CN205469827U - Newly monitor attack unmanned aerial vehicle - Google Patents
Newly monitor attack unmanned aerial vehicle Download PDFInfo
- Publication number
- CN205469827U CN205469827U CN201620223329.9U CN201620223329U CN205469827U CN 205469827 U CN205469827 U CN 205469827U CN 201620223329 U CN201620223329 U CN 201620223329U CN 205469827 U CN205469827 U CN 205469827U
- Authority
- CN
- China
- Prior art keywords
- firing mount
- afterbody
- aerial vehicle
- unmanned aerial
- wheel support
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a newly monitor attack unmanned aerial vehicle, including the unmanned aerial vehicle body, the afterbody firing mount, the middle part firing mount, the wing, unmanned aerial vehicle body middle part both sides all are provided with the wing, the middle part firing mount is all installed to the wing bottom, the afterbody firing mount is installed to unmanned aerial vehicle body afterbody bottom, bottom detector mounting panel is installed to the afterbody avris, top detector mounting panel is installed on anterior top, the rear wheel support is all installed to unmanned aerial vehicle body middle part both sides, the rear wheel is all installed to rear wheel support tip, the front wheel support is installed to unmanned aerial vehicle body front end bottom, the front wheel is installed to front wheel support tip, all install universal ball on bottom detector mounting panel and the top detector mounting panel, the annular is provided with the detector on the universal ball, the inside attack bullet that all is equipped with of afterbody firing mount and middle part firing mount, unmanned aerial vehicle body top is equipped with anti -interference ware. Beneficial effect lies in: adopt universal ball formula detector to carry out real -time supervision to each position environment, coordinate each position to attack the bullet, carry out crushing strike to the enemy.
Description
Technical field
This utility model belongs to fighter plane and controls technical field, is specifically related to one and newly monitors Attack UAV.
Background technology
UAV is called for short unmanned plane, is the most manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself.Without driving on machine
Cabin, but the equipment such as automatic pilot, presetting apparatus is installed.On ground, naval vessels or machine tool remote control station personnel are by the equipment such as radar, to it
Be tracked, position, remote control, remote measurement and Digital Transmission.Can take off as conventional airplane under wireless remotecontrol or launch with booster rocket,
Also can be taken to by machine tool and throw in flight in the air.During recovery, available mode automatic Landing as conventional airplane landing mission, it is possible to used by remote control
Parachute or block reclaim.Can use repeatedly by repetitiousness.Be widely used in aerial reconnaissance, monitor, communicate, antisubmarine, electronic interferences etc..Present is unmanned
Machine is functional single, and composite class is fewer, and the disposal ability pinpointed the problems in time is the poorest, and sense of self-protection is weaker, therefore, promotes one
Newly monitor Attack UAV.
Utility model content
The purpose of this utility model is that provides one newly to monitor Attack UAV to solve the problems referred to above.
This utility model is achieved through the following technical solutions above-mentioned purpose:
One newly monitors Attack UAV, and including unmanned body, afterbody firing mount, middle part firing mount, wing, in the middle part of described unmanned body, both sides are provided with
Described wing, described wing bottom is mounted on described middle part firing mount, and described unmanned body afterbody bottom is provided with described afterbody firing mount, tail edge side
Being provided with bottom detector installing plate, top front is provided with top detector installing plate, and in the middle part of described unmanned body, both sides are mounted on rear wheel support,
Described rear wheel support end is mounted on trailing wheel, and described unmanned body front bottom end is provided with front-wheel support, and described front-wheel support end is provided with front-wheel,
Being mounted on multi-directional ball on described bottom detector installing plate and described top detector installing plate, in described multi-directional ball, annular is provided with detector, institute
Stating and be each equipped with inside afterbody firing mount and described middle part firing mount attacking bullet, described unmanned body top is equipped with suppressor.
In said structure, on described afterbody firing mount and described middle part firing mount, the described attack bullet of assembling can carry out super remote attack, described suppressor to enemy
Can shield hostile electromagnetic interference, described bottom detector installing plate can pass through with the described detector on the detector installing plate of described top
The environment of different directions is monitored by described multi-directional ball in real time.
In order to improve the reliability of monitoring Attack UAV further, in the middle part of described unmanned body, both sides are mounted on rear wheel support, described rear wheel support end
Portion is mounted on trailing wheel, and described unmanned body front bottom end is provided with front-wheel support, and described front-wheel support end is provided with front-wheel.
In order to improve the reliability of monitoring Attack UAV further, described bottom detector installing plate is mounted on the detector installing plate of described top
Multi-directional ball, in described multi-directional ball, annular is provided with detector.
In order to improve the reliability of monitoring Attack UAV further, it is each equipped with inside described afterbody firing mount and described middle part firing mount attacking bullet, described nothing
Human organism top is equipped with suppressor.
Have the beneficial effects that: use universal ball detector that each location circumstances is monitored in real time, better, coordinate each position to attack bullet, to enemy
The destructive strike of Fang Jinhang.
Accompanying drawing explanation
Fig. 1 is the front view of a kind of new monitoring Attack UAV described in the utility model;
Fig. 2 is the side view of a kind of new monitoring Attack UAV described in the utility model.
1, unmanned body;2, multi-directional ball;3, suppressor;4, afterbody firing mount;5, bottom detector installing plate;6, trailing wheel;7, rear wheel support;
8, middle part firing mount;9, bullet is attacked;10, front-wheel support;11, front-wheel;12, top detector installing plate;13, detector;14, wing.
Detailed description of the invention
The utility model is described in further detail below in conjunction with the accompanying drawings:
As Figure 1-Figure 2, one newly monitors Attack UAV, including unmanned body 1, afterbody firing mount 4, middle part firing mount 8, wing 14, described
In the middle part of unmanned body 1, both sides are provided with described wing 14, and described wing 14 bottom is mounted on described middle part firing mount 8, described unmanned body 1
Afterbody bottom is provided with described afterbody firing mount 4, and tail edge side is provided with bottom detector installing plate 5, and top front is provided with top detector and installs
Plate 12, in the middle part of described unmanned body 1, both sides are mounted on rear wheel support 7, and described rear wheel support 7 end is mounted on trailing wheel 6, described unmanned plane
Body 1 front bottom end is provided with front-wheel support 10, and described front-wheel support 10 end is provided with front-wheel 11, and described bottom detector installing plate 5 is with described
Being mounted on multi-directional ball 2 on top detector installing plate 12, in described multi-directional ball 2, annular is provided with detector 13, described afterbody firing mount 4 and institute
Stating internal being each equipped with of middle part firing mount 8 and attack bullet 9, described unmanned body 1 top is equipped with suppressor 3.
In said structure, on described afterbody firing mount 4 and described middle part firing mount 8, the described attack bullet 9 of assembling can carry out super remote attack to enemy, described anti-
Hostile electromagnetic interference can be shielded by interference unit 3, described with on described top detector installing plate 12 of described bottom detector installing plate 5
The environment of different directions can be monitored in real time by detector 13 by described multi-directional ball 2.
In order to improve the reliability of monitoring Attack UAV further, in the middle part of described unmanned body 1, both sides are mounted on rear wheel support 7, and described trailing wheel props up
Frame 7 end is mounted on trailing wheel 6, and described unmanned body 1 front bottom end is provided with front-wheel support 10, before described front-wheel support 10 end is provided with
Wheel 11, described bottom detector installing plate 5 and described top detector installing plate 12 are mounted on multi-directional ball 2, annular in described multi-directional ball 2
Being provided with internal being each equipped with of detector 13, described afterbody firing mount 4 and described middle part firing mount 8 and attack bullet 9, described unmanned body 1 top is equipped with
Suppressor 3.
Of the present utility model ultimate principle, principal character and advantage have more than been shown and described.Skilled person will appreciate that of the industry, this utility model is not
It is restricted to the described embodiments, described in above-described embodiment and description, principle of the present utility model is simply described, without departing from this utility model essence
On the premise of god and scope, this utility model also has various changes and modifications, and these changes and improvements both fall within claimed this utility model model
In enclosing.This utility model claims scope and is defined by appending claims and effect thing thereof.
Claims (4)
1. a new monitoring Attack UAV, it is characterised in that: include unmanned body, afterbody firing mount, middle part firing mount, wing, described unmanned
In the middle part of body, both sides are provided with described wing, and described wing bottom is mounted on described middle part firing mount, and described unmanned body afterbody bottom has been installed
Stating afterbody firing mount, tail edge side is provided with bottom detector installing plate, and top front is provided with top detector installing plate.
One the most according to claim 1 newly monitors Attack UAV, it is characterised in that: in the middle part of described unmanned body, both sides are mounted on
Rear wheel support, described rear wheel support end is mounted on trailing wheel, and described unmanned body front bottom end is provided with front-wheel support, described front-wheel support end
Front-wheel is installed.
One the most according to claim 1 newly monitors Attack UAV, it is characterised in that: described bottom detector installing plate and described top
Being mounted on multi-directional ball on portion's detector installing plate, in described multi-directional ball, annular is provided with detector.
One the most according to claim 1 newly monitors Attack UAV, it is characterised in that: in described afterbody firing mount and described middle part firing mount
Portion is each equipped with attacking bullet, and described unmanned body top is equipped with suppressor.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620223329.9U CN205469827U (en) | 2016-03-22 | 2016-03-22 | Newly monitor attack unmanned aerial vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201620223329.9U CN205469827U (en) | 2016-03-22 | 2016-03-22 | Newly monitor attack unmanned aerial vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
CN205469827U true CN205469827U (en) | 2016-08-17 |
Family
ID=56651793
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201620223329.9U Expired - Fee Related CN205469827U (en) | 2016-03-22 | 2016-03-22 | Newly monitor attack unmanned aerial vehicle |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN205469827U (en) |
-
2016
- 2016-03-22 CN CN201620223329.9U patent/CN205469827U/en not_active Expired - Fee Related
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10137985B2 (en) | Stealth aerial vehicle | |
CN104875885B (en) | A kind of composite aircraft | |
US9952022B2 (en) | Modularized armor structure with unmanned aerial vehicle loaded and armored vehicle using the same | |
CN107161328B (en) | Projectile type disaster rescue and fire extinguishing unmanned aerial vehicle | |
US8973860B2 (en) | Aerial recovery of small and micro air vehicles | |
CN106394865B (en) | Detachable double multi-rotor unmanned aerial vehicles | |
CN106275402B (en) | Detachable four paddles double-vane unmanned plane | |
CN107132547A (en) | A kind of unmanned plane management-control method | |
EP2858899B1 (en) | Aircraft payload apparatus and method | |
CN108750101A (en) | A kind of super maneuver high speed compound unmanned rotary wing aircraft, assembly, assembly and disassembly methods | |
CN205396521U (en) | Alert tear -gas shells unmanned aerial vehicle transmitting system that uses | |
CN106741888B (en) | Bionic unmanned reconnaissance helicopter | |
CN106347694A (en) | Information acquisition system based on near space floating platform | |
CN206427263U (en) | multi-rotor unmanned aerial vehicle undercarriage | |
CN105346710A (en) | Six-rotor unmanned plane | |
CN210433868U (en) | Airborne guidable fire extinguishing bomb | |
CN204916155U (en) | Multipurpose unmanned aerial vehicle | |
CN207763580U (en) | Missile intercept system based on unmanned plane | |
CN205469827U (en) | Newly monitor attack unmanned aerial vehicle | |
CN202449205U (en) | Quickly detached mounting mechanism for tail wing of unmanned aerial vehicle | |
CN211519852U (en) | Throwing rotor wing mechanism of fixed-wing unmanned reconnaissance plane | |
CN106428570A (en) | Unmanned aerial vehicle for spraying pesticide | |
CN210433869U (en) | Airborne guidable gliding cruise fire extinguishing bomb | |
CN109808907A (en) | Autonomous the boat technology of pilotless helicopter | |
Cai et al. | Research on the development process and trend of unmanned aerial vehicle |
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 |
Granted publication date: 20160817 Termination date: 20180322 |
|
CF01 | Termination of patent right due to non-payment of annual fee |