CN206202687U - A kind of smooth power aerial vehicle - Google Patents
A kind of smooth power aerial vehicle Download PDFInfo
- Publication number
- CN206202687U CN206202687U CN201621307103.3U CN201621307103U CN206202687U CN 206202687 U CN206202687 U CN 206202687U CN 201621307103 U CN201621307103 U CN 201621307103U CN 206202687 U CN206202687 U CN 206202687U
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- CN
- China
- Prior art keywords
- fixed
- motor
- aircraft body
- support
- aerial vehicle
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Abstract
The utility model discloses a kind of smooth power aerial vehicle, including aircraft body, control system and power module, the first motor, the first propeller, the second motor, the second propeller, control system is electrically connected with the first motor, the second motor, power module respectively, the both sides that the top of aircraft body is located at the first motor are respectively fixed with a support, and the solar energy electroplax being electrically connected with power module is fixed with the top of support；The bottom of aircraft body is fixed with two and vertically fixes and have resilient support meanss, a plate body is respectively fixed with the top of support meanss, radiator fan is fixed between two boards body, the relay and temperature sensor being electrically connected with control system are fixed with aircraft body, relay is electrically connected with radiator fan.Its advantage is：Energy-saving effect is obvious, good heat dissipation effect, long service life.
Description
Technical field
The utility model is related to a kind of smooth power aerial vehicle.
Background technology
Chinese patent 201520673918.2 discloses a kind of novel agricultural spray unmanned plane, and engine is arranged on unmanned plane
Middle and upper part, engine is provided with propeller I, and engine bottom is provided with power supply, and fixed support, fixed branch are additionally provided with unmanned plane
The end of frame is provided with motor, and propeller II is further disposed on motor, and the bottom of unmanned plane is provided with liquid bag, and liquid bag passes through
The replaceable bottom for being connected to unmanned plane of connector, liquid bag is made up of elastomeric material, and the liquid portion of wrapping is provided with topping up
Mouth and valve inside charging connector, aerating valve mouth are arranged on the side of fluid-filling nozzle, and liquid bag bottom is provided with spray nozzle, on spray nozzle
Control valve is provided with, fixed support bottom is additionally provided with supporting leg, and the further connection support bar in supporting leg bottom, utility model design is closed
Reason, easy to operate, simple structure.But there is problems with the utility model：1st, without solar energy is sufficiently utilized, do not reach
To the effect of energy-conservation；2nd, the control system inside unmanned plane does not take cooling measure so that the service life contracting of control system
It is short.
Utility model content
It is obvious, good heat dissipation effect, long service life that problem to be solved in the utility model is to provide a kind of energy-saving effect
Light power aerial vehicle.
In order to solve the above-mentioned technical problem, the technical solution adopted in the utility model is：A kind of smooth power aerial vehicle, including
Aircraft body, the control system being fixed in the aircraft body and power module, in the top of the aircraft body
Heart position is fixed with the first motor, and the first propeller is fixed with the output shaft of first motor, the aircraft body
Left and right sides outer wall is respectively fixed with a transverse slat, and the second motor, the output of second motor are fixed with the top of the transverse slat
The second propeller is fixed with axle, the control system electrically connects with first motor, the second motor, power module respectively
Connect, it is characterised in that the both sides that the top of the aircraft body is located at first motor are respectively fixed with a support, described
The solar energy electroplax being electrically connected with the power module is fixed with the top of support；The bottom of the aircraft body is fixed with
Two are vertically fixed and have resilient support meanss, and a plate body, two are respectively fixed with the top of the support meanss
Radiator fan is fixed between plate body described in block, be fixed with the aircraft body with the control system be electrically connected with after
Electrical equipment and temperature sensor, the relay are electrically connected with the radiator fan.
Preferably, above-mentioned light power aerial vehicle, wherein being respectively fixed with each angle of the bottom of the aircraft body
One support feet.
Preferably, above-mentioned light power aerial vehicle, wherein the support meanss include being fixed on the aircraft body bottom
The base plate in portion, the support tube being fixed on the base plate, the top board being fixed at the top of the support tube, top and the plate body connect
The column for connecing, is slidably provided with a drive block in the support tube, the bottom of the column through the top board and with it is described
Drive block is connected, and many is fixed with the top of the top board and passes through the drive block and the bar being slidably connected with the drive block
Body, the bottom of the body of rod is connected with the base plate, is located on the body of rod and is arranged with bullet between the top board and drive block
Spring, is located on the body of rod and is arranged with lower spring between the drive block and base plate.
Preferably, above-mentioned light power aerial vehicle, wherein the quantity of the body of rod is two.
Preferably, above-mentioned light power aerial vehicle, wherein the solar energy electroplax is symmetrical centered on the first motor
Set.
It is of the present utility model to have the technical effect that：Solar energy electroplax can be converted solar energy into electrical energy and is stored in
In power module, for the utility model provides electric energy, energy-saving effect is obvious；Temperature sensor being capable of automatic detection aircraft body
Interior temperature and by signal transmission to control system, when preset temperature of the temperature for detecting higher than control system, control system
Radiator fan blowing radiating is automatically controlled, such design automation degree is high, extends the service life of control system；Support dress
Put with elasticity, damping can be played a part of, it is to avoid the shake of radiator fan and cause that aircraft body vibrations are excessive, this
Sample is designed and causes that the utility model is more practical.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the longitudinal sectional view of aircraft body in Fig. 1；
Fig. 3 is the structural representation of support meanss in Fig. 2.
Specific embodiment
Below in conjunction with accompanying drawing, specific embodiment of the present utility model is further described, so that the utility model
Technical scheme be more readily understood and grasp.
As shown in Figure 1, 2, 3, a kind of smooth power aerial vehicle, including aircraft body 1, it is fixed in aircraft body 1
Control system 11 and power module 12, the top center of aircraft body 1 are fixed with the first motor 13, the first motor 13
The first propeller 14 is fixed with output shaft, the left and right sides outer wall of aircraft body 1 is respectively fixed with a transverse slat 15, transverse slat 15
Top be fixed with the second motor 16, the second propeller 17 is fixed with the output shaft of the second motor 16, control system 11 is distinguished
It is electrically connected with the first motor 13, the second motor 16, power module 12.
The both sides that the top of aircraft body 1 is located at first motor are respectively fixed with a support 21, the top of support 21
Portion is fixed with the solar energy electroplax 22 being electrically connected with power module 12, the left and right centered on the first motor 13 of solar energy electroplax 22
It is symmetrical arranged.
The bottom of aircraft body 1 is fixed with two and vertically fixes and have resilient support meanss 3, support dress
The top for putting 3 is respectively fixed with a plate body 4, is fixed with radiator fan 5 between two boards body 4, be fixed with aircraft body 1 with
Relay 51 and temperature sensor 52 that control system 11 is electrically connected with, relay 51 are electrically connected with radiator fan 5.
A support feet 6 wherein is respectively fixed with each angle of the bottom of aircraft body 1, so design facilitates this practicality new
The landing of type.
Wherein support meanss 3 include the base plate 31 for being fixed on the bottom of aircraft body 1, the support tube being fixed on base plate 31
32nd, the top board 33, top at the top of support tube 32 and the column 34 of the connection of plate body 4 are fixed on, are slidably provided with support tube 32
One drive block 35, the bottom of column 34 is connected through top board 33 and with drive block 35, and the top of top board 33 is fixed with two and passes through
Drive block 35 and the body of rod 36 being slidably connected with drive block 35, the bottom of the body of rod 6 are connected with base plate 31, and top board is located on the body of rod 36
Spring 37 is arranged between 33 and drive block 35, is located on the body of rod 36 and is arranged with lower spring between drive block 35 and base plate 31
38, such design structure is firm so that the elastic performance of support meanss 3 is significantly improved.
Certainly, these are only preferred embodiment of the present utility model, it is non-therefore limit to patent of the present utility model
Simple modification and the equivalent structure change for it of scope, all utilization the utility model specifications and schema content institute, all should similarly wrap
It is contained within scope of patent protection of the present utility model.
Claims (5)
1. a kind of smooth power aerial vehicle, including aircraft body, the control system being fixed in the aircraft body and power supply
Module, the top center of the aircraft body is fixed with the first motor, is fixed with the output shaft of first motor
First propeller, the left and right sides outer wall of the aircraft body is respectively fixed with a transverse slat, is fixed with the top of the transverse slat
Second motor, is fixed with the second propeller on the output shaft of second motor, the control system is electric with described first respectively
Machine, the second motor, power module are electrically connected with, it is characterised in that：The top of the aircraft body is located at first motor
Both sides be respectively fixed with a support, be fixed with the top of the support with the power module be electrically connected with solar-electricity
Plate；The bottom of the aircraft body is fixed with two and vertically fixes and have resilient support meanss, the support
A plate body is respectively fixed with the top of device, radiator fan is fixed between two pieces of plate bodys, it is solid in the aircraft body
Surely there are the relay and temperature sensor being electrically connected with the control system, the relay electrically connects with the radiator fan
Connect.
2. smooth power aerial vehicle according to claim 1, it is characterised in that：At each angle of the bottom of the aircraft body
It is respectively fixed with a support feet.
3. smooth power aerial vehicle according to claim 1, it is characterised in that：The support meanss include being fixed on described flying
The base plate of row device body bottom portion, the support tube being fixed on the base plate, the top board being fixed at the top of the support tube, top with
The column of the plate body connection, is slidably provided with a drive block in the support tube, the bottom of the column passes through the top
Plate is simultaneously connected with the drive block, many is fixed with the top of the top board and is slided through the drive block and with the drive block
The body of rod of connection, the bottom of the body of rod is connected with the base plate, is located on the body of rod between the top board and drive block and covered
Spring is provided with, is located on the body of rod and is arranged with lower spring between the drive block and base plate.
4. smooth power aerial vehicle according to claim 3, it is characterised in that：The quantity of the body of rod is two.
5. smooth power aerial vehicle according to claim 1, it is characterised in that：During the solar energy electroplax is with the first motor
The heart is symmetrical set.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621307103.3U CN206202687U (en) | 2016-12-01 | 2016-12-01 | A kind of smooth power aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621307103.3U CN206202687U (en) | 2016-12-01 | 2016-12-01 | A kind of smooth power aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206202687U true CN206202687U (en) | 2017-05-31 |
Family
ID=58752225
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621307103.3U Expired - Fee Related CN206202687U (en) | 2016-12-01 | 2016-12-01 | A kind of smooth power aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206202687U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107215464A (en) * | 2017-06-27 | 2017-09-29 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned plane with long battery life |
-
2016
- 2016-12-01 CN CN201621307103.3U patent/CN206202687U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107215464A (en) * | 2017-06-27 | 2017-09-29 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned plane with long battery life |
| CN107215464B (en) * | 2017-06-27 | 2018-10-02 | 吉林省翼启飞科技有限公司 | A kind of intelligent unmanned plane with long battery life |
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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: 20170531 Termination date: 20171201 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |