CN106828897A - Anti-tampering unmanned plane - Google Patents
Anti-tampering unmanned plane Download PDFInfo
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- CN106828897A CN106828897A CN201611261420.0A CN201611261420A CN106828897A CN 106828897 A CN106828897 A CN 106828897A CN 201611261420 A CN201611261420 A CN 201611261420A CN 106828897 A CN106828897 A CN 106828897A
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- Prior art keywords
- fuselage
- unmanned plane
- sleeve
- connecting rod
- connecting portion
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- 239000007921 spray Substances 0.000 claims abstract description 30
- 239000007788 liquid Substances 0.000 claims description 74
- 230000008676 import Effects 0.000 claims description 6
- 238000004891 communication Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000003860 storage Methods 0.000 description 3
- 238000012271 agricultural production Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 239000003814 drug Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000003973 irrigation Methods 0.000 description 2
- 230000002262 irrigation Effects 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 241000238631 Hexapoda Species 0.000 description 1
- 206010044565 Tremor Diseases 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 239000003905 agrochemical Substances 0.000 description 1
- 150000001450 anions Chemical class 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 150000001768 cations Chemical class 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 241000894007 species Species 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 239000012780 transparent material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- 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
- B64D47/00—Equipment not otherwise provided for
-
- 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
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Remote Sensing (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses a kind of anti-tampering unmanned plane, belong to unmanned air vehicle technique field.The anti-tampering unmanned plane, unmanned plane includes fuselage, controller, spray assembly, multiple rotors, multiple horns and the battery compartment built with battery, spray assembly is arranged on fuselage, multiple rotors are arranged in fuselage outer side by horn, controller for controlling unmanned plane during flying is arranged in fuselage, battery compartment is arranged on external fuselage by hanger, hanger includes hanging plate, closed plate and multiple pegs, the bottom of hanging plate and fuselage is oppositely arranged, hanging plate is towards being provided with mounting groove on the side of fuselage, battery compartment is arranged in mounting groove, closed plate is covered on mounting groove, the two ends of peg are fixedly connected with hanging plate and fuselage respectively.The present invention makes to be arranged on fuselage outer side, i.e. external battery for the battery used by controller communication, and to avoid in unmanned plane during flying, battery may interfere with to controller generation, it is ensured that unmanned plane flies on set route.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of anti-tampering unmanned plane.
Background technology
Unmanned plane, is to realize sprinkling using radio robot and the not manned aircraft of the controller provided for oneself manipulation
Operation, can spray medicament, seed, pulvis etc..With land transformation, farm land production scale, to improve agricultural production
Efficiency, reduces agricultural production, and the demand for generalizing has been turned into using unmanned plane plant protection.
Existing unmanned plane generally comprises the liquid reserve tank equipped with liquid and the jet pipe being connected with liquid reserve tank.When unmanned plane is in agriculture
On field during flight, the liquid in liquid reserve tank is sprayed onto on the crop in farmland by jet pipe, realizes plant protection.
Realize it is of the invention during, it is found by the applicant that at least having the following disadvantages in the prior art：
In the prior art, unmanned plane need to match somebody with somebody the battery used by available controller communication, and battery is generally pacified jointly with controller
In fuselage, so it is possible in unmanned plane during flying, battery produces interference to controller, and influence unmanned plane is set
Flown on route.
The content of the invention
In order to solve in the prior art, battery is produced to controller caused by battery and controller are commonly mounted in fuselage
The problem of interference, the invention provides a kind of anti-tampering unmanned plane.The technical scheme is as follows：
A kind of anti-tampering unmanned plane, the unmanned plane includes fuselage, controller, spray assembly, multiple rotors and multiple machines
Arm, the spray assembly is arranged on the fuselage, the multiple rotor by horn that setting is corresponded with it angularly
Arranged for interval is arranged in the fuselage in the fuselage outer side, the controller for controlling the unmanned plane during flying,
The unmanned plane also includes the battery compartment built with battery, and the battery compartment is arranged on outside the fuselage by hanger
Portion, the hanger includes hanging plate, closed plate and multiple peg, and the bottom of the hanging plate and the fuselage is oppositely arranged, the extension
Plate is arranged in the mounting groove towards mounting groove, the battery is provided with the side of the fuselage, closed plate covering
On the mounting groove, the two ends of the multiple peg are fixedly connected with the hanging plate and the fuselage respectively.
Further, the unmanned plane also includes the support for supporting the fuselage, and the support is relative including two groups
The support component of arrangement, each described support component includes two perpendicular supports and a stull, and the perpendicular support has first end
And the second end, described two are erected the first ends for supportting and are fixedly mounted on the fuselage, described two the second ends of perpendicular support
In the stull, by connecting support connection between the described perpendicular support in support component described in two groups.
Further, the spray assembly includes liquid reserve tank, hydraulic pump, multiple jet pipe and one-to-one with the jet pipe
Shower nozzle, the liquid reserve tank is arranged on the hanger away from the side lower section of the fuselage and positioned at two groups of support groups of the support
Between part, the hydraulic pump is arranged on the liquid reserve tank, and the multiple jet pipe is arranged at the fuselage outer side, the jet pipe
With first end and the second end, the first end of the multiple jet pipe is connected by the hydraulic pump with liquid reserve tank, described
The second end of multiple jet pipes extends to the diverse location of the fuselage outer side, and the shower nozzle is arranged on the corresponding jet pipe
The second end.
Further, the spray assembly also includes the support for installing the liquid reserve tank, and the support includes relative
The top board and base plate of setting, the top board are fixedly connected by multiple screw rods with the hanging plate, the top board and the base plate it
Between connected by multiple fix bars, the multiple fix bar, the top board and the base plate surround one with the liquid reserve tank phase
The FX of matching, the liquid reserve tank is fixedly installed in the FX.
Further, the jet pipe and shower nozzle of the spray assembly are provided with two, and two jet pipes are oppositely arranged；
The spray assembly also includes threeway, and the threeway is arranged in the connection support, and the threeway has an import and two
Outlet, the import of the threeway connect with the delivery outlet of the hydraulic pump, two of the threeway export respectively with described in two
The first end connection of jet pipe.
Preferably, the side wall of the shower nozzle is provided with bolt hole, and the tune coordinated with its screw thread is provided with the bolt hole
Section screw rod, by rotating adjusting screw rod, can adjust the pressure of the liquor that shower nozzle is sprayed.
Further, the horn includes first connecting rod and second connecting rod, and the first connecting rod and the second connecting rod are equal
With first end and the second end, the first end of the first connecting rod is fixedly mounted on the fuselage, and described first connects
The second end of bar is arranged on described by folding device and the foldable connection of the first end of the second connecting rod, the rotor
The second end of second connecting rod.
Preferably, the folding device includes：
First sleeve, the first sleeve is fixedly set on the second end of the first connecting rod, is connected with described first
The second end of bar is relatively set with first connecting portion and second on the outer wall with the end of the first sleeve of first end
Connecting portion；
Second sleeve pipe, second sleeve pipe is fixedly set on the first end of the second connecting rod, is connected with described second
The first end of bar is relatively set with the 3rd connecting portion and the 4th on the outer wall with the end of second sleeve pipe of first end
Connecting portion, the 3rd connecting portion is rotatably connected by first rotating shaft with the second connecting portion；
Grab, the grab has first end and a second end, the first end of the grab by the second bearing pin with
The first connecting portion is rotatably connected, and the second end of the grab is snapped connection with the 4th connecting portion；
First bearing pin and second bearing pin be arranged in parallel, and are each perpendicular to the central shaft of the first sleeve.
Preferably, the folding device includes：
First sleeve, first sleeve is fixedly set on the second end of the first connecting rod, is connected with described first
The second end of bar is relatively set with first connecting portion and second on the outer wall with the end of first sleeve of first end
Connecting portion, the first connecting portion has sealed space；
Lock assembly, the lock assembly includes control-rod, gag lever post and return springs, and the control-rod has first
End and the second end, the first end of the control-rod are located at first connecting portion outside, the two of the return springs
End is connected with the first end and the first connecting portion of the control-rod respectively, and the second end of the control-rod extend into institute
State in sealed space, the gag lever post is located in the sealed space, and the gag lever post is vertically and fixedly arranged at the control-rod
On；
Second sleeve, the second sleeve is fixedly set on the first end of the second connecting rod, is connected with described second
The first end of bar is relatively set with the 3rd connecting portion and the 4th on the outer wall with the end of the second sleeve of first end
Connecting portion, the 3rd connecting portion is rotatably connected by the 3rd rotating shaft and the second connecting portion, and the 3rd rotating shaft is vertical
In the central shaft of the second sleeve；
Grab, the grab is fixedly installed on the 4th connecting portion, and the grab is extend into the sealed space,
The grab is operably separated or engaged with the gag lever post.
The beneficial effect that technical scheme is brought is：
A kind of anti-tampering unmanned plane disclosed in this invention, because unmanned plane includes the battery compartment built with battery, and electricity
Chi Cang is arranged on external fuselage by hanger, and hanger includes hanging plate, closed plate and multiple peg, and the bottom of hanging plate and fuselage is relative
Set, hanging plate is arranged in mounting groove towards mounting groove, battery is provided with the side of fuselage, and closed plate is covered in mounting groove
On, the two ends of multiple pegs are fixedly connected with hanging plate and fuselage respectively, can thus make for the battery used by controller communication
Installed in fuselage outer side, i.e. external battery, to avoid in unmanned plane during flying, battery may interfere with to controller generation, protect
Card unmanned plane flies on set route.
Brief description of the drawings
Technical scheme in order to illustrate more clearly the embodiments of the present invention, below will be to that will make needed for embodiment description
Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the present invention, for
For those of ordinary skill in the art, on the premise of not paying creative work, other can also be obtained according to these accompanying drawings
Accompanying drawing.
Fig. 1 is the structural representation of the anti-tampering unmanned plane of the embodiment of the present invention；
Fig. 2 is the arrangement schematic diagram of the jet pipe of the anti-tampering unmanned plane of the embodiment of the present invention；
Fig. 3 is the structural representation of the liquid reserve tank of the anti-tampering unmanned plane of the embodiment of the present invention；
The structural representation of the first implementation of each separate space connection in the liquid reserve tank of Fig. 4 embodiment of the present invention
Figure；
Fig. 5 is that the structure of second implementation of each separate space connection in the liquid reserve tank of the embodiment of the present invention is shown
It is intended to；
Fig. 6 is that the structure of the third implementation of each separate space connection in the liquid reserve tank of the embodiment of the present invention is shown
It is intended to；
Fig. 7 is the structural representation of the foldable implementation one of the horn of anti-tampering unmanned plane provided in an embodiment of the present invention
Figure；
Fig. 8 is the structural representation of the first sleeve of the first implementation of horn folding in the embodiment of the present invention；
Fig. 9 is the structural representation of the second sleeve of the first implementation of horn folding in the embodiment of the present invention；
Figure 10 is the structural representation of the grab of the first implementation of horn folding in the embodiment of the present invention；
Figure 11 is the structure of the folding implementation two of the horn of anti-tampering unmanned plane provided in an embodiment of the present invention
Schematic diagram；
Figure 12 is the structural representation of the first sleeve of second implementation of horn folding in the embodiment of the present invention；
Figure 13 is the structural representation of the second sleeve of second implementation of horn folding in the embodiment of the present invention.
Specific embodiment
To make the object, technical solutions and advantages of the present invention clearer, below in conjunction with accompanying drawing to embodiment party of the present invention
Formula is described in further detail.
The embodiment of the invention provides a kind of anti-tampering unmanned plane.
Fig. 1 is the structural representation of anti-tampering unmanned plane provided in an embodiment of the present invention, and Fig. 2 is the anti-of the embodiment of the present invention
Disturb the arrangement schematic diagram of the jet pipe of unmanned plane, referring to Fig. 1 and Fig. 2, the anti-tampering unmanned plane of the embodiment of the present invention, including fuselage
1st, controller, spray assembly a, multiple rotors 2 and multiple horns 4, spray assembly a are installed on the fuselage 1, and multiple rotors 2 pass through
Equiangularly spaced with the horn 4 that it corresponds setting to be arranged in the outside of fuselage 1, the controller for controlling unmanned plane during flying is pacified
In fuselage 1.Rotor rotational is controlled by controller, unmanned plane during flying can be driven, in the flight course of unmanned plane, spray
Component operation is spilt, the plant protection operation of unmanned plane is completed.
With reference to Fig. 1, in the embodiment of the present invention, the unmanned plane also includes the battery compartment 3 built with battery, and battery compartment 3 passes through
Hanger b is arranged on outside fuselage 1, and hanger b includes hanging plate 5, closed plate 6 and multiple pegs 7, and hanging plate 5 is relative with the bottom of fuselage 1
Set, hanging plate 5 is arranged in mounting groove towards mounting groove, battery is provided with the side of fuselage 1, and closed plate 6 is covered in installation
On groove, the two ends of multiple pegs 7 are fixedly connected with hanging plate 5 and fuselage 1 respectively.Can thus make for used by controller communication
Battery is arranged on the outside of fuselage 1, i.e. external battery, and to avoid in unmanned plane during flying, what battery was produced to controller can be competent
Disturb, it is ensured that unmanned plane flies on set route.
In the embodiment of the present invention, because battery compartment is external, the battery in battery compartment can use solar power generation, to save
The energy.In such cases, closed plate 6 can be made up of transparent material.
In addition, the weight in order to mitigate hanger b, can be provided with multiple lightening holes 9 on hanging plate 5.
With reference to Fig. 1 and Fig. 2, in the embodiment of the present invention, the unmanned plane also includes the support c for supporting fuselage 1, the support
C can include two groups of support components positioned opposite, and each support component includes two perpendicular supports 10 and a stulls 11, erects support
10 have first end and a second end, two first ends fixed installations of perpendicular support 10 on the fuselage 1, the of two perpendicular supports 10
Two ends are arranged in stull 11, are connected as one by connecting support 12 between the perpendicular support 10 in two groups of support components, to ensure
Support c overall steadiness.
With reference to Fig. 1 and Fig. 2, in the embodiment of the present invention, spray assembly a can include liquid reserve tank 13, hydraulic pump 14, multiple sprays
Pipe 15 and with the one-to-one shower nozzle 16 of jet pipe 15, liquid reserve tank 13 be arranged on hanger b away from fuselage 1 side lower section and positioned at branch
Between two groups of support components of frame c, hydraulic pump 14 is arranged on liquid reserve tank 13, and multiple jet pipes 15 are arranged at the outside of fuselage 1, spray
Pipe 15 has first end and the second end, and the first end of multiple jet pipes 15 is connected by hydraulic pump 14 with liquid reserve tank 13, many
The second end of individual jet pipe 15 extends to the diverse location in the outside of fuselage 1, and shower nozzle 16 is arranged on the second end of corresponding jet pipe 15
Portion.
With reference to Fig. 1 and Fig. 2, in the embodiment of the present invention, battery compartment 3 can also be arranged on support c two groups of support components it
Between, because liquid reserve tank 13 and battery compartment 3 can be arranged between two groups of support components of support c, so, support c can be right
Liquid reserve tank 13 and battery compartment 3 carry out certain protection, can to a certain extent prevent liquid reserve tank 13 and battery compartment 3 from being damaged by the external world
It is bad.
With reference to Fig. 1 and Fig. 2, in the embodiment of the present invention, spray assembly a can also include the support for installing liquid reserve tank 13
Frame d, support d include the top board 17 and base plate 18 that are oppositely arranged, and top board 17 passes through multiple screw rods 19 and is fixedly connected with hanging plate 5, pushes up
Connected by multiple fix bars 20 between plate 17 and base plate 18, multiple fix bars 20, top board 17 and base plate 18 surround one with storage
The FX that liquid case 13 matches, liquid reserve tank 13 is fixedly installed in the FX.
In the embodiment of the present invention, the bottom of liquid reserve tank 13 can with downwardly convex, be provided with base plate 18 with it is downwardly convex
The through hole that the bottom of liquid reserve tank 13 matches, the bottom of liquid reserve tank 13 plugs in through-holes, it is possible to achieve to determining for liquid reserve tank 13
Position, prevents unmanned plane liquid reserve tank 13 in flight from shaking.
Fig. 3 is the structural representation of the liquid reserve tank of the unmanned plane of the embodiment of the present invention, with reference to Fig. 3, in the embodiment of the present invention,
Some dividing plates 21 can be provided with liquid reserve tank 13, some dividing plates 21 will be divided into some interconnected independences in liquid reserve tank 13
Space, the liquor that can so cache in liquid reserve tank 13 is rocked during unmanned plane during flying and causes the shakiness of unmanned plane body
It is fixed, increase the stability of the flight of unmanned plane.
With reference to Fig. 3, in the embodiment of the present invention, dividing plate 21 can be provided with two, and two dividing plates 21 are in cross-shaped cloth
Put, two dividing plates 21 will be separated into four separate spaces inside liquid reserve tank 13, four separate spaces are interconnected.So, nobody
In flight, the mixed dynamic of liquid in liquid reserve tank 13 can be stopped machine by dividing plate 21, to cache impact of the liquid to liquid reserve tank 13, protect
Stability of the card unmanned plane in flight, it is ensured that the normal operation of plant protection.
With reference to Fig. 3, in the embodiment of the present invention, liquid reserve tank 13 can include upper lid 13a, lower cover 13b and side plate 13c, upper lid
The edge of 13a and the edge of lower cover 13b are connected by side plate 13c, and upper lid 13a, lower cover 13b and side plate 13c surround a closing
Storage room, the liquid for plant protection can be deposited in the locker room, the species of liquid can be divided into water body or agricultural chemicals, with realize
The anti-evil of irrigation of crops.
With reference to Fig. 3, in the embodiment of the present invention, upper lid 13a can be arc shape, and lower cover 13b can be disc, side plate
13c is arranged between lid 13a and lower cover 13b, and side plate 13c can be integral type structure with upper lid 13a and lower cover 13b,
Inlet and liquid outlet can be provided with upper lid 13a, to realize the absorption and discharge of liquid.
With reference to Fig. 3, in the embodiment of the present invention, each dividing plate 21 be respectively provided with top and bottom, the top of each dividing plate 21 and
Bottom is tightly connected with upper lid 13a and lower cover 13b respectively.
In the embodiment of the present invention, the first implementation of each separate space connection is：
Fig. 4 is that the structure of the first implementation of each separate space connection in the liquid reserve tank of the embodiment of the present invention is shown
Be intended to, with reference to Fig. 4, each dividing plate 21 is respectively provided with front-end and back-end, the front-end and back-end of each dividing plate 21 respectively with side plate 13c it
Between there is space, liquid flow in space, you can realize the interconnected of each separate space connection.
Fig. 5 is that the structure of second implementation of each separate space connection in the liquid reserve tank of the embodiment of the present invention is shown
It is intended to, with reference to Fig. 5, the front-end and back-end of each dividing plate 21 are tightly connected with side plate 13c, and in two bottoms of dividing plate 21
Portion is respectively provided with the opening for making four separate spaces interconnected, because liquid is flowed at the middle part of dividing plate 21, not only can be real
Existing four separate spaces are interconnected, and can also further cache impact of the liquid to liquid reserve tank side wall.
In the embodiment of the present invention, the third implementation of each separate space connection is：
Fig. 6 is that the structure of the third implementation of each separate space connection in the liquid reserve tank of the embodiment of the present invention is shown
It is intended to, with reference to Fig. 6, the front-end and back-end of each dividing plate 21 are tightly connected with side plate 13c, the both sides of the bottom of each dividing plate 21
It is respectively provided with the opening for making adjacent separate space interconnected.
In the embodiment of the present invention, slot can be provided with the inwall of lower cover 13c, the bottom of dividing plate 21 is plugged in slot 13c
In, to realize installation of the dividing plate 21 in liquid reserve tank 13.
Certainly, dividing plate 21 can be arranged in liquid reserve tank 13 using other connected modes, such as screw or bonding, the present invention
Embodiment is not limited herein to the connected mode that dividing plate 21 is arranged in liquid reserve tank 13.
In addition, in the embodiment of the present invention, can be provided with liquid level sensor in liquid reserve tank 13, liquid level sensor can pacify
On the inwall of lower cover 13c, can be with the sprinkling of stop liquid, save energy when there is no liquid in liquid reserve tank 13.
In the embodiment of the present invention, hydraulic pump 14 may be mounted at the bottom of liquid reserve tank 13, and the input port of hydraulic pump 14 can be with
It is connected with liquid outlet by a flexible pipe, to realize the discharge of the liquor in liquid reserve tank 21.
In the embodiment of the present invention, can in the liquid reserve tank 13 storage medicament or water, with the insect prevention for realizing to plant go evil and
Irrigation operation.
In the embodiment of the present invention, the jet pipe 15 and shower nozzle 16 of spray assembly a can be provided with two, two phases of jet pipe 15
To the left and right sides being arranged on during unmanned plane during flying, this set can be in the premise of the spray area for not reducing spray assembly a
Under, the quantity of spray assembly is farthest reduced, to streamline organizations.
In the embodiment of the present invention, spray assembly a can also include threeway 22, and the threeway 22 is arranged in connection support 12, three
Logical 22 have an import and two outlets, and the import of threeway 22 is connected with the delivery outlet of hydraulic pump 14, and two of threeway 22 go out
First end of the mouth respectively with two jet pipes 15 is connected.The liquor that hydraulic pump 14 is drawn from liquid reserve tank 13 can be by threeway 22
It is delivered in jet pipe 15, completes the conveying of liquor.
In the embodiment of the present invention, the side wall of shower nozzle 16 is provided with bolt hole, is provided with bolt hole and the cooperation of its screw thread
Adjusting screw rod, rotates adjusting screw rod, can adjust the pressure of the liquor that shower nozzle is sprayed.
In the embodiment of the present invention, positive-ion sheath can be coated with the inwall of shower nozzle 16, so, liquor sprays from shower nozzle
After can contain cation, and the anion of earth's surface attracts each other, so that liquor can preferably be absorbed.
Fig. 7 is the structural representation of the foldable implementation one of the horn of unmanned plane provided in an embodiment of the present invention, figure
11 is the structural representation of the folding implementation two of the horn of unmanned plane provided in an embodiment of the present invention, with reference to Fig. 7 and
Figure 11, in the embodiment of the present invention, horn 4 can include first connecting rod 4a and second connecting rod 4b, first connecting rod 4a and second connecting rod
4b is respectively provided with first end and the second end, and the first end of first connecting rod 4a is fixedly mounted on the fuselage 1, first connecting rod 4a's
The foldable connection of first end that the second end passes through folding device 8 and second connecting rod 4b, rotor 3 is arranged on second connecting rod 4b's
The second end, because first connecting rod 4a and second connecting rod 4b can realize the foldable of horn 4 by folding device 8, so, can
To reduce the floor space in unmanned plane, to facilitate transport.
In order to realize the foldable of horn 4, the folding device of the embodiment of the present invention has two kinds of implementations, respectively：
Implementation one：
With reference to Fig. 7, the folding device of the implementation one of the embodiment of the present invention includes：
First sleeve 8a, the first sleeve 8a is fixedly set on the second end of first connecting rod 4a, with first connecting rod 4a's
The second end is relatively set with the connections of first connecting portion 8b and second on the outer wall with the end of the first sleeve 8a of first end
Portion 8c；
Second sleeve 8d, second sleeve 8d is fixedly set on the first end of second connecting rod 4b, with second connecting rod 4b's
First end is relatively set with the 3rd connecting portion 8e and the 4th connection on the outer wall with the end of the second sleeve 8d of first end
Portion 8f, the 3rd connecting portion 8e is rotatably connected by first rotating shaft with second connecting portion 8c；
Grab 8g, grab 8g have first end and a second end, and the first end of grab 8g is by the second bearing pin and the
One connecting portion 8b is rotatably connected, and the second end of grab 8g is snapped connection with the 4th connecting portion 8f；
First bearing pin and the second bearing pin be arranged in parallel, and are each perpendicular to the central shaft of the first sleeve 4a.
In implementation one, when unmanned plane is in state of flight, the second end of grab 8g is buckled in the 4th connection
On portion 8f, first connecting rod 4a and second connecting rod 4b is in coaxial state, to realize flight and the spray function of unmanned plane；When nobody
Machine is in when working condition, and the second end of grab 8g and the 4th connecting portion 8f are separated from each other, and the 3rd can be made by external force
Connecting portion 8e and second connecting portion 8c realizes first connecting rod 4a and the foldable settings of second connecting rod 4b, i.e., around the second axis of rotation
The length of horn 4 can be changed, reduce the floor space of the unmanned plane in working condition is treated, to facilitate transport.
Fig. 8 is the structural representation of the first sleeve of the first implementation of horn folding in the embodiment of the present invention, knot
Close Fig. 8, the first connecting portion 8b of the embodiment of the present invention can include two the first otic placodes, two the first otic placodes are oppositely arranged on the
On the outer wall of one sleeve 8a, the two ends of first rotating shaft are secured across two the first otic placodes respectively.
In the embodiment of the present invention, two the first otic placodes and the first sleeve 8a can be integral type structure.
With reference to Fig. 8, the second connecting portion 8c of the embodiment of the present invention can include two the second otic placodes, two the second otic placode phases
To being arranged on the outer wall of the first sleeve 8a, the two ends of the second rotating shaft are secured across two the second otic placodes respectively.
In the embodiment of the present invention, two the second otic placodes and the first sleeve 8a can be integral type structure.
Fig. 9 is the structural representation of the second sleeve of the first implementation of horn folding in the embodiment of the present invention, knot
Close Fig. 9, the 3rd connecting portion 8e of the embodiment of the present invention can be that, in the first fixed block of strip, the first fixed block is provided with by the
The through hole that two rotating shaft activities are passed through, to realize being rotatably connected for the 3rd connecting portion 8e and second connecting portion 8c.
In the embodiment of the present invention, the 3rd connecting portion 8e and second sleeve 8d can be integral type structure.
With reference to Fig. 9, in the embodiment of the present invention, the 4th connecting portion 8f can be that, in the second hook-shaped fixed block, second fixes
The hook portion of block bends to away from the direction of first set cylinder 8a.
In the embodiment of the present invention, the 4th connecting portion 8f and second sleeve 8d can be integral type structure.
Figure 10 is the structural representation of the grab of the first implementation of horn folding in the embodiment of the present invention, with reference to figure
10, in the embodiment of the present invention, grab 8g can be with U-shaped, and grab 8g includes web and is located at the first wing plate of web both sides respectively
With the second wing plate, the first wing plate is provided with the through hole passed through by first rotating shaft, can with realize grab 8g and first connecting portion 8b
Connection is rotated, and the second wing plate can be snapped connection by fixture block 8h with the hook portion of the second fixed block.
Further, with reference to Figure 10, in the embodiment of the present invention, the middle part of fixture block 8h is by the 3rd bearing pin and the second of grab
Wing plate is rotatably connected, and the 3rd bearing pin is parallel to the first bearing pin and perpendicular to the central shaft of the first sleeve 8a, and fixture block 8h's is any
One end hook is located in the hook portion of the second fixed block, and when using, the hook portion moved not with the second fixed block by external force is engaged
Fixture block 8g one end, you can fixture block 8g is separated from the hook portion of the second fixed block.
With reference to Fig. 8, in the embodiment of the present invention, one section of first breach 8i can be provided with the side wall of the first sleeve 8a, the
One breach 8i extends from the either end of the first sleeve 8a to the middle part of the first sleeve 8a, to facilitate the first sleeve 8a to connect first
It is set with bar 4a, multigroup connector is provided with the side wall of the first sleeve 8a, every group of connector is included two connecting plates
8j, two connecting plate 8j are oppositely arranged on the both sides of the first breach 8i, and each connecting plate 8j is provided with bolt hole.By spiral shell
Bolt, you can realize the first sleeve 8a being fixedly installed on first connecting rod 4a.
In the embodiment of the present invention, the first breach 8i is preferably since the first sleeve 8a dorsad one end of second sleeve 8d to
The middle part of one sleeve 8a extends.
Certainly, the first sleeve being fixedly installed on first connecting rod can also use other modes, for example, the first sleeve mistake
Cooperation of being full of is first-class in first connecting rod, and the mode that is fixedly installed of the embodiment of the present invention to the first sleeve on first connecting rod is herein not
It is limited.
With reference to Fig. 9, in the embodiment of the present invention, one section of second breach 8k is provided with the side wall of second sleeve 8d, second lacks
Mouth 8k extends from the either end of second sleeve 8d to the middle part of second sleeve 8d, to facilitate second sleeve 8d in second connecting rod 4b
On be set with, be also equipped with multigroup connector on the side wall of second sleeve 8d, every group of connector includes two connecting plate 8j,
Two connecting plate 8j are oppositely arranged on the both sides of the second breach 8k, and each connecting plate 8j is provided with bolt hole.By bolt, i.e.,
It is capable of achieving second sleeve 8d being fixedly installed on second connecting rod 4b.
In the embodiment of the present invention, the second breach 8k is preferably since second sleeve 8d dorsad one end of the first sleeve 8a to
The middle part of two sleeve 8d extends.
Certainly, second sleeve being fixedly installed on second connecting rod can also use other modes, for example, second sleeve mistake
Cooperation of being full of is first-class in second connecting rod, and the mode that is fixedly installed of the embodiment of the present invention to second sleeve on second connecting rod is herein not
It is limited.
Implementation two：
Figure 12 is the structural representation of the first sleeve of second implementation of horn folding in the embodiment of the present invention, figure
13 is the structural representation of the second sleeve of second implementation of horn folding in the embodiment of the present invention, with reference to Figure 11, figure
12 and Figure 13, the folding device of the implementation two of the embodiment of the present invention includes：
First sleeve 8a, the first sleeve 8a is fixedly set on the second end of first connecting rod 4a, with first connecting rod 4a's
The second end is relatively set with the connections of first connecting portion 8b and second on the outer wall with the end of the first sleeve 8a of first end
Portion 8c, first connecting portion 8b has sealed space；
Lock assembly, lock assembly includes control-rod 8o, gag lever post 8p and return springs 8q, and control-rod 8o has first
End and the second end, the first end of control-rod 8o are located at first connecting portion 8b outsides, the two ends difference of return springs 8q
It is connected with the first end and first connecting portion 8b of control-rod 8o, the second end of control-rod 8o is extend into sealed space, is limited
Position bar 8p is located in sealed space, and gag lever post 8p is vertically and fixedly arranged on control-rod 8o；
Second sleeve 8d, second sleeve 8d is fixedly set on the first end of second connecting rod 4b, with second connecting rod 4b's
First end is relatively set with the 3rd connecting portion 8e and the 4th connection on the outer wall with the end of the second sleeve 8d of first end
Portion 8f, the 3rd connecting portion 8e is rotatably connected by the 3rd rotating shaft with second connecting portion 8c, and the 3rd rotating shaft is perpendicular to second sleeve
The central shaft of 8d；
Grab 8g, grab 8g is fixedly installed on the 4th connecting portion 8f, and grab 8g is extend into sealed space, grab 8g with
Gag lever post 8p is operably separated or engaged.
When in use, the gag lever post in lock assembly is fastened in grab unmanned plane of the invention, the reset of lock assembly
Elastic component provides coupling mechanism force, prevents gag lever post from departing from from grab, and unmanned plane is normally used；When the horn of unmanned plane needs to fold
When, the control-rod movement in lock assembly is promoted, gag lever post is departed from from grab, now, at first connecting rod and second connecting rod
In the state being rotatably connected, second connecting rod is rotated, you can realize the relative upset of first connecting rod and second connecting rod, make the horn can
To fold gathering, so that horn shortens, to reduce taking up room when unmanned plane is integrally deposited, and convenient transport.
With reference to Figure 12, in the embodiment of the present invention, first connecting portion 8b can be that, in the first fixed block of strip, first fixes
Block be provided with along the first sleeve 8a axially through groove, the groove is sealed space.
With reference to Figure 12, in the embodiment of the present invention, return springs 8q can be the compression spring being sleeved on control-rod 8o,
In such cases, the hook portion of grab 8g need to extend to the direction of the 3rd connecting portion 8e, when gag lever post 8p is fastened on the hook of grab 8g
During portion, due to the reset response of compression spring, can prevent gag lever post 8p from departing from from the hook portion of grab 8g.
With reference to Figure 12, in the embodiment of the present invention, cover plate 8m can be fixedly installed on the first end of control-rod 8o, with side
Just control-rod 8o is operated.
With reference to Figure 12, in the embodiment of the present invention, the middle part of gag lever post 8p can be fixedly installed on control-rod 8o, and grab
8g can be provided with two, and two grab 8g are mounted opposite in the both sides of control-rod 8o, due to using two grab 8g and one
Gag lever post 8p is engaged, it is thus possible to improve coupling mechanism force when horn is in not folded state, it is ensured that unmanned plane normally runs.
In addition, can be fixedly installed a guide plate 8n in sealed space, guide plate 8n is parallel to gag lever post 8p
Set, the middle part of guide plate 8n can be provided with the pilot hole slid through for the second end of control-rod 8o, so can be right
The operation of control-rod 8o is oriented to.
With reference to Figure 12, in the embodiment of the present invention, second connecting portion 8c can include two otic placodes, and two otic placodes are oppositely arranged
On the outer wall of the first sleeve 8a, the two ends of the 3rd rotating shaft are divided to and are secured across two otic placodes.
In the embodiment of the present invention, the first sleeve 8a and first connecting portion 8b and second connecting portion 8c positioned at its both sides can be with
It is integral type structure.
With reference to Figure 13, in the embodiment of the present invention, the 3rd connecting portion 8e can also be that, in the second fixed block of strip, second consolidates
Determine between block two otic placodes of setting, the second fixed block is provided with the through hole passed through by the 3rd rotating shaft activity, to realize the 3rd connection
Portion 8e is rotatably connected with second connecting portion 8c's.
With reference to Figure 13, in the embodiment of the present invention, the 4th connecting portion 8f can also be in the 3rd fixed block of strip, two cards
Hook 8g is fixedly installed on the 3rd fixed block.
With reference to Figure 13, in the embodiment of the present invention, second sleeve 8d, the 3rd connecting portion 8e, the 4th connecting portion 8f and two cards
Hook 8g can be integral type structure.
With reference to Figure 13, in the embodiment of the present invention, the connected mode and second sleeve 8d of the first sleeve 8a and first connecting rod 4a
Connected mode with second connecting rod 4b is similar, and the embodiment of the present invention is not described herein.
The embodiment of the present invention by the horn 4 that rotor 2 and fuselage 1 are connected due to being divided into the first connecting rod connected by folding device
And second connecting rod, the folding of horn can be realized by folding device due to two connecting rods, so, it is possible to reduce in unmanned plane
Floor space, to facilitate transport.
The foregoing is only presently preferred embodiments of the present invention, be not intended to limit the invention, it is all it is of the invention spirit and
Within principle, any modification, equivalent substitution and improvements made etc. should be included within the scope of the present invention.
Claims (9)
1. a kind of anti-tampering unmanned plane, the unmanned plane includes fuselage, controller, spray assembly, multiple rotors and multiple horns,
The spray assembly is arranged on the fuselage, and the multiple rotor is equiangularly spaced by corresponding the horn of setting with it
The fuselage outer side is arranged in, the controller for controlling the unmanned plane during flying is arranged in the fuselage, it is characterised in that
The unmanned plane also includes the battery compartment built with battery, and the battery compartment is arranged on the external fuselage by hanger,
The hanger includes hanging plate, closed plate and multiple peg, and the bottom of the hanging plate and the fuselage is oppositely arranged, the hanging plate court
Mounting groove is provided with side to the fuselage, the battery compartment is arranged in the mounting groove, and the closed plate is covered in
On the mounting groove, the two ends of the multiple peg are fixedly connected with the hanging plate and the fuselage respectively.
2. anti-tampering unmanned plane according to claim 1, it is characterised in that the unmanned plane also includes described for supporting
The support of fuselage, the support includes two groups of support components positioned opposite, and each described support component includes two perpendicular supports
With a stull, with first end and the second end, the first ends of described two perpendicular supports are fixedly mounted on institute for the perpendicular support
State on fuselage, the second end of described two perpendicular supports is arranged in the stull, the described perpendicular support in support component described in two groups
Between by connect support connection.
3. anti-tampering unmanned plane according to claim 2, it is characterised in that the spray assembly includes liquid reserve tank, hydraulic pressure
Pump, multiple jet pipe and with the one-to-one shower nozzle of the jet pipe, the liquid reserve tank is arranged on the hanger away from the fuselage
Side lower section, the liquid reserve tank is located between two groups of support components of the support, and the hydraulic pump is arranged on the liquid reserve tank
On, the multiple jet pipe is arranged at the fuselage outer side, and the jet pipe has first end and the second end, the multiple spray
The first end of pipe is connected by the hydraulic pump with the liquid reserve tank, and the second end of the multiple jet pipe extends to the machine
Diverse location on the outside of body, the shower nozzle is arranged on the second end of the corresponding jet pipe.
4. anti-tampering unmanned plane according to claim 3, it is characterised in that the spray assembly is also included for installing institute
The support of liquid reserve tank is stated, the support includes the top board and base plate that are oppositely arranged, and the top board passes through multiple screw rods and the extension
Plate is fixedly connected, and is connected by multiple fix bars between the top board and the base plate, the multiple fix bar, the top board and
The base plate surrounds a FX matched with the liquid reserve tank, and the liquid reserve tank is fixedly installed on the FX
It is interior.
5. the anti-tampering unmanned plane stated according to claim 3, it is characterised in that the jet pipe and shower nozzle of the spray assembly are respectively provided with
There are two, two jet pipes are oppositely arranged；The spray assembly also includes threeway, and the threeway is arranged on the connection support
On, the threeway has an import and two outlets, and the import of the threeway is connected with the delivery outlet of the hydraulic pump, described
First end of two outlets of threeway respectively with two jet pipes is connected.
6. anti-tampering unmanned plane according to claim 3, it is characterised in that the side wall of the shower nozzle is provided with bolt hole,
The adjusting screw rod coordinated with its screw thread is provided with the bolt hole.
7. the anti-tampering unmanned plane according to claim any one of 1-6, it is characterised in that the horn includes first connecting rod
And second connecting rod, the first connecting rod and second connecting rod are respectively provided with first end and the second end, the first of the first connecting rod
End is fixedly mounted on the fuselage, the second end of the first connecting rod pass through folding device and the second connecting rod the
The foldable connection of one end, the rotor is arranged on the second end of the second connecting rod.
8. anti-tampering unmanned plane according to claim 7, it is characterised in that the folding device includes：
First sleeve, the first sleeve is fixedly set on the second end of the first connecting rod, with the first connecting rod
The second end is relatively set with first connecting portion and the second connection on the outer wall with the end of the first sleeve of first end
Portion；
Second sleeve pipe, second sleeve pipe is fixedly set on the first end of the second connecting rod, with the second connecting rod
First end is relatively set with the 3rd connecting portion and the 4th connection on the outer wall with the end of second sleeve pipe of first end
Portion, the 3rd connecting portion is rotatably connected by first rotating shaft with the second connecting portion；
Grab, the grab has first end and a second end, the first end of the grab by the second bearing pin with it is described
First connecting portion is rotatably connected, and the second end of the grab is snapped connection with the 4th connecting portion；
First bearing pin and second bearing pin be arranged in parallel, and are each perpendicular to the central shaft of the first sleeve.
9. anti-tampering unmanned plane according to claim 7, it is characterised in that the folding device includes：
First sleeve, first sleeve is fixedly set on the second end of the first connecting rod, with the first connecting rod
The second end is relatively set with first connecting portion and the second connection on the outer wall with the end of first sleeve of first end
Portion, the first connecting portion has sealed space；
Lock assembly, the lock assembly includes control-rod, gag lever post and return springs, and the control-rod has first end
And the second end, the first end of the control-rod is positioned at first connecting portion outside, the two ends point of the return springs
It is not connected with the first end and the first connecting portion of the control-rod, the second end of the control-rod extend into the lock
Close in space, the gag lever post is located in the sealed space, and the gag lever post is vertically and fixedly arranged on the control-rod；
Second sleeve, the second sleeve is fixedly set on the first end of the second connecting rod, with the second connecting rod
First end is relatively set with the 3rd connecting portion and the 4th connection on the outer wall with the end of the second sleeve of first end
Portion, the 3rd connecting portion is rotatably connected by the 3rd rotating shaft and the second connecting portion, and the 3rd rotating shaft is perpendicular to institute
State the central shaft of second sleeve；
Grab, the grab is fixedly installed on the 4th connecting portion, and the grab is extend into the sealed space, described
Grab is operably separated or engaged with the gag lever post.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611261420.0A CN106828897A (en) | 2016-12-30 | 2016-12-30 | Anti-tampering unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611261420.0A CN106828897A (en) | 2016-12-30 | 2016-12-30 | Anti-tampering unmanned plane |
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| Publication Number | Publication Date |
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| CN106828897A true CN106828897A (en) | 2017-06-13 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201611261420.0A Pending CN106828897A (en) | 2016-12-30 | 2016-12-30 | Anti-tampering unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018184095A1 (en) * | 2017-04-07 | 2018-10-11 | Hanna Mark Holbrook | Distributed-battery aerial vehicle and a powering method therefor |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104654213A (en) * | 2013-11-22 | 2015-05-27 | 海洋王（东莞）照明科技有限公司 | Hasp structure of lamp and anti-dazzle floodlight lamp with hasp structure |
| CN105253304A (en) * | 2015-11-03 | 2016-01-20 | 南京林业大学 | Multi-rotor unmanned aerial vehicle variable spraying system |
| CN205044951U (en) * | 2015-10-22 | 2016-02-24 | 深圳市科卫泰实业发展有限公司 | Folding many rotor unmanned aerial vehicle of horn |
| CN205469808U (en) * | 2016-03-18 | 2016-08-17 | 苏州丰积能源科技有限公司 | Photovoltaic power plant detection device |
| CN106114839A (en) * | 2016-07-28 | 2016-11-16 | 顺丰科技有限公司 | A kind of unmanned plane |
-
2016
- 2016-12-30 CN CN201611261420.0A patent/CN106828897A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104654213A (en) * | 2013-11-22 | 2015-05-27 | 海洋王（东莞）照明科技有限公司 | Hasp structure of lamp and anti-dazzle floodlight lamp with hasp structure |
| CN205044951U (en) * | 2015-10-22 | 2016-02-24 | 深圳市科卫泰实业发展有限公司 | Folding many rotor unmanned aerial vehicle of horn |
| CN105253304A (en) * | 2015-11-03 | 2016-01-20 | 南京林业大学 | Multi-rotor unmanned aerial vehicle variable spraying system |
| CN205469808U (en) * | 2016-03-18 | 2016-08-17 | 苏州丰积能源科技有限公司 | Photovoltaic power plant detection device |
| CN106114839A (en) * | 2016-07-28 | 2016-11-16 | 顺丰科技有限公司 | A kind of unmanned plane |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018184095A1 (en) * | 2017-04-07 | 2018-10-11 | Hanna Mark Holbrook | Distributed-battery aerial vehicle and a powering method therefor |
| US10822082B2 (en) | 2017-04-07 | 2020-11-03 | Mark Holbrook Hanna | Distributed-battery aerial vehicle and a powering method therefor |
| US11811224B2 (en) | 2017-04-07 | 2023-11-07 | Mark Holbrook Hanna | Distributed-battery aerial vehicle and a powering method therefor |
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