CN206214770U - A kind of aircraft - Google Patents
A kind of aircraft Download PDFInfo
- Publication number
- CN206214770U CN206214770U CN201621232337.6U CN201621232337U CN206214770U CN 206214770 U CN206214770 U CN 206214770U CN 201621232337 U CN201621232337 U CN 201621232337U CN 206214770 U CN206214770 U CN 206214770U
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- CN
- China
- Prior art keywords
- main support
- aircraft according
- motor
- loaded
- cover
- 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
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Abstract
The utility model discloses a kind of aircraft, including main support, motor, battery, connection circuit, camera head.Four angles of the main support have been respectively and fixedly connected with drive installation part, the drive installation part center is equipped with the motor, and propeller is provided with motor output shaft, there is a cover above the main support, cover front end is equipped with pick-up lens, and the main support bottom is provided with dominant control.The camera head is loaded in the cover.The battery is loaded on main support bottom.The dominant control includes：Image pickup and wireless transmission control device, flight control circuit device.The utility model compact conformation, driving force are strong, fuselage is balanced, flight stability is good, and can realize video instantaneous transmission of taking photo by plane.
Description
Technical field
The utility model is related to aircraft, specifically a kind of aeromodelling aerocraft for carrying camera head.
Background technology
Aeromodelling aerocraft typically as manned aircraft, mainly by wing, empennage, fuselage, undercarriage and engine five
Part constitutes.Wing is that aeromodelling aerocraft produces the device of lift in flight, and horizontal stroke when can keep aeromodelling aerocraft flight
Side stabilization.Empennage includes tailplane and vertical tail two parts.Tailplane can keep pitching during aeromodelling aerocraft flight
Stabilization, vertical tail keeps direction stabilization during aeromodelling aerocraft flight.Elevator on tailplane can control model plane to fly
The lifting of device, the heading of the controllable aeromodelling aerocraft of rudder on vertical tail.Fuselage is to join each several part of model
Form a trunk portion for entirety fuselage.Simultaneously necessary control parts, equipment and fuel etc. can be loaded in fuselage.Rise
The device that the frame that falls takes off for aeromodelling aerocraft, lands and parks.An anterior undercarriage, behind each undercarriage in two sides preceding
Bikini, the anterior each undercarriage in two sides, latter one undercarriage is rear bikini.Engine is that aeromodelling aerocraft generation flies
The device of action edge.Modern Aviation model sport is divided into free flight, line manipulation, wireless remotecontrol, emulation and electronic etc. five big
Class.It is divided into again by power mode：The gliding of piston engine, jet engine, rubber-band model aircraft and motorless model
Machine etc..Propeller refers to rotate the device that engine rotation power is converted into propulsive force in atmosphere by blade.Propeller revolves
When turning, blade constantly backward pushes large quantity of air (propulsive medium), and propulsive force is produced on blade.
Aeromodelling aerocraft frame includes undercarriage, and camera head is carried in undercarriage, it is therefore an objective to flown using aeromodelling aerocraft
The image according to needed for is taken the photograph during row.
In the prior art, aeromodelling aerocraft has center convolution frame and spiral horn, also including control board, its structure compared with
It is complicated, flight stability is not good enough.
Utility model content
Technical problem to be solved：The utility model purpose is to provide that a kind of scientific and reasonable for structure, fuselage is balanced, flight
The aerial photography aircraft of good stability.
Technical scheme：A kind of aircraft, including main support, motor, battery, connection circuit, camera head.The main support
Four angles have been respectively and fixedly connected with drive installation part, and the drive installation part center is equipped with the motor, is provided with motor output shaft
Propeller, there is a cover above the main support, cover front end is equipped with pick-up lens, and the main support bottom is provided with master control
Part.
The camera head is loaded in the cover.The battery is loaded on main support bottom.
The dominant control includes：Image pickup and wireless transmission control device, flight control circuit device.
The drive installation part is fixed in four circular arcs at angle of main support with support arm, and the motor is loaded on support arm end
End, the support arm is also connected with support member, and the support member outer end is connected with annular element, and the propeller is in annular element.
Described image is imaged has image transmitting frequency modulation button and image transmitting charactron with wireless transmission control device.
There is power outlet the main support bottom.The main support bottom is also equipped with foot stool.
Beneficial effect：The utility model is by adopting the above-described technical solution, its compact conformation, scientific and reasonable, fuselage are equal
Weighing apparatus, flight stability are good.Due to being mounted with that image pickup and wireless transmission control device can be realized taking photo by plane in aerial photography aircraft
Video instantaneous transmission.
Brief description of the drawings
Fig. 1 is the utility model front view.
Fig. 2 is the utility model rearview.
Fig. 3 is the utility model left view.
Fig. 4 is the utility model right view.
Fig. 5 is the utility model top view.
Fig. 6 is the utility model upward view.
Label is represented in figure：Main support 1, cover 2, pick-up lens 3, support arm 4, motor 5, propeller 6, support member 7, annular
Part 8, battery 9, image transmitting frequency modulation button 10, image transmitting charactron 11, power outlet 12, flight control circuit device 13,
Foot stool 14, image pickup and wireless transmission control device 15, circular arc 16.
Specific embodiment
For the ease of understanding the utility model, the utility model will be described more fully below.The utility model
Give better embodiment.But, the utility model can be realized in many different forms, however it is not limited to be retouched herein
The implementation method stated.On the contrary, the purpose for providing these implementation methods is to make to understand more disclosure of the present utility model
Plus it is thorough comprehensive.
It should be noted that when element is referred to as " connection " another element, it can be directly to another yuan
Part may be simultaneously present centering elements.Unless otherwise defined, all of technologies and scientific terms used here by the article and category
The implication being generally understood that in those skilled in the art of the present utility model is identical.Institute in the description of the invention herein
The term for using is intended merely to describe the purpose of specific embodiment, it is not intended that in limitation the utility model.Made herein
Term " and/or " include the arbitrary and all of combination of one or more related Listed Items.
See Fig. 1-6, a kind of aircraft, including main support 1, motor 5, battery 9, connection circuit, camera head.The shooting
Loaded in the cover 2, the battery 9 is loaded on the bottom of main support 1 to device, and shell and main support, battery 9 can be used to be loaded on shell
It is interior.
1 four angles of the main support have been respectively and fixedly connected with drive installation part, and the drive installation part center is equipped with the motor
5, propeller 6 is installed in motor output shaft, the main support 1 has a cover 2 above, and the front end of cover 2 is equipped with pick-up lens 3.
The bottom of the main support 1 is provided with dominant control.The dominant control includes image pickup and wireless transmission control device
15th, flight control circuit device 13 is constituted.Described image is imaged has image transmitting frequency modulation button with wireless transmission control device 15
10 and image transmitting charactron 11.Dominant control is prior art, is not described further.
In one embodiment, the drive installation part is fixed in 1 four circular arcs at angle 16 of main support, institute with support arm 4
Motor 5 is stated loaded on the end of the support arm 4, the support arm 4 is also connected with support member 7, and the outer end of the support member 7 is connected with annular element
8, the propeller 6 is in annular element 8.Annular element can further assemble rotating wind, increase driving force, and can reduce outside
The adverse effect of wind direction.
In one embodiment, there be power outlet 12 bottom of the main support 1, charges the battery.
In one embodiment, the bottom of main support 1 is also equipped with foot stool 14, is parked for fuselage.
The connection circuit is motor, battery, camera head, image pickup and wireless transmission control device, flight control
Line unit is electrically connected with circuit.
Its course of work：The utility model is matching used wireless receiving and control device.Wireless receiving and control
Device can control propeller by image pickup and wireless transmission control device, the signal transmission of flight control circuit device
Rotating speed and control aircraft heading, and the taking the photograph according to operation of camera head can be controlled, the video image that will be taken the photograph passes to
In wireless receiving and control device.
Charged the battery by power outlet with civil power, by matching used wireless receiving and control device to mixing up image
Transmission frequency modulation button, presses power switch, and propeller starts to airflight, is operated by terrestrial wireless and shakes control, flight control
Line unit receives instruction, and pick-up lens finds required target, and video image passes through image pickup and wireless transmission control device
Pass the wireless receiving and control device on ground back.
Above content is to combine specific preferred embodiment further detailed description of the utility model, it is impossible to
Assert that specific implementation of the present utility model is confined to these explanations.For the ordinary skill of the utility model art
For personnel, without departing from the inventive concept of the premise, some simple deduction or replace can also be made, should all be considered as category
In protection domain of the present utility model.
Claims (8)
1. a kind of aircraft, including main support (1), motor (5), battery (9), connection circuit, camera head, it is characterised in that：
(1) four angle of the main support has been respectively and fixedly connected with drive installation part, and the drive installation part center is equipped with the motor (5), electricity
Propeller (6) is installed, the main support (1) has a cover (2) above, and cover (2) front end is equipped with camera lens in machine output shaft
Head (3), main support (1) bottom is provided with dominant control.
2. a kind of aircraft according to claim 1, it is characterised in that：The camera head is loaded in the cover (2).
3. a kind of aircraft according to claim 1, it is characterised in that：The battery (9) is loaded on main support (1) bottom.
4. a kind of aircraft according to claim 1, it is characterised in that the dominant control includes：Image pickup and wireless biography
Defeated control device (15), flight control circuit device (13).
5. a kind of aircraft according to claim 1, it is characterised in that：The drive installation part is fixed in support arm (4)
The circular arc (16) at (1) four angle of main support, the motor (5) is loaded on the support arm (4) end, and the support arm (4) is also affixed
There is support member (7), support member (7) outer end is connected with annular element (8), and the propeller (6) is in annular element (8).
6. a kind of aircraft according to claim 4, it is characterised in that：Described image is imaged and wireless transmission control device
(15) there are image transmitting frequency modulation button (10) and image transmitting charactron (11).
7. a kind of aircraft according to claim 1, it is characterised in that：There is power outlet main support (1) bottom
(12)。
8. a kind of aircraft according to claim 1, it is characterised in that：Main support (1) bottom is also equipped with pin
Frame (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621232337.6U CN206214770U (en) | 2016-11-17 | 2016-11-17 | A kind of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621232337.6U CN206214770U (en) | 2016-11-17 | 2016-11-17 | A kind of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206214770U true CN206214770U (en) | 2017-06-06 |
Family
ID=58792679
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621232337.6U Expired - Fee Related CN206214770U (en) | 2016-11-17 | 2016-11-17 | A kind of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206214770U (en) |
-
2016
- 2016-11-17 CN CN201621232337.6U patent/CN206214770U/en not_active Expired - Fee Related
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170606 Termination date: 20201117 |