CN204270148U - A kind of small-sized individual combat UAS - Google Patents
A kind of small-sized individual combat UAS Download PDFInfo
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- CN204270148U CN204270148U CN201420685793.0U CN201420685793U CN204270148U CN 204270148 U CN204270148 U CN 204270148U CN 201420685793 U CN201420685793 U CN 201420685793U CN 204270148 U CN204270148 U CN 204270148U
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- aircraft
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Abstract
The utility model relates to a kind of small-sized individual combat UAS, comprise aircraft, hand held controller and individual soldier's helmet, aircraft is provided with airborne communication control, on-board controller and airborne task device, carry out wireless connections by Wireless Telecom Equipment between aircraft and hand held controller, between aircraft and individual soldier's helmet, carry out wireless connections by Wireless Telecom Equipment.Aerodynamic arrangement of the present utility model is good, and self stability is excellent, and security is high; Flight-line service ability is strong, is easy to carry; Simple to operate, start setup time short.
Description
Technical field
The utility model belongs to unmanned plane field, especially a kind of small-sized individual combat UAS.
Background technology
In recent years, along with the maturation gradually of unmanned spacecraft technology, and the progress of supporting opertaing device had possessed the feasibility of technical multiple application.Current UAS is normally undertaken unifying to control by ground control station, and single unmanned plane application of going out when executing the task comparatively is short of, and dirigibility is not enough.
The publication technology identical with this patent is not found through preliminary search.
Utility model content
The purpose of this utility model is to overcome the deficiencies in the prior art part, provides a kind of small-sized individual combat UAS.
The utility model solves its technical matters and takes following technical scheme to realize:
A kind of small-sized individual combat UAS, it is characterized in that: comprise aircraft, hand held controller and individual soldier's helmet, aircraft is provided with airborne communication control, on-board controller and airborne task device, wireless connections are carried out by Wireless Telecom Equipment between aircraft and hand held controller, wireless connections are carried out by Wireless Telecom Equipment between aircraft and individual soldier's helmet
(1) concrete structure of aircraft, comprises fuselage, main wing, flank, screw propeller and motor, and the equal symmetrical elasticity of this fuselage both lateral sides is hinged with a wing, is hinged with flank outside wing, and fuselage and wing are 5 sections; In the middle part of the main wing of these aircraft both sides, front end is separately installed with one by the screw propeller of drive and control of electric machine; Screw propeller adopts soft folding screw wing, Automatic-expanding during rotation; Airborne task device is installed in aircraft lower end;
(2) system of hand held controller is that JAUS is compatible, is based on high stability (SuSE) Linux OS;
(3) individual soldier's helmet comprises individual soldier's signal transmission apparatus, processing signals converter, storer, individual soldier's signal converter, video player, image scanning module, audio-frequency module and distance-measuring device, the front end of the helmet is provided with camera by angle controller, the helmet is anterior by support hinge dress video player, the inside of helmet both sides is provided with audio-frequency module, this audio-frequency module comprises microphone and earphone, helmet rear end is fixed with a control enclosure, individual soldier's signal transmission apparatus is installed in this control enclosure, processing signals converter, storer, individual soldier's signal converter and distance-measuring device.
And described airborne task device is photoelectric nacelle, comprises thermal camera, visible light camera and range finder using laser.
And described airborne task device is thermal camera.
Advantage of the present utility model and good effect are:
1, the utility model possesses and vertical takeoff and landing, hand can throw and fly, parachuting, hit the multiple landing modes such as net landing, and have lightweight, collapsible, easy to carry, simple operation and other advantages, easy to carry, individual soldier can carry 2-4 piece of CD-1UAV.
2, the transmission of the utility model real-time high definition image, 12 Zoom Lens, scouting, precision strike, incidentally few advantage is injured.
3, aerodynamic arrangement of the present utility model is good, and self stability is excellent, and security is high; Flight-line service ability is strong, is easy to carry; Simple to operate, start setup time short.
Accompanying drawing explanation
Fig. 1 is system chart of the present utility model;
Fig. 2 is the structural front view of aircraft;
Fig. 3 is the vertical view of Fig. 2;
Fig. 4 is the structural representation of individual soldier's helmet.
Embodiment
Below in conjunction with accompanying drawing, also by specific embodiment, the utility model is described in further detail, and following examples are descriptive, are not determinate, can not limit protection domain of the present utility model with this.
A kind of small-sized individual combat UAS, comprise aircraft, hand held controller and individual soldier's helmet, aircraft is provided with airborne communication control, on-board controller and airborne task device, carry out wireless connections by Wireless Telecom Equipment between aircraft and hand held controller, between aircraft and individual soldier's helmet, carry out wireless connections by Wireless Telecom Equipment.
(1) concrete structure of aircraft is see accompanying drawing 2 and accompanying drawing 3, adopts carbon fibre composite to make, has lightweight feature, can improve load; Comprise fuselage 1, main wing 3, flank 4, screw propeller 2 and motor 5, the equal symmetrical elasticity of this fuselage both lateral sides is hinged with a wing, is hinged with flank outside wing, fuselage and wing are 5 sections, when carrying, the wing of both sides is carried out the folding length that can make and reduce 60%, compact, portable;
In the middle part of the main wing of these aircraft both sides, front end is separately installed with one by the screw propeller of motor 5 drived control, and the motor of these both sides is controlled respectively by on-board controller, motor speed adjustable, can adapt to wider velocity range; Screw propeller adopts soft folding screw wing, and Automatic-expanding during rotation, can not injure wing.
This vehicle technology parameter
Operational distance: 5-10km
CD-1 size: 50*200*620
The span: 1.4m
Operation flight relative height: 50m ~ 1000m
Payload capacity: 0.5kg
Velocity range: 45 ~ 120km/h (sea-level standard air)
Propulsion system: brushless motor two
Cruise speed: 80km/h
Cruise time: 50 scout; Hit 20
Maximum take-off weight: 1500g
Wind loading rating: 4 grades of vertical takeoff and landing, 6 grades are cruised
Airborne task device is installed in aircraft lower end, and the airborne task device of the present embodiment adopts modular design, and be convenient to change, the present embodiment selects following equipment:
1. photoelectric nacelle is a kind of optical device applying gyrocontrol technology; Generally include the multiple optical sensors such as thermal camera, visible light camera and range finder using laser, and there is the function of isolation carrier movement maintenance boresight at inertial space angle stabilization; The various carrying platforms such as helicopter, fixed wing aircraft, unmanned plane, naval vessel and vehicle can be equipped on; Can be used for the military fields such as scouting, aiming, missile guidance, also can be used for the non-military fields such as search and rescue, anti-smuggling, safety, environmental monitoring, forest fire protection.Photoelectric nacelle feature: adopt biaxial stabilization platform, volume is little, lightweight; Adopt low-cost design, the tasks such as forest fire protection, search and rescue, anti-smuggling can be completed; Highgrade integration designs, and control circuit is built-in; Be applicable to the airborne application such as unmanned plane, light aerocraft.
2. thermal camera, visible light camera, ensures to gather image identical with the visible image of human eye;
(2) the system JAUS of hand held controller is compatible, is based on high stability (SuSE) Linux OS, adopts advanced control technology, can be more natural, intuitively, realizes the interaction between people and aircraft;
(3) individual soldier's helmet structure figure is see accompanying drawing 1 and accompanying drawing 4, comprise individual soldier's signal transmission apparatus, processing signals converter, storer, individual soldier's signal converter, video player, image scanning module, audio-frequency module and distance-measuring device, the front end of the helmet 11 is provided with camera 7 by angle controller 8, the helmet is anterior by support hinge dress video player 6, the inside of helmet both sides is provided with audio-frequency module, this audio-frequency module comprises microphone 9 and earphone 10, helmet rear end is fixed with a control enclosure 12, individual soldier's signal transmission apparatus is installed in this control enclosure, processing signals converter, storer, individual soldier's signal converter and distance-measuring device.
Individual soldier's helmet can promote the perception of soldier, help they around environment occur variation time, make adjustment rapidly and dispose.On battlefield, the map etc. in the position of such as enemy army, the orientation of comrade-in-arms and city or house is all the utilizable important information of soldier.The visual helmet of individual soldier arises at the historic moment thus, and it can measuring distance, scans the 3D rendering of building, can also the video that gathers of real-time Transmission unmanned plane.
In addition, it is also furnished with the function of night vision enhancing and enemy and we's identification.The real time data beyond visual range can be collected and provide text message, warning and threat etc. to soldier.Had the help of these information, soldier will obtain additional advantage at reply dangerous situation.
Communication facilities: body always has two antennas, is respectively Data-Link antenna and lower Data-Link antenna.Uplink is responsible for receiving instruction, and lower link is responsible for the information such as transmission of video information, video tracking state, flight parameter.
Transmission of video flow process is introduced: by the high definition Image transmission equipment of aircraft by vision signal real-time Transmission to terrestrial operation device, then by terrestrial operation device, control task order has been reached instruction.
The application of native system
(1) military requirement
When performing combat duty, when not exposing own target, enemy's trend can be grasped, guided by operator, adopt television guided mode offensive attack, accurately rush at target, and blasting in a flash of target can clashed into, or realize type self-destroyed blast when target run overhead.
Look into dozen unmanned plane and can carry high explosive, target can be eliminated rapidly after ignition, can enemy firepower be slackened, as sniper, machine gunner, and mortar etc.
(2) application is scouted
Look into that to beat be aly by electronic reconnaissance equipment on machine, to obtain the UAS of target information, can may be used for battlefield surveillance, for the operation of army provides intelligence, information can be divided into, strategfic reconnaissance, the reconnaissance of a campaign nature and tactical reconnaissance.
(3) application is hit
When performing combat duty, when not exposing own target, enemy's trend can be grasped, guided by operator, adopt television guided mode offensive attack, accurately rush at target, and blasting in a flash of target can clashed into, or realize type self-destroyed blast when target run overhead.
Look into dozen unmanned plane and can carry high explosive, target can be eliminated rapidly after ignition, can enemy firepower be slackened, as sniper, machine gunner, and mortar etc.
Although disclose embodiment of the present utility model and accompanying drawing for the purpose of illustration, but it will be appreciated by those skilled in the art that: in the spirit and scope not departing from the utility model and claims, various replacement, change and amendment are all possible, therefore, scope of the present utility model is not limited to the content disclosed in embodiment and accompanying drawing.
Claims (3)
1. a small-sized individual combat UAS, it is characterized in that: comprise aircraft, hand held controller and individual soldier's helmet, aircraft is provided with airborne communication control, on-board controller and airborne task device, carry out wireless connections by Wireless Telecom Equipment between aircraft and hand held controller, between aircraft and individual soldier's helmet, carry out wireless connections by Wireless Telecom Equipment;
(1) concrete structure of aircraft, comprises fuselage, main wing, flank, screw propeller and motor, and the equal symmetrical elasticity of this fuselage both lateral sides is hinged with a wing, is hinged with flank outside wing, and fuselage and wing are 5 sections; In the middle part of the main wing of these aircraft both sides, front end is separately installed with one by the screw propeller of drive and control of electric machine; Screw propeller adopts soft folding screw wing; Airborne task device is installed in aircraft lower end;
(2) individual soldier's helmet comprises individual soldier's signal transmission apparatus, processing signals converter, storer, individual soldier's signal converter, video player, image scanning module, audio-frequency module and distance-measuring device, the front end of the helmet is provided with camera by angle controller, the helmet is anterior by support hinge dress video player, the inside of helmet both sides is provided with audio-frequency module, this audio-frequency module comprises microphone and earphone, helmet rear end is fixed with a control enclosure, individual soldier's signal transmission apparatus is installed in this control enclosure, processing signals converter, storer, individual soldier's signal converter and distance-measuring device.
2. small-sized individual combat UAS according to claim 1, is characterized in that: described airborne task device is photoelectric nacelle, comprises thermal camera, visible light camera and range finder using laser.
3. small-sized individual combat UAS according to claim 1, is characterized in that: described airborne task device is thermal camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420685793.0U CN204270148U (en) | 2014-11-17 | 2014-11-17 | A kind of small-sized individual combat UAS |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420685793.0U CN204270148U (en) | 2014-11-17 | 2014-11-17 | A kind of small-sized individual combat UAS |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204270148U true CN204270148U (en) | 2015-04-15 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420685793.0U Expired - Fee Related CN204270148U (en) | 2014-11-17 | 2014-11-17 | A kind of small-sized individual combat UAS |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104820422A (en) * | 2015-04-20 | 2015-08-05 | 杨珊珊 | Unmanned aerial vehicle |
-
2014
- 2014-11-17 CN CN201420685793.0U patent/CN204270148U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104820422A (en) * | 2015-04-20 | 2015-08-05 | 杨珊珊 | Unmanned aerial vehicle |
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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: 20150415 Termination date: 20181117 |