CN101917583A - Military unmanned aerial vehicle - Google Patents
Military unmanned aerial vehicle Download PDFInfo
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- CN101917583A CN101917583A CN 201010244122 CN201010244122A CN101917583A CN 101917583 A CN101917583 A CN 101917583A CN 201010244122 CN201010244122 CN 201010244122 CN 201010244122 A CN201010244122 A CN 201010244122A CN 101917583 A CN101917583 A CN 101917583A
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- aerial vehicle
- unmanned aerial
- military unmanned
- carrier aircraft
- video signal
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Abstract
The invention discloses a military unmanned aerial vehicle, and aims to provide a military unmanned aerial vehicle with the advantages of simple structure, low manufacturing cost and multiple functions. The structure of the military unmanned aerial vehicle mainly comprises an aerial vehicle carrier which is provided with a camera, a throwing cabin and a video signal transmitting device; and the ground is provided with a corresponding video signal receiving device and a matched display screen. The military unmanned aerial vehicle has the advantages of simple structure, low manufacturing cost, suitability for large-scale equipment, complete function and high applicability.
Description
Technical field
The present invention relates to the aviation aircraft field, particularly relate to a kind of military unmanned aerial vehicle.
Background technology
At present, military unmanned aerial vehicle is considered as extremely important strategic arms by various countries, and it is of a great variety, technical merit is different, and its principle is the presetting apparatus manipulation that utilizes radio robot and provide for oneself mostly, complex structure, manufacturing cost height, and function singleness.
Summary of the invention
The purpose of this invention is to provide a kind of simple in structure, cheap for manufacturing cost and function military unmanned aerial vehicle how.
The technical solution adopted in the present invention is: a kind of military unmanned aerial vehicle, mainly comprise the flight carrier aircraft, it is armoring that described flight carrier aircraft skin is provided with protection, on the flight carrier aircraft camera, throwing position, video signal transmission device are installed, also are provided with corresponding video signals receiving device and suitable display screen on the ground.
The invention has the beneficial effects as follows: simple in structure, cheap for manufacturing cost, be suitable for extensive equipment; Multiple functional, applicability is strong.
Description of drawings
Below in conjunction with drawings and Examples the present invention is described in further detail, but does not constitute any limitation of the invention.
Fig. 1 is the fly structural representation of carrier aircraft part of the present invention;
Fig. 2 is the structural representation of Ground Control part of the present invention.
Embodiment
As shown in Figure 1, present embodiment mainly comprises flight carrier aircraft 1, described flight carrier aircraft 1 skin is provided with protection plate armour 2, on the flight carrier aircraft 1 camera 3, throwing position 4, video signal transmission device 5 is installed, and also is provided with corresponding video signals receiving device 6 and suitable display screen 7 on the ground.During use, flight carrier aircraft 1 is at radio robot and provide for oneself under the control of program and carry out aerial mission, when arriving the appointed area, camera 3 is launched the realtime graphic that photographed by video signal transmission device 5, ground vision signal receiving device 6 is accepted and by display screen 7 image is shown, reaches the purpose of scouting.Meanwhile, in the throwing position 4 on the flight carrier aircraft 1, can also place offensive weapon, realize the enemy is attacked, also can place military supplies and drop support, therefore, the present invention has multi-functionals such as scouting, attack and support.
Flight carrier aircraft 1 among the present invention and radio robot thereof, video signal transmission device 5 and vision signal receiving device 6 are prior art, are not described in detail in this.
Claims (1)
1. military unmanned aerial vehicle, mainly comprise the flight carrier aircraft, it is characterized in that: it is armoring that described flight carrier aircraft skin is provided with protection, on the flight carrier aircraft camera, throwing position, video signal transmission device are installed, also are provided with corresponding video signals receiving device and suitable display screen on the ground.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010244122 CN101917583A (en) | 2010-07-30 | 2010-07-30 | Military unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010244122 CN101917583A (en) | 2010-07-30 | 2010-07-30 | Military unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101917583A true CN101917583A (en) | 2010-12-15 |
Family
ID=43324952
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201010244122 Pending CN101917583A (en) | 2010-07-30 | 2010-07-30 | Military unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101917583A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201000576Y (en) * | 2007-01-26 | 2008-01-02 | 青岛天骄无人机遥感技术有限公司 | Flight control system for unmanned plane |
| CN101609589A (en) * | 2008-06-17 | 2009-12-23 | 侯荣琴 | Multi-frequency image fire detection system |
| CN101650866A (en) * | 2009-09-22 | 2010-02-17 | 华南理工大学 | Fire detecting system applied to unmanned helicopter and fire detecting method thereof |
| CN101746503A (en) * | 2008-12-01 | 2010-06-23 | 厦门市罗普特科技有限公司 | Police reconnaissance aircraft with GPS positioning missile |
-
2010
- 2010-07-30 CN CN 201010244122 patent/CN101917583A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201000576Y (en) * | 2007-01-26 | 2008-01-02 | 青岛天骄无人机遥感技术有限公司 | Flight control system for unmanned plane |
| CN101609589A (en) * | 2008-06-17 | 2009-12-23 | 侯荣琴 | Multi-frequency image fire detection system |
| CN101746503A (en) * | 2008-12-01 | 2010-06-23 | 厦门市罗普特科技有限公司 | Police reconnaissance aircraft with GPS positioning missile |
| CN101650866A (en) * | 2009-09-22 | 2010-02-17 | 华南理工大学 | Fire detecting system applied to unmanned helicopter and fire detecting method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20101215 |