CN208842627U - One kind is for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil - Google Patents
One kind is for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil Download PDFInfo
- Publication number
- CN208842627U CN208842627U CN201821425369.7U CN201821425369U CN208842627U CN 208842627 U CN208842627 U CN 208842627U CN 201821425369 U CN201821425369 U CN 201821425369U CN 208842627 U CN208842627 U CN 208842627U
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- main body
- welded
- oil
- propeller
- 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
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The utility model discloses one kind for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil, including main body, the outer surface corner location of the main body is welded with brake box, and the upper end of brake box is movably installed with propeller, the lower end outer surface corner location of the main body is welded with support socle, the internal activity of the main body is equipped with protective plate, and the position between the two neighboring protective plate is fixedly installed with battery and signal receiving member, and the outside of the propeller is enclosed with shield.The utility model makes the present apparatus in use and can effectively reduce the impact that body is subject to when unmanned plane landing by being provided with a series of structure, reduce the damage that body is subject to, the damage that internal body is subject to can also be effectively reduced simultaneously, extend the service life of the unmanned plane, and the situation that propeller is hurted sb.'s feelings when can effectively reduce unmanned landing occurs, and makes the unmanned plane more multi-functional.
Description
Technical field
The utility model relates to air vehicle technique field, it is specially a kind of for the plant area's safety patrol inspection that recovers the oil it is multi-functional nobody
Machine.
Background technique
Unmanned plane refers to the not manned aircraft using radio robot and the presetting apparatus provided for oneself manipulation, nobody
Machine has many uses, including takes photo by plane, agricultural, plant protection, miniature self-timer, express transportation etc., but existing unmanned plane structure is simple,
Protection effect is poor, so that unmanned plane its external structure in landing is easily damaged, and the internal electron components of unmanned plane
More accurate, so that nobody its internal electron components in landing are also easy to damage because of vibration, while nobody is landing
When its propeller there is the danger hurted sb.'s feelings, function is more single, to unmanned plane meeting with bringing certain influence.
Utility model content
The purpose of this utility model is to provide one kind for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil, on solving
State the problem of proposing in background technique.
To achieve the above object, the utility model provides the following technical solutions: one kind is more for the plant area's safety patrol inspection that recovers the oil
Function unmanned plane, including main body, the outer surface corner location of the main body is welded with brake box, and the upper end of brake box is living
Dynamic to be equipped with propeller, the lower end outer surface corner location of the main body is welded with support socle, the inside of the main body
It is movably installed with protective plate, the position between the two neighboring protective plate is fixedly installed with battery and signal receiving member,
The outside of the propeller is enclosed with shield, and the lower end outer surface of the main body is welded with link block, two neighboring described
Position between link block is movably installed with overturning seat, and the lower end of the overturning seat is fixedly installed with camera, the main body
Leading exterior surface be hinged with maintenance door, the inside of the brake box is fixedly installed with brake motor, under the support socle
Side is equipped with partial pressure block, and the inside of the support socle is plugged with guide post, and guide post is connect with partial pressure block welding, the support socle
Inner tip be movably installed with buffer spring.
By using above-mentioned technical proposal, being provided with a series of structure makes the present apparatus in use can be effective
The impact that body is subject to when reducing unmanned plane landing, reduces the damage that body is subject to, while can also effectively reduce machine
The damage that internal portion is subject to, propeller when extending the service life of the unmanned plane, and can effectively reduce unmanned landing
The situation hurted sb.'s feelings occurs.
Preferably, the lower end of the shield is welded with connecting column, and the inner surface of the propeller offers link slot, and
The inner surface of link slot offers ball grooves, and the internal activity of the ball grooves is equipped with ball, and the inside of the link slot is living
It is dynamic that connector is installed, and connector and connecting column are welded to connect.
By using above-mentioned technical proposal, it can be avoided propeller rotational and drive shield rotation.
Preferably, the position between the protective plate and the inner wall of main body is movably installed with protection spring, and protects bullet
The quantity of spring is at least four.
By using above-mentioned technical proposal, protective plate be combined with protection spring can reduce components inside unmanned plane by
The vibration arrived.
Preferably, it is described protection spring upper end and main body inner wall be welded to connect, it is described protection spring lower end with
Protective plate is welded to connect.
By using above-mentioned technical proposal, can be avoided protection spring and fall off influences protection effect.
Preferably, the flip angle range of the overturning seat is 0 ° to 180 °.
By using above-mentioned technical proposal, allow the camera on overturning seat being capable of better filmed image.
Preferably, the output end of the battery is electrically connected the input of camera, signal receiving member and brake motor
End.
By using above-mentioned technical proposal, battery is that camera, signal receiving member and brake motor are powered.
In conclusion the utility model has the following beneficial effects:
1, by wrapping up shield in the external of propeller, shield effectively can avoid unmanned plane from dropping on ground
Afterwards, the situation that propeller rotation is hurted sb.'s feelings occurs, and shield is Openworks shape, will not influence the use of propeller, while shield is logical
It crosses in the link slot that the connector on connecting column is mounted on propeller, ball grooves, the rolling in ball grooves has been opened up in link slot
Pearl can be combined with the connector on connecting column, and the situation that propeller-driven shield can be effectively prevent to rotate occurs, effectively
The safety for improving the unmanned plane, also allow the unmanned plane more multi-functional；
2, by the partial pressure block in setting, unmanned plane can be dropped on ground with the power of ground face contact more by dividing block
It is uniformly transmitted on guide post, then power is transmitted on buffer spring by guide post, buffer spring can absorb the power of guide post conduction, come
Reach the impact force for mitigating that unmanned plane shell is subject to when unmanned plane drops on ground, to effectively extend making for unmanned plane
Use the service life；
3, it is all mounted on protective plate by the protective plate of setting, battery and signal receiving member, in protective plate and master
It is mounted with that protective plate is mounted on inside main body by protection spring, protection spring between on the inner wall of body, can reduce electric power storage
The impact force that pond and signal receiving member are subject to during unmanned plane during flying and in descent, further extends this
The service life of unmanned plane.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model；
Fig. 2 is the main body interior views of the utility model；
Fig. 3 is that the propeller of the utility model matches view with shield；
Fig. 4 is the enlarged view in Fig. 3 of the utility model at A；
Fig. 5 is the support socle interior views of the utility model.
In figure: 1, main body；2, brake box；201, brake motor；3, propeller；301, link slot；302, ball grooves；
303, ball；4, socle is supported；401, block is divided；402, guide post；403, buffer spring；5, protective plate；501, spring is protected；6,
Battery；7, signal receiving member；8, shield；801, connecting column；802, connector；9, link block；10, overturning seat；11, it takes the photograph
As head；12, maintenance door.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
In the description of the present invention, it should be noted that term " on ", "lower", "inner", "outside" " front end ", " after
The orientation or positional relationship of the instructions such as end ", " both ends ", " one end ", " other end " is that orientation based on the figure or position are closed
System, is merely for convenience of describing the present invention and simplifying the description, rather than the device or element of indication or suggestion meaning are necessary
It with specific orientation, is constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.In addition,
Term " first ", " second " are used for descriptive purposes only and cannot be understood as indicating or suggesting relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified
Dress ", " being provided with ", " connection " etc., shall be understood in a broad sense, such as " connection ", may be a fixed connection, be also possible to detachably connect
It connects, or is integrally connected；It can be mechanical connection, be also possible to be electrically connected；It can be directly connected, intermediate matchmaker can also be passed through
Jie is indirectly connected, and can be the connection inside two elements.It for the ordinary skill in the art, can be with concrete condition
Understand the concrete meaning of above-mentioned term in the present invention.
Please refer to Fig. 1-5, a kind of embodiment provided by the utility model: one kind is multi-functional for the plant area's safety patrol inspection that recovers the oil
Unmanned plane, including main body 1, the running of brake motor 201 when use in brake box 2 drives 3 high speed rotation of propeller, to come
Unmanned plane during flying is driven, the support socle 4 of the lower end outer surface corner location welding of main body 1 can be mentioned when unmanned plane lands
For support, unmanned plane landing time-division briquetting 401 can first contact ground, and power is transmitted to buffering elastic by guide post 402 by partial pressure block 401
The impact force that unmanned plane shell is subject to is reduced on spring 403, battery 6 and signal receiving member 7 are mounted on inside main body 1
On protective plate 5, battery 6 is unmanned plane power supply, and signal receiving member 7 is used to receive control signal, the external package of propeller 3
Shield 8 can prevent propeller 3 from hurting sb.'s feelings, and overturning seat 10 is mounted between link block 9, in the fixed peace in the lower end of overturning seat 10
Camera 11 is filled for filmed image, the hinged maintenance door 12 of the leading exterior surface of main body 1.
Further, the lower end of shield 8 is welded with connecting column 801, and the inner surface of propeller 3 offers link slot 301, and
The inner surface of link slot 301 offers ball grooves 302, and the internal activity of ball grooves 302 is equipped with ball 303, link slot 301
Internal activity is equipped with connector 802, and connector 802 and connecting column 801 are welded to connect, and can be avoided propeller 3 and rotates band
Dynamic shield 8 rotates.
Further, the position between protective plate 5 and the inner wall of main body 1 is movably installed with protection spring 501, and protects bullet
The quantity of spring 501 is at least four, protective plate 5 be combined with protection spring 501 can reduce components inside unmanned plane by
Vibration.
Further, the upper end of protection spring 501 and the inner wall of main body 1 are welded to connect, and are protected the lower end of spring 501 and are prevented
Backplate 5 is welded to connect, and can be avoided protection spring 501 and fall off influences protection effect.
Further, the flip angle range of overturning seat 10 is 0 ° to 180 °, allows the camera 11 on overturning seat 10 can be more
Good filmed image.
Further, it is defeated with brake motor 201 to be electrically connected camera 11, signal receiving member 7 for the output end of battery 6
Outlet, battery 6 are that camera 11, signal receiving member 7 and brake motor 201 are powered.
It should be noted that the utility model is a kind of for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil, in use,
The running of brake motor 201 in brake box 2 drives 3 high speed rotation of propeller to drive unmanned plane during flying, the type of brake motor 201
Number be BMU80H60V3, main body 1 lower end outer surface corner location welding support socle 4 can unmanned plane land when mention
For support, unmanned plane landing time-division briquetting 401 can first contact ground, and partial pressure block 401 can drop to unmanned plane on ground will
With the power of ground face contact on the guide post 402 of more uniform conduction, then by guide post 402 power is transmitted on buffer spring 403, is delayed
The power of the conduction of guide post 402 can be absorbed by rushing spring 403, mitigate what unmanned plane shell when unmanned plane drops on ground was subject to reach
Impact force, to effectively extend the service life of unmanned plane, battery 6 and signal receiving member 7 are all mounted on protective plate 5
On, on the inner wall of protective plate 5 and main body 1 between be mounted with protection spring 501, protection spring 501 protective plate 5 is mounted on
Inside main body 1, can reduce battery 6 and signal receiving member 7 during unmanned plane during flying and in descent by
Impact force, further extend the service life of the unmanned plane, battery 6 is unmanned plane power supply, the model of battery 6
For NCR18500, signal receiving member 7 is used to receive control signal, the model WD-1509N of signal receiving member 7, shield
After 8 effectively can avoid unmanned plane from dropping on ground, propeller 3 rotates the situation hurted sb.'s feelings and occurs, and shield 8 is hollow out
Shape will not influence the use of propeller 3, while shield 8 is mounted on propeller 3 by the connector 802 on connecting column 801
Link slot 301 in, ball grooves 302 have been opened up in link slot 301, the ball 303 in ball grooves 302 can be combined with connecting column
Connector 802 on 801, the situation that can effectively prevent propeller 3 that shield 8 is driven to rotate occur, and effectively raise this
The safety of unmanned plane, overturning seat 10 are mounted between link block 9, and camera 11 has been fixedly mounted in the lower end of overturning seat 10 and has used
Carry out filmed image, the hinged maintenance door 12 of the leading exterior surface of main body 1 effectively increases the functionality of its own, more practical.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
Claims (6)
1. one kind is for the recover the oil multi-functional unmanned plane of plant area's safety patrol inspection, including main body (1), it is characterised in that: the host
The outer surface corner location of body (1) is welded with brake box (2), and the upper end of brake box (2) is movably installed with propeller (3), institute
The lower end outer surface corner location for stating main body (1) is welded with support socle (4), the internal activity installation of the main body (1)
Have protective plate (5), the position between the two neighboring protective plate (5) is fixedly installed with battery (6) and signal receiving member
(7), the outside of the propeller (3) is enclosed with shield (8), and the lower end outer surface of the main body (1) is welded with link block
(9), the position between the two neighboring link block (9) is movably installed with overturning seat (10), the lower end of the overturning seat (10)
It is fixedly installed with camera (11), the leading exterior surface of the main body (1) is hinged with maintenance door (12), the brake box (2)
Inside be fixedly installed with brake motor (201), it is described support socle (4) lower section be equipped with partial pressure block (401), the support leg
The inside of column (4) is plugged with guide post (402), and guide post (402) and partial pressure block (401) are welded to connect, support socle (4)
Inner tip is movably installed with buffer spring (403).
2. according to claim 1 a kind of for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil, it is characterised in that: described
The lower end of shield (8) is welded with connecting column (801), and the inner surface of the propeller (3) offers link slot (301), and even
The inner surface of access slot (301) offers ball grooves (302), and the internal activity of the ball grooves (302) is equipped with ball (303),
The internal activity of the link slot (301) is equipped with connector (802), and connector (802) and connecting column (801) welding connect
It connects.
3. according to claim 1 a kind of for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil, it is characterised in that: described
Position between protective plate (5) and the inner wall of main body (1) is movably installed with protection spring (501), and protects spring (501)
Quantity is at least four.
4. according to claim 3 a kind of for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil, it is characterised in that: described
The inner wall of the upper end and main body (1) of protecting spring (501) is welded to connect, the lower end of protection spring (501) and protective plate
(5) it is welded to connect.
5. according to claim 1 a kind of for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil, it is characterised in that: described
The flip angle range of overturning seat (10) is 0 ° to 180 °.
6. according to claim 1 a kind of for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil, it is characterised in that: described
The output end of battery (6) is electrically connected the input terminal of camera (11), signal receiving member (7) and brake motor (201).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821425369.7U CN208842627U (en) | 2018-08-31 | 2018-08-31 | One kind is for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821425369.7U CN208842627U (en) | 2018-08-31 | 2018-08-31 | One kind is for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208842627U true CN208842627U (en) | 2019-05-10 |
Family
ID=66357891
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821425369.7U Expired - Fee Related CN208842627U (en) | 2018-08-31 | 2018-08-31 | One kind is for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208842627U (en) |
-
2018
- 2018-08-31 CN CN201821425369.7U patent/CN208842627U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206885363U (en) | The slow multiple protector of unmanned plane | |
| CN206766329U (en) | One kind is taken photo by plane unmanned plane | |
| CN206107557U (en) | Unmanned aerial vehicle for remote sensing fire control detection | |
| CN105947171A (en) | Flying robot protection device and flying robot with same | |
| CN205273843U (en) | Many rotor unmanned aerial vehicle's multi -functional undercarriage | |
| CN107108038A (en) | A kind of device for controlling forced landing, method, equipment | |
| JP6308550B2 (en) | Aircraft battery with protection frame that can run on land or water and its charge exchange device | |
| CN109367805A (en) | A kind of mapping unmanned plane with rotating camera | |
| CN205256683U (en) | Unmanned vehicles protection device that falls | |
| CN105882966B (en) | A kind of novel unmanned plane based on Internet of Things | |
| CN208842627U (en) | One kind is for the multi-functional unmanned plane of plant area's safety patrol inspection that recovers the oil | |
| CN110466774B (en) | Plant protection unmanned aerial vehicle is with field flight protector | |
| CN206511133U (en) | A kind of parachute of unmanned plane | |
| CN108341047A (en) | It is a kind of that there is the anti-safe unmanned plane blocked | |
| CN208102336U (en) | Rotor protection mechanism in a kind of unmanned plane | |
| CN206307266U (en) | A kind of multi-rotor unmanned aerial vehicle double damping undercarriage | |
| CN218431768U (en) | Unmanned aerial vehicle low-altitude flight protector | |
| CN109760830A (en) | A kind of three support leg module combined type rotor wing unmanned aerial vehicles of environment survey | |
| CN108791824A (en) | A kind of unmanned plane damping device | |
| CN207173956U (en) | A kind of fire-fighting duct depopulated helicopter | |
| CN205707278U (en) | The safe unmanned plane that a kind of cruising time is longer | |
| CN109131853A (en) | A kind of six rotor wing unmanned aerial vehicle of full module | |
| CN207292385U (en) | A kind of fire-fighting duct unmanned helicopter | |
| CN210707883U (en) | Security protection control unmanned aerial vehicle that can protect camera | |
| CN205633040U (en) | Medical treatment unmanned aerial vehicle |
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: 20190510 Termination date: 20200831 |