CN208092229U - Low latitude unmanned plane detects radar installations - Google Patents
Low latitude unmanned plane detects radar installations Download PDFInfo
- Publication number
- CN208092229U CN208092229U CN201820318493.7U CN201820318493U CN208092229U CN 208092229 U CN208092229 U CN 208092229U CN 201820318493 U CN201820318493 U CN 201820318493U CN 208092229 U CN208092229 U CN 208092229U
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- column
- rotating box
- unmanned plane
- driven gear
- low latitude
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Abstract
The utility model is related to a kind of low latitude unmanned planes to detect radar installations,Belong to detecting Radar Technology field,It provides a kind of simple in structure,It is easy to use,The position of automatic sensorcraft,The low latitude unmanned plane for collecting unmanned plane during flying data detects radar installations,Used technical solution is that radar is mounted on column,Rotating box is installed on column,Cover board is provided on rotating box,The both sides of rotating box are equipped with shaft,Thermal camera is fixed in shaft,Lifting motor is installed in shaft,Positioning convex platform is installed on column,Rotating box is sleeved on column,And on positioning convex platform,Driven gear is fixed on column,Driven gear is located in rotating box,Rotary electric machine is also equipped in rotating box,Driving gear is installed on the output shaft of rotary electric machine,Driving gear is meshed with driven gear,Lifting motor and rotary electric machine are connected with radar system；The utility model is widely used in low latitude monitoring unmanned.
Description
Technical field
The utility model is related to a kind of low latitude unmanned planes to detect radar installations, belong to detecting Radar Technology field.
Background technology
Unmanned plane is the not manned vehicle manipulated using radio robot and the presetting apparatus provided for oneself.Nobody
Machine is actually the general designation of unmanned vehicle, can be divided into from technical standpoint definition：Unmanned fixed wing aircraft, nobody is vertical
Landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..Compared with manned aircraft, it
Have many advantages, such as that small, low cost, easy to use, low to operational environment requirement, battlefield survival is stronger.With science and technology
It continues to develop, the application of unmanned plane gradually extends from military field to civil field, in security protection, meteorological monitoring, rain making, boat
Empty mine locating, air remote sensing, power-line patrolling, traffic monitoring, news live game coverage, tracking crime, border patrol, marine monitoring, boat
There is the figure of unmanned plane in the fields such as sky protects a forest, the conservation of wildlife, geological mapping.Especially security protection use nobody
Machine mostly uses greatly low latitude unmanned plane, but when being monitored to low latitude unmanned plane, simple being monitored by radar can not be played more
Good monitoring effect.
Utility model content
To solve technical problem of the existing technology, the utility model provide it is a kind of simple in structure, it is easy to use, from
The position of dynamic sensorcraft, the low latitude unmanned plane for collecting unmanned plane during flying data detect radar installations.
To achieve the above object, technical solution used by the utility model is that low latitude unmanned plane detects radar installations, packet
Column and radar are included, radar is mounted on column, rotating box is equipped on the column, cover board is provided on the rotating box,
The both sides of the rotating box are equipped with shaft, and thermal camera is fixed in the shaft, and lifting electricity is equipped in the shaft
Machine is equipped with positioning convex platform on the column, and the rotating box is sleeved on column, and on positioning convex platform, the column
On be fixed with driven gear, the driven gear is located in rotating box, is also equipped with rotary electric machine in the rotating box, described turn
Driving gear is installed on the output shaft of dynamic motor, the driving gear is meshed with driven gear, the lifting motor and turn
Dynamic motor is connected with radar system.
Preferably, it is both provided with mounting hole on the bottom of the rotating box and cover board, axle sleeve is installed in the mounting hole,
Baffle ring is installed on the axle sleeve, positioning protrusion is provided on the axle sleeve, is provided in corresponding inner wall of the hole installing
Locating groove is provided with first pressure bearing, the axle sleeve on the cover board between rotating box bottom axle sleeve and positioning convex platform
Second pressure bearing is installed on baffle ring, washer is installed on the second pressure bearing, locking screw is installed on the washer
It is female.
Preferably, fixed lobe is installed on the column, the driven gear is located on fixed lobe, and with column key
It connects, sleeve is also equipped on the driven gear.
Preferably, it is set with dirt-proof boot on the first pressure bearing and second pressure bearing.
Compared with prior art, the utility model has the following technical effects：The utility model is simple in structure, user
Just, low altitude radar is monitored using radar and thermal camera, can realizes 360 ° of real-time monitoring, and to unmanned plane
The data such as speed, position, direction and image are collected in real time, can fully ensure that the flight safety of low latitude unmanned plane.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the structural schematic diagram of the utility model bottom bracket axle.
Specific implementation mode
In order to make technical problem to be solved in the utility model, technical solution and advantageous effect be more clearly understood, with
Lower combination accompanying drawings and embodiments, the present invention will be further described in detail.It should be appreciated that specific reality described herein
It applies example to be only used to explain the utility model, is not used to limit the utility model.
As shown in Figure 1 and Figure 2, low latitude unmanned plane detects radar installations, including column 1 and radar 2, and radar 2 is mounted on column
On 1, rotating box 3 is installed on column 1, cover board 4 is provided on rotating box 3, the both sides of rotating box 3 are equipped with shaft 5, shaft 5
On be fixed with thermal camera 6, lifting motor 7 is installed in shaft 5, positioning convex platform 8 is installed on column 1, rotating box 3 is set with
On column 1, and on positioning convex platform 8, driven gear 9 is fixed on column 1, driven gear 9 is located in rotating box 3, turns
Be also equipped with rotary electric machine 10 in dynamic case 3, driving gear 11 be installed on the output shaft of rotary electric machine 10, driving gear 11 with from
Moving gear 9 is meshed, and lifting motor 7 and rotary electric machine 10 are connected with radar system.
When in use, radar can monitor the flight position of unmanned plane in real time, then controlled and risen by -- Radar Control System
Motor and rotary electric machine are dropped, controls rotating box left-right rotation and oscilaltion, and then acquire by thermal camera real-time tracking
The flight position image of unmanned plane, and then ensure that unmanned plane during flying is safer, it is easy to operate, it is easy to use.
Wherein, it is both provided with mounting hole 12 on the bottom of rotating box 3 and cover board 4, axle sleeve 13, axis is installed in mounting hole 12
Baffle ring 14 is installed on set 13, positioning protrusion 15 is provided on axle sleeve 13, is provided on 12 inner wall of corresponding mounting hole
Locating groove 16 is provided with first pressure bearing 17 between 3 bottom axle sleeve of rotating box and positioning convex platform 8, the axle sleeve gear on cover board 4
Second pressure bearing 18 is installed on circle, washer 19 is installed on second pressure bearing 18, locking nut is installed on washer 19
20.Using this structure, it can ensure that rotating box rotates more flexible and easy for installation, repair easy to disassemble.
In addition, being equipped with fixed lobe 21 on column 1, driven gear 9 is located on fixed lobe 21, and connects with 1 key of column
It connects, sleeve 22 is also equipped on driven gear 9.Driven gear is fixed reliably, easy for installation.First pressure bearing 17 and second is pressed
Dirt-proof boot 23 is set on power bearing 18, dirt-proof boot can prevent bearing into ash, influence the lubrication of bearing.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
All any modification, equivalent and improvement etc., should all wrap in the utility model model made by within the spirit and principle of utility model
In enclosing.
Claims (4)
1. low latitude unmanned plane detects radar installations, it is characterised in that：Including column and radar, radar is mounted on column, described
Rotating box is installed on column, cover board is provided on the rotating box, the both sides of the rotating box are equipped with shaft, the shaft
On be fixed with thermal camera, lifting motor is installed in the shaft, positioning convex platform, the rotation are installed on the column
Housing-case is fixed with driven gear on column, and on positioning convex platform on the column, the driven gear is located at rotation
In case, it is also equipped with rotary electric machine in the rotating box, driving gear, the master are installed on the output shaft of the rotary electric machine
Moving gear is meshed with driven gear, and the lifting motor and rotary electric machine are connected with radar system.
2. low latitude unmanned plane according to claim 1 detects radar installations, it is characterised in that：The bottom of the rotating box and
It is both provided with mounting hole on cover board, axle sleeve is installed in the mounting hole, baffle ring is installed on the axle sleeve, is set on the axle sleeve
It is equipped with positioning protrusion, locating groove, rotating box bottom axle sleeve and positioning are provided in corresponding inner wall of the hole installing
It is provided with first pressure bearing between boss, second pressure bearing is installed on the axle sleeve baffle ring on the cover board, described second
Washer is installed on pressure bearing, locking nut is installed on the washer.
3. low latitude unmanned plane according to claim 1 detects radar installations, it is characterised in that：It is equipped on the column solid
Fixed protrusion, the driven gear are located on fixed lobe, and are keyed with column, and sleeve is also equipped on the driven gear.
4. low latitude unmanned plane according to claim 2 detects radar installations, it is characterised in that：The first pressure bearing and
It is set with dirt-proof boot on second pressure bearing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820318493.7U CN208092229U (en) | 2018-03-08 | 2018-03-08 | Low latitude unmanned plane detects radar installations |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820318493.7U CN208092229U (en) | 2018-03-08 | 2018-03-08 | Low latitude unmanned plane detects radar installations |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208092229U true CN208092229U (en) | 2018-11-13 |
Family
ID=64061976
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820318493.7U Active CN208092229U (en) | 2018-03-08 | 2018-03-08 | Low latitude unmanned plane detects radar installations |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208092229U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112204416A (en) * | 2019-11-04 | 2021-01-08 | 深圳市大疆创新科技有限公司 | Sensor and movable platform |
-
2018
- 2018-03-08 CN CN201820318493.7U patent/CN208092229U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112204416A (en) * | 2019-11-04 | 2021-01-08 | 深圳市大疆创新科技有限公司 | Sensor and movable platform |
| WO2021087690A1 (en) * | 2019-11-04 | 2021-05-14 | 深圳市大疆创新科技有限公司 | Sensor and movable platform |
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