CN207029535U - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
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- CN207029535U CN207029535U CN201720121022.2U CN201720121022U CN207029535U CN 207029535 U CN207029535 U CN 207029535U CN 201720121022 U CN201720121022 U CN 201720121022U CN 207029535 U CN207029535 U CN 207029535U
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- unmanned plane
- gas port
- rotor mechanism
- propeller
- carburetor
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Abstract
The utility model provides a kind of unmanned plane, and the unmanned plane includes rotor mechanism, fuel tank, and the rotor mechanism includes propeller, collection gas port and carburetor, and the Plane of rotation of the propeller is vertical with the direction of the collection gas port；The air above the collection gas port of Plane of rotation is accelerated to enter carburetor during the propeller rotation.The Plane of rotation for stating propeller is vertical with the direction of the collection gas port；The air above the collection gas port of Plane of rotation is accelerated to enter carburetor during the propeller rotation, the amount for admitting air into carburetor is bigger, gasoline can effectively be mixed with air, effectively improve the efficiency of gasoline combustion, engine acceleration and deceleration respond faster, emission is reduced, environmental protection and energy saving.
Description
Technical field
Mechanical equipment technical field is the utility model is related to, more particularly to a kind of unmanned plane.
Background technology
At present, unmanned air vehicle technique is one of focus technology of science-and-technology enterprise research, and from the perspective of the energy, unmanned plane can
Length when mixing unmanned plane, electronic unmanned plane environmental protection to be divided into the dynamic unmanned plane of electronic unmanned plane, oil and oil electricity, but continuing a journey, oil
Although dynamic unmanned plane is using traditional fossil fuel, welcomed by the people because continuation of the journey duration is long, existing oil moves nobody
The intake method of machine with the following drawback that：Air inflow is inadequate, and intake resistance is big, and atomizing effect is bad, and fuel particles are thick.Combustion
Burn insufficient, exhaust emissions is not up to standard.
Utility model content
In view of the above problems, it is proposed that the utility model overcomes above mentioned problem to provide one kind or solved at least in part
A kind of certainly unmanned plane of above mentioned problem.
In order to solve the above problems, the utility model discloses a kind of unmanned plane, the unmanned plane includes rotor mechanism, oil
Case, the rotor mechanism include propeller, collection gas port and carburetor, the side of the Plane of rotation of the propeller and the collection gas port
To vertical；The air above the collection gas port of Plane of rotation is accelerated to enter carburetor during the propeller rotation.
Preferably, the rotor mechanism includes venturi accelerating tube, nanofilter, intake elbow, the collection gas port, institute
Venturi accelerating tube, the nanofilter, the intake elbow and the carburetor is stated from top to bottom to be sequentially connected；Air adds
Speed enters the collection gas port, is again speeded up by the venturi accelerating tube, then passes through the nanofilter filtering micronic dust, warp
Carburetor is entered by the intake elbow.
Preferably, there is steering wheel in the envisaged underneath of carburetor；The steering wheel passes through control to change the aperture of air throttle
The aperture of air throttle further controls air inflow, that is, controls the rotating speed size of unmanned plane.
Preferably, the rotor mechanism includes crankcase, bent axle and cylinder head, and the propeller is connected with bent axle；The song
Axle position is in the center of crankcase；Described crankcase the right and left is connected with cylinder head respectively, and the crankcase and cylinder head are bearing
Load.
Preferably, the rotor mechanism also includes blast pipe, and the cylinder head is connected with the blast pipe；The blast pipe is used
To discharge waste gas.
Preferably, the unmanned plane includes medicine-chest.
Preferably, the unmanned plane includes six rotor mechanisms or four rotor mechanisms or 2N rotor mechanism, wherein, N
For positive integer.
Preferably, the unmanned plane includes battery and ECU.
Preferably, the unmanned plane includes frame and undercarriage.
Preferably, six rotor mechanisms or four rotor mechanisms are separately fixed at the end of the frame；Described six
Individual rotor mechanism or four rotor mechanisms are providing power；
The frame is fixedly arranged above battery and ECU；The ECU is providing the circuit control of unmanned plane
Function processed；
The bottom center of the frame is fixed with medicine-chest and fuel tank；The medicine-chest to store medicine, the fuel tank to
Store fuel oil.
The utility model includes advantages below：
In the embodiment of the present invention, the unmanned plane includes rotor mechanism, fuel tank, and the rotor mechanism includes propeller, collection
Gas port and carburetor, the Plane of rotation of the propeller is vertical with the direction of the collection gas port, and the propeller accelerates when rotating
Air above the collection gas port of Plane of rotation enters carburetor, and air accelerates into the collection gas port, passes through the text
Accelerating tube is again speeded up in mound, then by the nanofilter filtering micronic dust, enters carburetor via the intake elbow,
Atomization is carried out in carburetor with the gasoline from fuel tank to mix, there is provided power, the Plane of rotation of the propeller and the gas collection
The direction of mouth is vertical；The air above the collection gas port of Plane of rotation is accelerated to enter carburetor during the propeller rotation,
It is bigger to admit air into the amount of carburetor, gasoline can effectively be mixed with air, effectively improve the efficiency of gasoline combustion,
Engine acceleration and deceleration are responded faster, and emission is reduced, environmental protection and energy saving.
Brief description of the drawings
Fig. 1 is a kind of structured flowchart of rotor mechanism of the present utility model；
Fig. 2 is a kind of structured flowchart of unmanned plane of the present utility model.
Embodiment
To enable above-mentioned purpose of the present utility model, feature and advantage more obvious understandable, below in conjunction with the accompanying drawings and tool
Body embodiment is described in further detail to the utility model.
Reference picture 1, a kind of structured flowchart of rotor mechanism of the present utility model is shown, can specifically be included：
In the utility model embodiment, the rotor mechanism 101 includes propeller 1011, collection gas port 1012, carburetor
1013rd, venturi accelerating tube 1014, nanofilter 1015, intake elbow 1016, the collection gas port 1012, the venturi add
Fast pipe 1014, the nanofilter 1015, the intake elbow 1016 and the carburetor 1013 are from top to bottom sequentially connected；
The Plane of rotation formed during the rotation of the propeller 1011 is vertical with the direction of the collection gas port 1012；Air accelerates into
The collection gas port 1012, is again speeded up, then filtered by the nanofilter 1015 by the venturi accelerating tube 1014
Micronic dust, enter carburetor 1013 via the intake elbow 1016, mist is carried out with the gasoline from fuel tank in carburetor 1013
Change mixing, fully provide power after burning.
In a kind of preferred embodiment of the utility model embodiment, the rotor mechanism 101 also include blast pipe 1017 and
Cylinder head 1018, the cylinder head 1018 are connected with the blast pipe 1017；The blast pipe 1017 is discharging waste gas, it is preferable that
Each rotor mechanism 101 includes two blast pipes 1017, and the quantity of blast pipe can also be three or more, the utility model
Embodiment is not limited specifically the quantity of blast pipe.
In the utility model embodiment, the rotor mechanism 101 includes crankcase 1019 and bent axle 1021, the propeller
1011 are connected with bent axle 1021；The bent axle 1021 is located at the center of crankcase 1019；Described the right and left of crankcase 1019 point
It is not connected with cylinder head 1018, the crankcase 1019 and cylinder head 1018 are to bearing load, crankcase 1019 and the chi of cylinder head 1018
It is very little can be related according to design specification to material, the utility model embodiment need not be limited specifically this.
It is specifically applied in the utility model embodiment, has steering wheel 1020 in the envisaged underneath of carburetor 1013；The rudder
Machine 1020 is used for the aperture for controlling air throttle, by controlling the aperture of air throttle further to control air inflow, that is, controls unmanned plane
Rotating speed size.
In the utility model embodiment, air accelerates into the collection gas port 1012, passes through the venturi accelerating tube
1014 again speed up, then by the filtering micronic dust of nanofilter 1015, enter carburetor via the intake elbow 1016
1013, in carburetor carrying out atomization with the gasoline from fuel tank mixes, there is provided power, the Plane of rotation of the propeller 1011
It is vertical with the direction of the collection gas port 1012；Accelerate the collection gas port 1012 perpendicular to Plane of rotation when the propeller 1011 rotates
The air of top enters carburetor, and it is bigger to admit air into the amount of carburetor, can effectively mix gasoline with air, effectively
Ground improves the efficiency of gasoline combustion, and engine acceleration and deceleration are responded faster, and emission is reduced, environmental protection and energy saving.
Reference picture 2, a kind of structured flowchart of unmanned plane of the present utility model is shown, can specifically be included：
In the utility model embodiment, the unmanned plane includes rotor mechanism 101, fuel tank 102, and the rotor mechanism includes
Propeller 1011, collection gas port 1012 and carburetor 1013, the Plane of rotation of the propeller 1011 and the collection gas port 1012
Direction is vertical；The air above the collection gas port 1012 of Plane of rotation is accelerated to enter carburetion when the propeller 1011 rotates
Device 1013, the fuel oil from fuel tank 102 is in carburetor 1013 and from the abundant mist of the air accelerated into for collecting gas port 1012
Change mixing, fully burning, which more has, efficiently provides power.
Preferably, the unmanned plane includes medicine-chest 107.The unmanned plane includes frame 105 and undercarriage 106, frame
105 size can be related according to design load-bearing weight to material, and the utility model embodiment need not be limited specifically this.
As the utility model embodiment in the specific implementation, the bottom center of the frame 105 be fixed with medicine-chest 107 and
Fuel tank 102；The medicine-chest 107 is to store medicine, and the fuel tank 102 is to store fuel oil, the medicine-chest 107 and fuel tank 102
Depending on specification can be because of the quantity or specification of rotor mechanism 101, the utility model embodiment is not limited specifically this.
In the utility model embodiment in a kind of preferred embodiment, the unmanned plane includes six or four rotor mechanisms
101.Described six or four rotor mechanisms 101 are separately fixed at the end of the frame 105；Described six or four gyroplanes
Structure 101 is providing power；Certainly, the unmanned plane can also be the unmanned plane for including eight or three rotor mechanisms 101, this
Utility model embodiment is not limited specifically the quantity of rotor mechanism.
Apply in the utility model embodiment, the unmanned plane includes battery 103 and ECU 104, described
Frame is fixedly arranged above battery 103 and ECU 104；The ECU 104 controls to provide the circuit of unmanned plane
Function, the battery 103 can include lithium ion battery, can also include ickel-cadmium cell, Ni-H cell etc., and the utility model is real
The species that example is applied for battery does not limit specifically.
The ECU 104 can include CPU or single-chip microcomputer, memory, wire, signal receiving device and signal are sent
Device etc., the utility model embodiment do not limit specifically for ECU.
In the embodiment of the present invention, the unmanned plane includes rotor mechanism 101, fuel tank 102, and the rotor mechanism includes bent axle
1021st, propeller 1011, collection gas port 1012 and carburetor 1013, the Plane of rotation of the propeller 1011 and the collection gas port
1012 direction is vertical；The air above the collection gas port 1012 of Plane of rotation is accelerated to enter when the propeller 1011 rotates
Enter carburetor 1013, using the Plane of rotation of the propeller rotor mechanism vertical with the direction of the collection gas port, improve nothing
Man-machine fuel oil efficiency of combustion, can effectively improve flight efficiency, more energy-conserving and environment-protective.
Finally, it is to be noted that, herein, such as first and second or the like relational terms be used merely to by
One entity or operation make a distinction with another entity or operation, and not necessarily require or imply these entities or operation
Between any this actual relation or order be present.Moreover, term " comprising ", "comprising" or its any other variant meaning
Covering including for nonexcludability, so that process, method, article or terminal device including a series of elements are not only wrapped
Those key elements, but also the other element including being not expressly set out are included, or is also included for this process, method, article
Or the key element that terminal device is intrinsic.In the absence of more restrictions, wanted by what sentence "including a ..." limited
Element, it is not excluded that other identical element in the process including the key element, method, article or terminal device also be present.
Above to a kind of unmanned plane provided by the utility model, it is described in detail, it is used herein specifically individual
Example is set forth to principle of the present utility model and embodiment, and the explanation of above example is only intended to help and understands this reality
With new method and its core concept；Meanwhile for those of ordinary skill in the art, according to thought of the present utility model,
There will be changes in specific embodiments and applications, in summary, this specification content should not be construed as to this
The limitation of utility model.
Claims (10)
1. a kind of unmanned plane, the unmanned plane includes rotor mechanism, fuel tank, the rotor mechanism include propeller, collection gas port and
Carburetor, it is characterised in that the Plane of rotation of the propeller is vertical with the direction of the collection gas port；During the propeller rotation
The air above the collection gas port of Plane of rotation is accelerated to enter carburetor.
2. unmanned plane according to claim 1, it is characterised in that the rotor mechanism includes venturi accelerating tube, nanometer
Filter, intake elbow, the collection gas port, the venturi accelerating tube, the nanofilter, the intake elbow and described
Carburetor is from top to bottom sequentially connected；
Air accelerates into the collection gas port, is again speeded up by the venturi accelerating tube, then pass through the nanofilter
Filtering micronic dust, enter carburetor via the intake elbow.
3. unmanned plane according to claim 1 or 2, it is characterised in that have steering wheel in the envisaged underneath of carburetor；The rudder
Machine is used for the aperture for controlling air throttle, by controlling the aperture of air throttle further to control air inflow, that is, controls turning for unmanned plane
Fast size.
4. unmanned plane according to claim 1, it is characterised in that the rotor mechanism includes crankcase, bent axle and cylinder head,
The propeller is connected with crankcase；The bent axle is located at the center of crankcase；Described crankcase the right and left respectively with cylinder head
Connection, the crankcase and cylinder head are to bearing load.
5. unmanned plane according to claim 4, it is characterised in that the rotor mechanism also includes blast pipe, the cylinder head
It is connected with the blast pipe；The blast pipe is discharging waste gas.
6. unmanned plane according to claim 1, it is characterised in that the unmanned plane includes medicine-chest.
7. unmanned plane according to claim 1, it is characterised in that the unmanned plane includes 2N rotor mechanism, wherein, N
For positive integer.
8. unmanned plane according to claim 1, it is characterised in that the unmanned plane includes battery and ECU.
9. unmanned plane according to claim 1, it is characterised in that the unmanned plane includes frame and undercarriage.
10. according to the unmanned plane described in claim 1 or 6 or 7 or 8 or 9, it is characterised in that rotor mechanism is separately fixed at machine
The end of frame；The rotor mechanism is providing power；The frame is fixedly arranged above battery and ECU；It is described automatically controlled
Unit is providing the circuit control function of unmanned plane；The bottom center of the frame is fixed with medicine-chest and fuel tank；The medicine-chest
To store medicine, the fuel tank is storing fuel oil.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720121022.2U CN207029535U (en) | 2017-02-09 | 2017-02-09 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720121022.2U CN207029535U (en) | 2017-02-09 | 2017-02-09 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207029535U true CN207029535U (en) | 2018-02-23 |
Family
ID=61472037
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720121022.2U Active CN207029535U (en) | 2017-02-09 | 2017-02-09 | A kind of unmanned plane |
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| Country | Link |
|---|---|
| CN (1) | CN207029535U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023058721A1 (en) * | 2021-10-07 | 2023-04-13 | 株式会社石川エナジーリサーチ | Flight device |
-
2017
- 2017-02-09 CN CN201720121022.2U patent/CN207029535U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023058721A1 (en) * | 2021-10-07 | 2023-04-13 | 株式会社石川エナジーリサーチ | Flight device |
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| TR01 | Transfer of patent right |
Effective date of registration: 20220425 Address after: 518000 a1311, building 5, Shenzhen Bay science and technology ecological park, No. 26, Gaoxin South Ring Road, high tech Zone community, Yuehai street, Nanshan District, Shenzhen, Guangdong Patentee after: Shenzhen Lingyue Aviation Technology Co.,Ltd. Address before: No. 518000, Longping street, Longping District, Shenzhen, Guangdong Province Patentee before: SHENZHEN CHANGFENG INFORMATION TECHNOLOGY Co.,Ltd. |