CN209521870U - A kind of air firing unmanned plane - Google Patents
A kind of air firing unmanned plane Download PDFInfo
- Publication number
- CN209521870U CN209521870U CN201822059383.6U CN201822059383U CN209521870U CN 209521870 U CN209521870 U CN 209521870U CN 201822059383 U CN201822059383 U CN 201822059383U CN 209521870 U CN209521870 U CN 209521870U
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- China
- Prior art keywords
- unmanned plane
- unit
- air firing
- automatic
- control unit
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Abstract
The utility model relates to a kind of air firing unmanned planes, including rotor wing unmanned aerial vehicle and the rotatable gunnery system being mounted on the rotor wing unmanned aerial vehicle, the gunnery system includes two pistols, IR pointer unit and searchlight unit, described two pistols are removably mounted to two sides on the equipment carrying platform of the unmanned plane, the trigger connection automatic cocking lever of the pistol pulls device, the automatic cocking lever pulls device connection automatic control unit, and the automatic control unit is connected with the IR pointer unit and searchlight unit by signal wire.The utility model air firing unmanned plane may be implemented after being aimed at by IR pointer unit target object in the sky by using above technical solution, and automatic trigger trigger is shot to the target object of aiming, can be used for anti-terrorism or anti-riot use.
Description
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of air firing unmanned plane.
Background technique
Unmanned plane militarily can be used for scouting, monitor, the guidance of relayed communications, electronic countermeasure, firepower, combat success assessment, disturbing
It disturbs, lure, (sea) attack, target simulation and early warning etc. over the ground.In civil field, can be used for geodesic survey, meteorological watch,
Urban environment detection, earth resource exploration and forest fire protection etc..Therefore, the small-sized nothing of detectable, search and Tracking Ground Targets
The man-machine growth requirement for complying with military and civilian, has broad application prospects, especially in military field, unmanned plane oneself through obtaining
Large-scale development, and the trend of substituted someone's fighter plane.In all previous fight that this year comes, unmanned plane passes through network number
It plays an increasingly important role according to chain, so that unmanned plane becomes more and more important and dashes forward under the background of Modern Information war
Out.However existing unmanned plane is still further improved in Military Application.
Utility model content
It provides utility model aims to solve above-mentioned technical problem a kind of configured with automatic fire system
Air firing unmanned plane.
To achieve the above objectives, the present invention adopts the following technical solutions:
A kind of air firing unmanned plane including rotor wing unmanned aerial vehicle and is mounted on can be rotated on the rotor wing unmanned aerial vehicle
Gunnery system, the gunnery system include two pistols, IR pointer unit and searchlight unit, described two pistols can
Detachable is mounted on two sides on the equipment carrying platform of the unmanned plane, and the trigger connection automatic cocking lever of the pistol pulls device,
The automatic cocking lever pulls device connection automatic control unit, the automatic control unit and the IR pointer unit and searchlighting
Lamp unit is connected by signal wire.
Radar and folding undercarriage are installed on the body platform of the unmanned plane.
The undercarriage includes the first undercarriage and the second undercarriage.
The automatic control unit is connect with wireless remote control command system wireless signal.
The utility model air firing unmanned plane may be implemented in the sky by using above technical solution to mesh
After object is marked by the aiming of IR pointer unit, automatic trigger trigger is shot to the target object of aiming, can be used for anti-terrorism or anti-
It is sudden and violent to use.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of air firing unmanned plane provided by the embodiment of the utility model.
Specific embodiment
In the following, being further described in conjunction with substantive distinguishing features and advantage of the example to the utility model, but this is practical new
Type is not limited to listed embodiment.
It is shown in Figure 1, a kind of air firing unmanned plane, including rotor wing unmanned aerial vehicle 100 and be installed in rotation on
Rotatable gunnery system on the rotor wing unmanned aerial vehicle, the gunnery system include two pistols 5, IR pointer unit 7 with
And searchlight unit 6, described two pistols are removably mounted to two sides on the equipment carrying platform of the unmanned plane, the hand
The trigger 9 of rifle connects automatic cocking lever and pulls device 10, and the automatic cocking lever is pulled device connection automatic control unit and (is set on body not
Show), the automatic control unit is connected with the IR pointer unit and searchlight unit by signal wire.
The gunnery system is mounted in rotatable mechanism, and the rotatable mechanism is mounted on the body of the unmanned plane
On, in this way, by the signal according to the automatic control unit, may be implemented to control the rotatable mechanism by control signal around
On central axial or it is rotated down certain angle, realizes the realization with respect to the horizontal plane shot upward or downward.
The rotatable mechanism can be connected with the automatic control unit, receive the rotation control of the automatic control
Information processed carries out the rotation of corresponding direction or angular dimension, to realize the downward of gunnery system or tilt down, realizes angle
Spend the function of control.
When specific installation, the pikestaff 8 of the pistol fixes installation by multiple limited posts 11, and automatic cocking lever is pulled
Device 10, which is located at 9 side of trigger and is in contact with trigger 9, to be connect.
The automatic cocking lever pulls device 10 after receiving the triggering trigger signal of the automatic control unit, can make similar
In the movement of manpower cocking backward, to realize that shooting is realized in trigger triggering.
Wherein, in the utility model, radar 3 and folding undercarriage 4 are installed on the body platform of the unmanned plane.
The undercarriage 4 can be connected by electric folding device with body, be folded up when taking off in shape shown in Fig. 1
State, and put down falling, it is supported on ground or supporter, realizes the support to unmanned plane.
It is connected and composed specifically, the undercarriage 4 can be by two supporting leg such as U-shapes with certain radian,
It can be using other structures, it is specific unlimited.
Specifically, the undercarriage includes the first undercarriage and the second undercarriage in the utility model, it is oppositely arranged on nothing
The two sides of man-machine body.
Wherein, the automatic control unit is connect with wireless remote control command system wireless signal.
It should be noted that corresponding space is reserved between described two pistols in the utility model, described in installation
Searchlight unit 6, the IR pointer unit 7 are mounted on the top position of the searchlight unit 6.
The utility model unmanned plane can unmanned plane as shown in Figure 1, by flight support part 1, (flight support part 1 be can be
Upward outwardly angled sections with connection horizontal part, the upward outwardly angled sections include the first rake and the second inclination
The body of portion, horizontal part and unmanned plane is connected to a fixed) rotor 2 is installed, the rotor wing unmanned aerial vehicle of other structures can also be used,
It is specific unlimited.
The utility model air firing unmanned plane may be implemented in the sky by using above technical solution to mesh
After object is marked by the aiming of IR pointer unit, automatic trigger trigger is shot to the target object of aiming, can be used for anti-terrorism or anti-
It is sudden and violent to use.
The above is only the preferred embodiment of the utility model, it is noted that for the common skill of the art
For art personnel, without departing from the principle of this utility model, several improvements and modifications can also be made, these improve and
Retouching also should be regarded as the protection scope of the utility model.
Claims (4)
1. a kind of air firing unmanned plane, which is characterized in that including rotor wing unmanned aerial vehicle and be mounted on the rotor wing unmanned aerial vehicle
On rotatable gunnery system, the gunnery system include two pistols, IR pointer unit and searchlight unit, it is described
Two pistols are removably mounted to two sides on the equipment carrying platform of the unmanned plane, and the trigger connection of the pistol is pulled automatically
Machine pulls device, and the automatic cocking lever pulls device connection automatic control unit, the automatic control unit and the IR pointer list
Member and searchlight unit are connected by signal wire.
2. air firing unmanned plane according to claim 1, which is characterized in that installed on the body platform of the unmanned plane
There are radar and folding undercarriage.
3. air firing unmanned plane according to claim 2, which is characterized in that the undercarriage include the first undercarriage with
Second undercarriage.
4. air firing unmanned plane according to claim 3, which is characterized in that the automatic control unit and wireless remote control
The connection of command system wireless signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822059383.6U CN209521870U (en) | 2018-12-10 | 2018-12-10 | A kind of air firing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822059383.6U CN209521870U (en) | 2018-12-10 | 2018-12-10 | A kind of air firing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209521870U true CN209521870U (en) | 2019-10-22 |
Family
ID=68226314
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822059383.6U Expired - Fee Related CN209521870U (en) | 2018-12-10 | 2018-12-10 | A kind of air firing unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209521870U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113716050A (en) * | 2021-09-26 | 2021-11-30 | 湖南数军物联网科技有限公司 | Automatic shooting unmanned aerial vehicle and unmanned on duty system |
-
2018
- 2018-12-10 CN CN201822059383.6U patent/CN209521870U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113716050A (en) * | 2021-09-26 | 2021-11-30 | 湖南数军物联网科技有限公司 | Automatic shooting unmanned aerial vehicle and unmanned on duty system |
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Legal Events
| 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: 20191022 Termination date: 20201210 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |