Wherein, the lifting assembly corresponding with radar equipment cabin hatchcover slippage parts (104) is designated as radar equipment Lift Part (105), follows the tracks of the corresponding lifting assembly of cabin hatchcover slippage parts (107) be designated as optoelectronic device Lift Part (108) with optoelectronic monitoring;
Described probe assembly comprises low latitude early warning radar (106) and optoelectronic monitoring tracking equipment (109); Wherein, low latitude early warning radar (106) is arranged on radar equipment Lift Part (105), and optoelectronic monitoring tracking equipment (109) is arranged on optoelectronic device Lift Part (108).
7. a kind of low latitude according to claim 1 early warning detection self-propelled vehicle, is characterized in that: described hatchcover sliding assembly comprises slide rail (401), hatchcover (402) and electric pushrod (403); Wherein, be provided with slide rail (401) at the window place of equipment shelter (102), slide rail (401) is furnished with hatchcover (402); Described hatchcover (402) is connected with one end of electric pushrod (403), and the other end of electric pushrod (403) is connected with equipment shelter (102); Drive hatchcover (402) along slide rail (401) closure or openness by electric pushrod (403).
8. a kind of low latitude according to claim 7 early warning detection self-propelled vehicle, is characterized in that: be provided with 2 hatchcover limit switches at each window place of equipment shelter (102), detects hatchcover (402) be in open and close state by hatchcover limit switch.
9. a kind of low latitude according to claim 1 early warning detection self-propelled vehicle, is characterized in that: lifting assembly comprises spiral lift (501) and bearing base (502); The frame body that described spiral lift (501) is rectangle; Bearing base (502) is movably connected in spiral lift (501), and moves up and down along the vertical bar of spiral lift (501); Probe assembly is arranged on the top of bearing base (502).
10. a kind of low latitude according to claim 9 early warning detection self-propelled vehicle, is characterized in that: the vertical bar direction along spiral lift (501) is provided with 2 base limit switches, is detected the jacking condition of bearing base (502) by base limit switch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520242768.XU CN204641507U (en) | 2015-04-21 | 2015-04-21 | A kind of low latitude early warning detection self-propelled vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520242768.XU CN204641507U (en) | 2015-04-21 | 2015-04-21 | A kind of low latitude early warning detection self-propelled vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204641507U true CN204641507U (en) | 2015-09-16 |
Family
ID=54094280
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520242768.XU Expired - Fee Related CN204641507U (en) | 2015-04-21 | 2015-04-21 | A kind of low latitude early warning detection self-propelled vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204641507U (en) |
-
2015
- 2015-04-21 CN CN201520242768.XU patent/CN204641507U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150916 Termination date: 20210421 |