CN206537497U - A kind of aircraft with anticollision control function - Google Patents
A kind of aircraft with anticollision control function Download PDFInfo
- Publication number
- CN206537497U CN206537497U CN201720063266.XU CN201720063266U CN206537497U CN 206537497 U CN206537497 U CN 206537497U CN 201720063266 U CN201720063266 U CN 201720063266U CN 206537497 U CN206537497 U CN 206537497U
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- China
- Prior art keywords
- remote control
- utility
- model
- fin assembly
- controller
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- Expired - Fee Related
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Abstract
The utility model is related to vehicle technology field, more particularly to a kind of aircraft with anticollision control function；The utility model includes body and remote control, and the bottom of body, which is provided with the top of undercarriage, body, is provided with roof limb component, and the afterbody of body is provided with fin assembly, and the head of body is provided with range sensor；Controller and transmitter are provided with body；Fin assembly includes revolving vane and electric rotating machine, and remote control is provided with receiver；In the utility model, controller controls roof limb component and fin assembly control flight, range sensor carries out the distance of reaction with front obstacle, such as sense front obstacle it is closer when, the electric rotating machine of controller control fin assembly is out of service, does not accelerate flight forwards, is sent by transmitter on turn signal to the receiver of remote control, turn is remotely controlled, so as to avoid knocking barrier.
Description
Technical field
The utility model is related to vehicle technology field, more particularly to a kind of aircraft with anticollision control function.
Background technology
Remote-controlled unmanned vehicle refers to the aircraft that can be flown with far distance controlled, and it is a kind of self-powered, by remote control control
Make the small aircraft that is flown, colored telecontrolled aircraft is easily fallen during the landing of conventional telecontrolled aircraft, be allowed to surface and leave fall
Trace, and easily damage internals, not easy-maintaining or replacing, so that the use time of telecontrolled aircraft is too short.
Patent name is a kind of telecontrolled aircraft（Publication No. CN204319765U）Chinese utility model patent, disclose
A kind of telecontrolled aircraft, including fuselage, two wings and tail, two wings are respectively symmetrically fixedly installed on the side of fuselage two, tail
The rear portion of fuselage is fixedly installed on, protecting bin is fixedly installed in the lower-end rear portion of fuselage, receiver of remote-control sytem is fixedly installed on guarantor
Protect in storehouse, fuselage afterbody is provided with propeller groove, motor is fixedly installed on the front end of propeller groove, and on fuselage, electricity
Propeller on machine output shaft is arranged in propeller groove, is fixedly installed respectively in the front lower ends of fuselage and the lower end of protecting bin
There are multiple V-type landing chassis, a line of multiple V-type landing chassis is respectively fixedly disposed under the front lower ends and protecting bin of fuselage
On end face；The telecontrolled aircraft internal structure is more complicated, and whard to control, barrier is easily knocked, without collision prevention function.
The content of the invention
Described above in order to overcome the shortcomings of, the purpose of this utility model is to provide a kind of flying with anticollision control function
Row device, its is simple in construction, by controlling fin assembly to be slowed down, and sends pre-warning signal, is turned round, it is to avoid collision.
The technical scheme in the invention for solving the technical problem is：
A kind of aircraft with anticollision control function, wherein, including body and remote control, the bottom of the body is set
There are the roof limb component being provided with the top of undercarriage, the body for controlling the body to carry out sporting flying, the body
Afterbody be provided with fin assembly for controlling the body to carry out accelerated motion forward, the head of the body be provided with away from
From sensor；The controller of interconnection and the transmitter for transmission signal to the remote control are provided with the body；
The fin assembly includes revolving vane and electric rotating machine, and the controller is respectively by wire and the electric rotating machine, described
Roof limb component is connected；The remote control is provided with the receiver of the signal for receiving the transmitter transmitting.
As a kind of improvement of the present utility model, the roof limb component includes propeller blade and main motor, the main motor
It is connected by wire with the controller.
As further improvement of the utility model, the head of the body, which is provided with camera, the remote control, to be set
It is equipped with display screen.
Further improved as of the present utility model, the alarm dress for alarm is provided with the remote control
Put.
Further improved as of the present utility model, the warning device includes indicator lamp and alarming horn.
In the utility model, controller control roof limb component and fin assembly control flight, range sensor carry out with
The distance of reaction of front obstacle, when such as sensing front obstacle is closer, the electric rotating machine of controller control fin assembly stops
Only run, do not accelerate flight forwards, sent by transmitter on turn signal to the receiver of remote control, be remotely controlled and turn
It is curved, so as to avoid knocking barrier；The utility model is simple in construction, by controlling fin assembly to be slowed down, and sends early warning
Signal, is turned round, it is to avoid collision.
Brief description of the drawings
For ease of explanation, the utility model is described in detail by following preferred embodiments and accompanying drawing.
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the internal structure block diagram of body of the present utility model；
Reference：1- bodies, 11- undercarriages, 12- roof limb components, 121- propeller blades, 122- main motors, 13- empennages
Component, 131- revolving vanes, 132- electric rotating machines, 14- range sensors, 15- controllers, 17- cameras, 2- remote controls,
21- receivers.
Embodiment
In order that the purpose of this utility model, technical scheme and advantage are more clearly understood, below in conjunction with accompanying drawing and implementation
Example, the utility model is further elaborated.It should be appreciated that specific embodiment described herein is only to explain
The utility model, is not used to limit the utility model.
It should be noted that in the case where not conflicting, the feature in embodiment and embodiment in the utility model can
To be mutually combined.
In description of the present utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " on ", " under ",
The orientation or position relationship of the instruction such as "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of description the utility model and simplifies description, rather than indicate
Or imply that the device or element of meaning must have specific orientation, with specific azimuth configuration and operation, therefore be not understood that
For to limitation of the present utility model.In addition, term " first ", " second " etc. are only used for describing purpose, and it is not intended that indicating
Or imply relative importance or the implicit quantity for indicating indicated technical characteristic.Thus, " first ", " second " etc. are defined
Feature can express or implicitly include one or more this feature.In description of the present utility model, unless separately
It is described, " multiple " are meant that two or more.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly
Connection；Can be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected to by intermediary,
It can be the connection of two element internals.For the ordinary skill in the art, on being understood by concrete condition
State concrete meaning of the term in the utility model.
As shown in figure 1, a kind of aircraft with anticollision control function of the present utility model, including body 1 and remote control
2。
The bottom of body 1 is provided with undercarriage 11, and the top of body 1 is provided with for controlling body 1 to carry out sporting flying
Roof limb component 12, the afterbody of body 1 is provided with the fin assembly 13 for controlling body 1 to carry out accelerated motion forward, body 1
Head be provided with range sensor 14.
The controller 15 of interconnection and the transmitter for transmission signal to remote control 2 are provided with body 1.
Fin assembly 13 includes revolving vane 131 and electric rotating machine 132, and controller 15 passes through wire and electric rotating machine respectively
131st, roof limb component 12 is connected.
Remote control 2 is provided with the receiver 21 of the signal for receiving transmitter transmitting.
In the utility model, the control roof limb of controller 15 component 12 and the control flight of fin assembly 13, range sensor
14 carry out the distance of reaction with front obstacle, when such as sensing front obstacle is closer, the control fin assembly 13 of controller 15
Electric rotating machine 132 it is out of service, not forwards accelerate flight, pass through transmitter send turn signal to remote control 2 reception
On device 21, turn is remotely controlled, so as to avoid knocking barrier.
The utility model provides a kind of embodiment of roof limb component 12, and roof limb component 12 includes propeller blade 121 and main
Motor 122, main motor 122 is connected by wire with controller 15.
In order to which the utility model can carry out high-altitude shooting, the head of body 1, which is provided with camera 17, remote control 2, to be set
Display screen is equipped with, is easy to high-altitude to shoot, view is easy on remote control 2.
In order to preferably play remote control 2 to be provided with the alarm dress for alarm in danger early warning, remote control 2
Put, further, warning device includes indicator lamp and alarming horn.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
Any modifications, equivalent substitutions and improvements made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (1)
1. a kind of aircraft with anticollision control function, it is characterised in that including body and remote control, the bottom of the body
The roof limb component being provided with the top of undercarriage, the body for controlling the body to carry out sporting flying is provided with, it is described
The afterbody of body is provided with the fin assembly for controlling the body to carry out accelerated motion forward, and the head of the body is set
There is range sensor；The controller of interconnection and the transmitting for transmission signal to the remote control are provided with the body
Device；The fin assembly includes revolving vane and electric rotating machine, and the controller passes through wire and the electric rotating machine, institute respectively
State the connection of roof limb component；The remote control is provided with the receiver of the signal for receiving the transmitter transmitting；
The roof limb component includes propeller blade and main motor, and the main motor is connected by wire with the controller；
The head of the body is provided with camera, the remote control and is provided with display screen；
The warning device for alarm is provided with the remote control；
The warning device includes indicator lamp and alarming horn.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720063266.XU CN206537497U (en) | 2017-01-19 | 2017-01-19 | A kind of aircraft with anticollision control function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720063266.XU CN206537497U (en) | 2017-01-19 | 2017-01-19 | A kind of aircraft with anticollision control function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206537497U true CN206537497U (en) | 2017-10-03 |
Family
ID=59939882
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720063266.XU Expired - Fee Related CN206537497U (en) | 2017-01-19 | 2017-01-19 | A kind of aircraft with anticollision control function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206537497U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112687200A (en) * | 2021-01-14 | 2021-04-20 | 安徽省东超科技有限公司 | Display device and intelligent lamp pole |
-
2017
- 2017-01-19 CN CN201720063266.XU patent/CN206537497U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112687200A (en) * | 2021-01-14 | 2021-04-20 | 安徽省东超科技有限公司 | Display device and intelligent lamp pole |
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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: 20171003 Termination date: 20190119 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |