CN108146611A - A kind of portable agricultural formula unmanned plane and its application method - Google Patents
A kind of portable agricultural formula unmanned plane and its application method Download PDFInfo
- Publication number
- CN108146611A CN108146611A CN201711406343.8A CN201711406343A CN108146611A CN 108146611 A CN108146611 A CN 108146611A CN 201711406343 A CN201711406343 A CN 201711406343A CN 108146611 A CN108146611 A CN 108146611A
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- set casing
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- plate
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- 238000000034 method Methods 0.000 title claims abstract description 16
- 230000006835 compression Effects 0.000 claims description 20
- 238000007906 compression Methods 0.000 claims description 20
- 230000000694 effects Effects 0.000 claims description 6
- 239000007787 solid Substances 0.000 claims description 3
- 230000002035 prolonged effect Effects 0.000 claims 2
- 230000003139 buffering effect Effects 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 239000000575 pesticide Substances 0.000 description 3
- 238000013016 damping Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000005507 spraying Methods 0.000 description 2
- 241000700605 Viruses Species 0.000 description 1
- 230000006978 adaptation Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 230000004083 survival effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Catching Or Destruction (AREA)
Abstract
The present invention relates to unmanned air vehicle technique fields, disclose a kind of portable agricultural formula unmanned plane, including fuselage and wing, wing is fixedly connected with set casing close to the side of fuselage, the bottom of set casing, which is run through, connecting rod, one end that connecting rod is extended to outside set casing is fixedly connected with connecting plate, the bottom of connecting plate is fixedly connected with arc panel, fuselage offers the arc groove being adapted with arc panel close to the side of wing, the both sides of fuselage roof have been fixedly connected with support plate, and the invention also discloses its application methods.The portable agricultural formula unmanned plane and its application method, set casing is fixedly connected with close to the side of fuselage by wing, it is more convenient using meeting, all complicated program is simplified so that carrying and installing, the surface that one end inside set casing is extended to by connecting rod is fixedly connected with fixed plate, wing section is dismantled, then can easily be carried, use is very convenient and simple.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specially a kind of portable agricultural formula unmanned plane and its user
Method.
Background technology
UAV abbreviation unmanned plane is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft without cockpit on machine, but is equipped with the equipment such as automatic pilot, presetting apparatus, on ground, naval vessels or female
Machine remote control station personnel, can be distant in radio to it into line trace, positioning, remote control, telemetering and Digital Transmission by equipment such as radars
Take off as conventional airplane or launched with booster rocket under control, can also be taken to by machine tool it is aerial launch flight, during recycling,
The mode automatic Landing as conventional airplane landing mission can be used, can also be recycled by remote control parachute or block, it can be anti-
It is multiple to use repeatedly, aerial reconnaissance, monitoring, communication, antisubmarine and electronic interferences etc. are widely used in, compared with manned aircraft, it has
Small, low cost, it is easy to use, to operational environment require low and battlefield survival it is stronger the advantages that, receive countries in the world
The favor of army, in several local wars, UAV with its accurate, efficient and nimble scouting, interference, deception,
Search, school are penetrated and a variety of fight capabilities such as operation under the conditions of informal, plays obvious action, and caused and emerged in an endless stream
The relevant issues such as art of war, equipment technology research, it by with breed in arsenal warship, robot tank, robot
Soldier, computer virus weapon, space-based weapon, laser weapon etc. together, become 21st century land battle, sea warfare, air battle, day war
Key player on stage causes more far-reaching influence to following military struggle.
The typically use of agricultural unmanned plane can replace the artificial sprinkling for carrying out pesticide in terms of pesticide spraying, in order to
Efficient production is obtained, but general unmanned plane volume is larger, it has not been convenient to it carries, the people for agricultural planting brings puzzlement,
Using very cumbersome.
Invention content
In view of the deficiencies of the prior art, the present invention provides a kind of portable agricultural formula unmanned plane and its users
Method solves the problem of inconvenient to carry, use is very cumbersome.
In order to achieve the above object, the present invention is achieved by the following technical programs：A kind of portable agricultural formula without
Man-machine, including fuselage and wing, the wing is fixedly connected with set casing close to the side of fuselage, and the bottom of set casing is passed through
Connecting rod is installed with, one end that the connecting rod is extended to outside set casing is fixedly connected with connecting plate, and the bottom of connecting plate
Arc panel is fixedly connected with, the fuselage offers the arc groove being adapted with arc panel, and fuselage close to the side of wing
The both sides at top have been fixedly connected with support plate, and the side of the support plate is through there is catch bar, and the catch bar is far from support
Plate has single inside run through set casing and extend to set casing, and the catch bar extends to the surface one of one end inside set casing
Side offers the card slot being adapted with connecting rod, and the surface activity of the catch bar is connected with lantern ring.
Preferably, the surface of the connecting rod and positioned at set casing bottom and connecting plate top between be fixedly connected with
First spring, the surface of the catch bar and positioned at support plate side and set casing side between be fixedly connected with the second bullet
Spring.
Preferably, the connecting rod extends to the surface of one end inside set casing and is fixedly connected with fixed plate, the promotion
One end that bar is extended to outside support plate is fixedly connected with handle.
Preferably, the both sides of the wing bottom have been fixedly connected with shell, and both sides of fuselage roof and positioned at solid
The side for determining shell is fixedly connected with fixed link, and the top of the fixed link runs through shell and extends to the inside of shell, described solid
The both sides of fixed pole are through there is an arc block, and arc block extends to one end of enclosure and is fixedly connected with third spring.
Preferably, the both sides of the fuselage bottom have been fixedly connected with compression bar, and the bottom end of compression bar is through there is sheath body, institute
It states one end that compression bar is extended to inside sheath body and is fixedly connected with movable block, and the both sides of movable block bottom are connected with cunning
Bar, the both sides of the sheath body inner wall have been fixedly connected with slide plate, and the opposite side of slide plate slidably connects sliding block, described
One end of slide bar is flexibly connected with the side of sliding block.
Preferably, one end both sides that the compression bar is extended to inside sheath body have been fixedly connected with teeth, and inside sheath body
Both sides be fixedly connected with the gear being meshed with teeth, the bottom of the movable block is fixedly connected with the body of rod, and the body of rod
Bottom end be fixedly connected with the first plate body, the both sides of the first plate body bottom are connected with the first motion bar, and
The bottom end of one motion bar is connected with the second motion bar, and the bottom end of second motion bar is connected with the second plate body, and
And second the both sides of plate body bottom be fixedly connected with telescopic rod, the surface of the telescopic rod and positioned at the bottom of the second plate body with
The 4th spring is fixedly connected between the bottom of sheath body inner wall.
The invention also discloses a kind of application methods of portable agricultural formula unmanned plane, include the following steps：
S1, first the arc panel being adapted with arc groove is sticked into arc groove；
S2, catch bar is injected by support plate in set casing by handle again, in the card that the bottom of catch bar is provided with
Slot blocks the top of connecting rod, so as to being stuck in arc groove tightly by arc panel；
Arc block in S3 while fixed link can be popped up by the elastic force of third spring, and fixed link is stuck in by arc block
In shell, and then complete the fixation to wing.
The present invention provides a kind of portable agricultural formula unmanned plane and its application methods.Has following advantageous effect：
(1), the portable agricultural formula unmanned plane and its application method are fixed close to the side of fuselage by wing and connected
Set casing is connected to, and the bottom of set casing, through there is connecting rod, one end that connecting rod is extended to outside set casing is fixedly connected
There is connecting plate, and the bottom of connecting plate is fixedly connected with arc panel, fuselage offers and arc panel phase close to the side of wing
The arc groove of adaptation, and the both sides of fuselage roof have been fixedly connected with support plate, and the side of support plate is pushed away through there is catch bar
Lever has single inside run through set casing and extend to set casing far from support plate, and catch bar extends to one end inside set casing
Surface side offer the card slot being adapted with connecting rod, the surface activity of catch bar is connected with lantern ring, utilize assembling installation
Mode, agricultural unmanned plane is dismantled, using can be more convenient so that carry and installation is all simple by complicated program
Change, facilitate the operation of agricultural producer significantly.
(2), the portable agricultural formula unmanned plane and its application method are extended to by connecting rod one inside set casing
The surface at end is fixedly connected with fixed plate, and one end that catch bar is extended to outside support plate is fixedly connected with handle, wing bottom
Both sides be fixedly connected with shell, and the both sides of fuselage roof and be fixedly connected with fixed link positioned at the side of set casing,
The top of fixed link runs through shell and extends to the inside of shell, and the both sides of fixed link, which are run through, arc block, and arc block
The one end for extending to enclosure is fixedly connected with third spring, and unmanned plane is exactly mainly that wing section area occupied is larger, will
Wing section is dismantled, and then can easily be carried, and use is very convenient and simple.
(3), the portable agricultural formula unmanned plane and its application method, one end inside sheath body is extended to by compression bar
Both sides have been fixedly connected with teeth, and the both sides inside sheath body are fixedly connected with the gear being meshed with teeth, movable block
Bottom be fixedly connected with the body of rod, and the bottom end of the body of rod is fixedly connected with the first plate body, the both sides of the first plate body bottom are living
It is dynamic to be connected with the first motion bar, and the bottom end of the first motion bar is connected with the second motion bar, the bottom end of the second motion bar
The second plate body is connected with, and the both sides of the second plate body bottom have been fixedly connected with telescopic rod, the surface and position of telescopic rod
It is fixedly connected with the 4th spring between the bottom of the second plate body and the bottom of sheath body inner wall, decline when carries out universal wheel
Damping can keep stationarity and the safety of fuselage so that pesticide spraying carries out under the environment of a safety.
(4), the portable agricultural formula unmanned plane and its application method, are fixedly connected with by the both sides of fuselage bottom
There is compression bar, and the bottom end of compression bar, through there is sheath body, one end that compression bar is extended to inside sheath body is fixedly connected with movable block, and
The both sides of movable block bottom are connected with slide bar, and the both sides of sheath body inner wall have been fixedly connected with slide plate, and slide plate is opposite
Side slidably connect sliding block, one end of slide bar is flexibly connected with the side of sliding block, and compression bar extends to one inside sheath body
End both sides have been fixedly connected with teeth, and the both sides inside sheath body are fixedly connected with the gear being meshed with teeth, activity
The bottom of block is fixedly connected with the body of rod, and the bottom end of the body of rod is fixedly connected with the first plate body, and the both sides of the first plate body bottom are equal
The first motion bar is connected with, and the bottom end of the first motion bar is connected with the second motion bar, the bottom of the second motion bar
End is connected with the second plate body, to the sheath body of decline into row buffering, it is ensured that the safety of unmanned plane, user also can be compared with
To feel at ease, operation also can be more safe and quick.
Description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is the sectional view of airframe structure of the present invention；
Fig. 3 is the sectional view of fixed rod structure of the present invention；
Fig. 4 is the front view of airframe structure of the present invention；
Fig. 5 is the sectional view of case structure of the present invention.
In figure：1 fuselage, 2 wings, 3 set casings, 4 connecting rods, 5 connecting plates, 6 arc panels, 7 arc grooves, 8 support plates, 9 push away
Lever, 10 card slots, 11 lantern rings, 12 first springs, 13 second springs, 14 fixed plates, 15 handles, 16 shells, 17 fixed links, 18 arcs
Shape block, 19 third springs, 20 compression bars, 21 sheath bodies, 22 movable blocks, 23 slide bars, 24 slide plates, 25 sliding blocks, 26 gears, 27 bodies of rod, 28
First plate body, 29 first motion bars, 30 second motion bars, 31 second plate bodys, 32 telescopic rods, 33 the 4th springs, 34 teeth.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other without making creative work
Embodiment shall fall within the protection scope of the present invention.
- 5 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of portable agricultural formula unmanned plane, including machine
Body 1 and wing 2, the both sides of 2 bottom of wing have been fixedly connected with shell 16, and the both sides at 1 top of fuselage and positioned at set casing 3
Side be fixedly connected with fixed link 17, the top of fixed link 17 is through shell 16 and extends to the inside of shell 16, fixed link
17 both sides, which are run through, has arc block 18, and one end that arc block 18 is extended to inside shell 16 is fixedly connected with third spring
19, the both sides of 1 bottom of fuselage have been fixedly connected with compression bar 20, and compression bar 20 extends to the fixed company in one end both sides inside sheath body 21
Teeth 34 are connected to, and the both sides inside sheath body 21 are fixedly connected with the gear 26 being meshed with teeth 34, movable block 22
Bottom is fixedly connected with the body of rod 27, and the bottom end of the body of rod 27 is fixedly connected with the first plate body 28, and the two of 28 bottom of the first plate body
Side is connected with the first motion bar 29, and the bottom end of the first motion bar 29 is connected with the second motion bar 30, and second
The bottom end of motion bar 30 is connected with the second plate body 31, and the both sides of 31 bottom of the second plate body have been fixedly connected with telescopic rod
32, the surface of telescopic rod 32 and positioned at the second plate body 31 21 inner wall of bottom and sheath body bottom between be fixedly connected with the 4th bullet
Spring 33, and the bottom end of compression bar 20 is through there is sheath body 21, to the sheath body 21 of decline into row buffering, it is ensured that the safety of unmanned plane
Property, user also can more feel at ease, operation also can more safety with quick, the bottom of sheath body 21 is fixedly connected with universal wheel,
A distance, the pressure that buffer falling is brought can be slided when landing, one end that compression bar 20 is extended to inside sheath body 21 is consolidated
Surely movable block 22 is connected with, and the both sides of 22 bottom of movable block are connected with slide bar 23, the both sides of 21 inner wall of sheath body are equal
It is fixedly connected with slide plate 24, and the opposite side of slide plate 24 slidably connects sliding block 25, one end and the sliding block 25 of slide bar 23
Side flexible connection, when unmanned plane will land, compression bar 20 can be pressed downward, and gear 26 can under the drive of teeth 34
It is rotated, slide bar 23 can push sliding block 25 to be moved on slide plate 24, and the first plate body 28 can be pressed downward, the first motion bar 29
With the second motion bar 30 meeting opposing compression, damping is carried out under the buffering of telescopic rod, wing 2 is fixed close to the side of fuselage 1 to be connected
Be connected to set casing 3, and the bottom of set casing 3 is through there is a connecting rod 4, the surface of connecting rod 4 and positioned at the bottom of set casing 3 with
The first spring 12, the surface of catch bar 9 and side and the fixation for being located at support plate 8 are fixedly connected between the top of connecting plate 5
Second spring 13 is fixedly connected between the side of shell 3, the surface that connecting rod 4 extends to 3 inside one end of set casing is fixedly connected
There is fixed plate 14, one end that catch bar 9 is extended to outside support plate 8 is fixedly connected with handle 15, and connecting rod 4 extends to set casing
One end outside 3 is fixedly connected with connecting plate 5, and the bottom of connecting plate 5 is fixedly connected with arc panel 6, and fuselage 1 is close to wing
2 side offers the arc groove 7 being adapted with arc panel 6, and the both sides at 1 top of fuselage have been fixedly connected with support plate 8,
The side of support plate 8, which is run through, catch bar 9, the having list through set casing 3 and extending to set casing 3 far from support plate 8 of catch bar 9
Inside, the surface side that catch bar 9 extends to 3 inside one end of set casing offers the card slot 10 being adapted with connecting rod 4, pushes away
The surface activity of lever 9 is connected with lantern ring 11.
The invention also discloses a kind of application methods of portable agricultural formula unmanned plane, include the following steps：
S1, first the arc panel 6 being adapted with arc groove 7 is sticked into arc groove 7；
S2, catch bar 9 is injected by support plate 8 in set casing 3 by handle 15 again, is set in the bottom of catch bar 9
Some card slots 10 block the top of connecting rod 4, so as to being stuck in arc groove 7 tightly by arc panel 6；
Arc block 18 in S3 while fixed link 17 can be popped up by the elastic force of third spring 19, and fixed link 17 passes through arc
Shape block 18 is stuck in shell 16, and then completes the fixation to wing 2.
Finally illustrate, the above embodiments are merely illustrative of the technical solutions of the present invention and it is unrestricted, although with reference to compared with
The present invention is described in detail in good embodiment, it will be understood by those of ordinary skill in the art that, it can be to the skill of the present invention
Art scheme is modified or replaced equivalently, and without departing from the objective and range of the technical program, should all be covered in the present invention
Right in.
Claims (7)
1. a kind of portable agricultural formula unmanned plane, including fuselage (1) and wing (2), it is characterised in that：The wing (2)
Set casing (3) is fixedly connected with close to the side of fuselage (1), and the bottom of set casing (3) is through there is connecting rod (4), it is described
Connecting rod (4) extends to the external one end of set casing (3) and is fixedly connected with connecting plate (5), and the bottom of connecting plate (5) is fixed
Arc panel (6) is connected with, the fuselage (1) offers the arc groove being adapted with arc panel (6) close to the side of wing (2)
(7), and the both sides at the top of fuselage (1) have been fixedly connected with support plate (8), and the side of the support plate (8), which is run through, promotion
Bar (9), the catch bar (9) have single inside run through set casing (3) and extend to set casing (3), institute far from support plate (8)
It states catch bar (9) and extends to the surface side of the internal one end of set casing (3) and offer the card slot being adapted with connecting rod (4)
(10), the surface activity of the catch bar (9) is connected with lantern ring (11).
2. the portable agricultural formula unmanned plane of one kind according to claim 1, it is characterised in that：The connecting rod (4)
Surface and positioned at set casing (3) bottom and connecting plate (5) top between be fixedly connected with the first spring (12), it is described to push away
The surface of lever (9) and positioned at support plate (8) side and set casing (3) side between be fixedly connected with second spring
(13)。
3. the portable agricultural formula unmanned plane of one kind according to claim 1, it is characterised in that：The connecting rod (4)
The surface for extending to the internal one end of set casing (3) is fixedly connected with fixed plate (14), and the catch bar (9) extends to support plate
(8) external one end is fixedly connected with handle (15).
4. the portable agricultural formula unmanned plane of one kind according to claim 1, it is characterised in that：Wing (2) bottom
The both sides in portion have been fixedly connected with shell (16), and both sides at the top of fuselage (1) and being fixed positioned at the side of set casing (3) connect
Fixed link (17) is connected to, the top of the fixed link (17) runs through shell (16) and extends to the inside of shell (16), described solid
The both sides of fixed pole (17), which are run through, arc block (18), and arc block (18) extends to the internal one end of shell (16) and fixes and connects
It is connected to third spring (19).
5. the portable agricultural formula unmanned plane of one kind according to claim 1, it is characterised in that：Fuselage (1) bottom
The both sides in portion have been fixedly connected with compression bar (20), and the bottom end of compression bar (20), through there is sheath body (21), the compression bar (20) is prolonged
It extends to the internal one end of sheath body (21) and is fixedly connected with movable block (22), and the both sides of movable block (22) bottom are flexibly connected
There is slide bar (23), the both sides of sheath body (21) inner wall have been fixedly connected with slide plate (24), and the side that slide plate (24) is opposite
Sliding block (25) is slidably connected, one end of the slide bar (23) is flexibly connected with the side of sliding block (25).
6. the portable agricultural formula unmanned plane of one kind according to claim 5, it is characterised in that：The compression bar (20) is prolonged
It extends to the internal one end both sides of sheath body (21) and has been fixedly connected with teeth (34), and the fixed company in both sides that sheath body (21) is internal
The gear (26) being meshed with teeth (34) is connected to, the bottom of the movable block (22) is fixedly connected with the body of rod (27), and bar
The bottom end of body (27) is fixedly connected with the first plate body (28), and the both sides of the first plate body (28) bottom are connected with first
Motion bar (29), and the bottom end of the first motion bar (29) is connected with the second motion bar (30), second motion bar
(30) bottom end is connected with the second plate body (31), and the both sides of the second plate body (31) bottom have been fixedly connected with telescopic rod
(32), the surface of the telescopic rod (32) and the fixation between the bottom of the second plate body (31) and the bottom of sheath body (21) inner wall
It is connected with the 4th spring (33).
7. a kind of application method of portable agricultural formula unmanned plane as described in claim 1~6 any one, feature
It is, includes the following steps：
S1, first the arc panel (6) being adapted with arc groove (7) is sticked into arc groove (7)；
S2, catch bar (9) is injected by support plate (8) in set casing (3) by handle (15) again, at the bottom of catch bar (9)
The card slot (10) that portion is provided with blocks the top of connecting rod (4), so as to being stuck in arc groove (7) tightly by arc panel (6)；
Arc block (18) in S3 while fixed link (17) can be popped up by the elastic force of third spring (19), and fixed link (17) is logical
It crosses arc block (18) to be stuck in shell (16), and then completes the fixation to wing (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711406343.8A CN108146611B (en) | 2017-12-22 | 2017-12-22 | Portable agricultural unmanned aerial vehicle and use method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711406343.8A CN108146611B (en) | 2017-12-22 | 2017-12-22 | Portable agricultural unmanned aerial vehicle and use method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108146611A true CN108146611A (en) | 2018-06-12 |
| CN108146611B CN108146611B (en) | 2022-03-11 |
Family
ID=62465198
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711406343.8A Active CN108146611B (en) | 2017-12-22 | 2017-12-22 | Portable agricultural unmanned aerial vehicle and use method thereof |
Country Status (1)
| Country | Link |
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| CN (1) | CN108146611B (en) |
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| CN109353507A (en) * | 2018-10-17 | 2019-02-19 | 中卫航空科技发展有限公司 | A kind of portable multi-function individual combat unmanned plane |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109353507A (en) * | 2018-10-17 | 2019-02-19 | 中卫航空科技发展有限公司 | A kind of portable multi-function individual combat unmanned plane |
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