CN109110101A - A kind of novel plant protection unmanned plane - Google Patents
A kind of novel plant protection unmanned plane Download PDFInfo
- Publication number
- CN109110101A CN109110101A CN201811108331.1A CN201811108331A CN109110101A CN 109110101 A CN109110101 A CN 109110101A CN 201811108331 A CN201811108331 A CN 201811108331A CN 109110101 A CN109110101 A CN 109110101A
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- Prior art keywords
- rack
- motor
- unmanned plane
- horn
- medicine
- Prior art date
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 17
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 12
- 239000007788 liquid Substances 0.000 claims description 31
- 238000005119 centrifugation Methods 0.000 claims description 14
- 239000012530 fluid Substances 0.000 claims description 10
- 229910000838 Al alloy Inorganic materials 0.000 claims description 5
- 230000003014 reinforcing effect Effects 0.000 claims description 5
- 239000003814 drug Substances 0.000 claims description 4
- 238000007789 sealing Methods 0.000 claims description 4
- 230000005611 electricity Effects 0.000 claims 1
- 238000012423 maintenance Methods 0.000 abstract description 15
- 238000013461 design Methods 0.000 abstract description 6
- 238000005457 optimization Methods 0.000 abstract description 4
- 238000010276 construction Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 8
- 238000000034 method Methods 0.000 description 4
- 238000013016 damping Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 230000010412 perfusion Effects 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 206010000369 Accident Diseases 0.000 description 1
- 239000006096 absorbing agent Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000012876 topography Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
-
- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
-
- 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
- B64C25/64—Spring shock-absorbers; Springs using rubber or like elements
-
- 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
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses a kind of novel plant protection unmanned planes, it is characterized by comprising rack, battery component, medicine-chest, fly control module, horn, electric machine assembly and foot prop, the battery component, medicine-chest and winged control module are arranged in rack, the top of the rack is equipped with upper carbon plate, the bottom of the rack is equipped with lower carbon plate, one end of the horn and the outside of rack connect, the other end of the horn is connect with electric machine assembly, the bottom of the lower carbon plate is equipped with section board and water pump, the front end of the connection of the outside of the foot prop and rack, the rack is equipped with head-shield.Novel plant protection unmanned plane of the invention is made that optimization for traditional unmanned plane, and under the premise of stable structure, firm, using fairshaped design, the battery of same capacity can increase the time of operation, more efficient；The construction of body frame posture does not need large area in the maintenance of later period circuit system, maintenance and removes, it is high generally to embody convenient, resilient degree.
Description
Technical field
The present invention relates to agricultural plant protection air vehicle technique fields, and in particular to a kind of novel plant protection unmanned plane.
Background technique
The unmanned plane of mainstream at present interacts in the cooperation of self structure, and changing is obtained very much in terms of complete machine structure intensity
It is kind；Considerably increase the rigidity of complete machine.
But there is also following disadvantages for current plant protection drone:
1, because of self structure moulding system the reason of, aerodynamic streamlined configuration is not met, so that aircraft operation
When, need to overcome the resistance of advance big, cause power loss to increase in this way, prevent battery from adequately utilizing.
2, after aircraft collides, horn fracture causes Internal cable water pipe to be torn.
3, as unmanned plane core inner cabin, all electronic hardware modules all concentrate on the inside, occur in unmanned plane
When colliding, fuselage falls apart, and is unable to protective module, in the case where repairing, inconvenience maintenance；Needing all to disassemble can
Maintenance, so, traditional structure system is unfavorable for the maintenance of unmanned plane.
4, after operation, the maintenance of complete machine is carried out, inevitably carries out water cleaning, and core part is without waterproof function
Can, be easy electronic module is damaged, be not easy to operation it is complete after maintenance.
Summary of the invention
The purpose of the invention is to overcome the deficiencies of the prior art and provide a kind of novel plant protection unmanned plane, for tradition
Unmanned plane is made that optimization, and under the premise of stable structure, firm, using fairshaped design, the battery of same capacity can increase
Add the time of operation, it is more efficient；The construction of body frame posture does not need large area in the maintenance of later period circuit system, maintenance
It removes, it is high generally to embody convenient, resilient degree.
The present invention is implemented as follows:
A kind of novel plant protection unmanned plane, it is characterised in that: including rack, battery component, medicine-chest, fly control module, horn, motor group
Part and foot prop, the battery component, medicine-chest and winged control module are arranged in rack, and the top of the rack is equipped with upper carbon plate, institute
The bottom for stating rack is equipped with lower carbon plate, and one end of the horn and the outside of rack connect, the other end and motor of the horn
Component connection, the bottom of the lower carbon plate are equipped with section board and water pump, and the outside of the foot prop and rack connects, the rack
Front end is equipped with head-shield.
The present invention is further preferred, is set in the rack there are two demarcation plate, the rear end of the rack is equipped with mounting post, institute
The front end for stating rack is equipped with protection protrusion, and the bottom of the front end of rack is equipped with wire casing, and the wire casing is two, described in two
Fixture block is equipped between wire casing.
The present invention is further preferred, and the top of the medicine-chest is outlet end, outlet end bottom liquid outlet, the liquid out
Mouth is equipped with forced locking device, and the lower part of the medicine-chest is equipped with medical liquid container, and the top of the medicine-chest is equipped with inlet, described
Inlet is equipped with feed liquor lid, and the bottom of the medical liquid container is equipped with leakage fluid dram, and the leakage fluid dram is equipped with bottom cover, the medicine-chest
Interior to be equipped with outlet tube, one end of the outlet tube extends to leakage fluid dram, and the other end of outlet tube is connect with forced locking device.
The present invention is further preferred, and the forced locking device includes inlet valve, shell, liquid output element and spring, it is described into
The lower part of shell is arranged in water valve and cage connection, the liquid output element, and the spring is arranged at inlet valve and cage connection
In inner cavity, sealing ring is equipped at the inlet valve and cage connection.
The present invention is further preferred, and the electric machine assembly includes motor cabinet, motor, centrifugal energy nozzle and blade, the motor
The top of motor cabinet is set, and the bottom of motor cabinet is arranged in the centrifugal energy nozzle, and the top of motor is arranged in the blade.
The present invention is further preferred, and the rear end of the motor cabinet is equipped with horn interconnecting piece, and the front end of the motor cabinet is equipped with
Anticollision rubber, the anticollision rubber are equipped with fixed strip, and the anticollision rubber is connect by fixed strip with motor cabinet, described
The two sides of horn interconnecting piece are equipped with reinforcing rib.
The present invention is further preferred, and the centrifugal energy nozzle includes upper cover, yielding rubber, centrifugal energy nozzle shell, motor fastening
Part, centrifugation motor and centrifugal turntable, the yielding rubber are arranged between upper cover and centrifugal energy nozzle shell, the motor fastener
The lower section of centrifugal energy nozzle shell is set, motor housing is equipped in the motor fastener, the centrifugation motor is arranged in motor
In shell, the lower part of the centrifugation motor is equipped with water proof rubber, and the bottom of the centrifugation motor is equipped with centrifugal pan rotating member, described
Centrifugal turntable is connect with centrifugal pan rotating member, and the bottom of the motor fastener is equipped with lower cover.
The present invention is further preferred, and the cross section of the foot prop is V-shaped structure, the thickness of the foot prop from top to bottom by
Decrescence small, the foot prop includes front foot frame, rear leg and connecting plate, one end connection of the front foot frame and connecting plate, after described
The junction of the connection of the other end of foot prop and connecting plate, the foot prop and connecting plate is equipped with rubber block.
The present invention is further preferred, the horn be circular hollow structure, the horn be from outside to inside Carbon fibe layer and
Aluminium alloy layer.
Present invention substantive distinguishing features outstanding and significant progress are:
1, novel plant protection unmanned plane of the invention is made that optimization for traditional unmanned plane, in stable structure, firm premise
Under, using fairshaped design, front face area is smaller, and air aerodynamic drag is smaller, and the battery of same capacity can increase operation
It is time, more efficient；Most of load-bearing is completed by mesh font frame, ensure that entire nothing by the construction of body frame posture
Man-machine high intensity, later period circuit system maintenance, maintenance do not need large area remove, generally embody it is convenient, can answer
Former degree is high.
2, unmanned plane entirety streamlined configuration, air pneumatic drag coefficient is 0.5 hereinafter, the head-shield of unmanned plane, medicine-chest, foot
Frame etc. all carries out incorporating fairshaped design, can reduce vortex effect or avoid the formation being vortexed, to greatly lower
Resistance of the fluid to it, improves battery utilization rate, reduces the loss of power, to ensure that under strong wind weather handling situations
The safety of aircraft.
3, the present invention uses mesh font rack, is connected and fixed mode for tradition and is made that optimization, using rack as support force,
Under the premise of multiclass connector and fixed rack, main structure is flexible and changeable, and intensity is good, is unlikely to deform, and structure type is brief,
And it is lighter, removable technique ensure that the intensity and flatness of entire unmanned plane, and to internal module, electronic component
It is easy to maintain and maintenance.
4, the present invention uses plug-in medicine-chest, can plug from unmanned plane at any time, can be more after extracting medicine-chest from unmanned plane
It changes transfer place and carries out perfusion, the position insertion unmanned plane of aircraft is returned again to after the completion of perfusion, facilitate unmanned plane can be
Operation is with a varied topography, and explosive barrel is not easy to the place moved to, and medicine-chest uses fairshaped design, cooperates with airframe, reduces wind
Resistance promotes flight efficiency；Medicine-chest liquid outlet passes through peripheral hardware water pump automatic outletting, when medicine-chest is extracted from aircraft, medicine-chest liquid outlet
There is forced locking device, liquid outlet can be blocked, prevent liquid medicine from outflowing；When medicine-chest is inserted into aircraft, automatically lock dress
Unlock is set, at this moment the liquid outlet of medicine-chest is open-minded, and liquid medicine can be extracted out by the liquid medicine in the pump handle medicine-chest in fuselage, thus
The liquid outlet that intelligence locks medicine-chest is realized, the liquid outlet of medicine-chest is automatically opened.
5, battery plug-in powers on, and working efficiency is higher, is more convenient battery maintenance.
6, unmanned plane motor cabinet main body of the invention uses frame-type hollow structure, when motor cabinet is by side impact,
Tower structure forms flexible deformation to cushion impact forces in side；It is outstanding using rubber by the way that anticollision rubber is arranged
Shock resistance absorbs energy when hitting, further enhances the impact resistance of motor cabinet；Motor cabinet ontology is connect with horn
It is equipped with reinforcing rib on the outside of the junction in portion, greatly eliminates the phenomenon that stress is concentrated when colliding, increases motor cabinet intensity and shock resistance
Performance is broken it easily.
7, horn of the invention encases an institutional structure of aluminium alloy layer using carbon fiber, and intensity has obtained significant increase；
And collide or aircraft bombing after, fracture separation does not occur for horn, ensure that the cable or water pipe inside horn will not be pulled apart；Machine
The combination of arm end is assembled with an aluminum alloy connector, and connector is linked and packed with rack, this ensure that the one of entire horn
Cause property, while horn can carry out disassembly technique, ensure that aircraft collides or when aircraft bombing, fuselage will not fall apart, maintenance fuselage
The rigidity of framework ensure that fuselage interior system is unaffected, facilitate care and maintenance.
8, complete machine seals waterproof, and effective protection electronic component uses safe.
9, centrifugal energy nozzle of the invention makes it have the function of anticollision and damping, anticollision by increasing yielding rubber
Function greatly reduces spray head and aircraft accident is occurring and is carrying the probability damaged when collision；Improve the sprinkling effect of centrifugal energy nozzle
Fruit improves the service life of electronic component and motor；It is more convenient to install, and versatility is stronger, and user buys
It is mounted directly, does not need additional designs mounting shock absorber, damping rubber rubber and half clad type fastening structure of centrifugal energy nozzle shell,
Product appearance is more neat and artistic in the case where meeting structural strength.
10, foot prop of the invention, which uses, meets aerodynamic streamlined configuration, greatly reduces air and pneumatically hinders
Force coefficient reduces the loss of power indirectly, substantially increases the utilization rate of battery, foot prop bottom is mounted with rubber block, and matches
The conjunction distinctive toughness of carbon fiber, integrally formed foot prop, when aircraft landing, in addition the characteristic of rubber block material itself,
Play the role of damping, buffering, foot prop has obtained protective effect.
Detailed description of the invention
Fig. 1 is a kind of three-dimensional structure diagram of novel plant protection unmanned plane of the present invention.
Fig. 2 is a kind of decomposition chart of novel plant protection unmanned plane of the present invention.
Fig. 3 is the structural schematic diagram of the frame of the invention 1.
Fig. 4 is the structural schematic diagram of medicine-chest of the present invention.
Fig. 5 is the structural schematic diagram of forced locking device of the present invention.
Fig. 6 is the structural schematic diagram of electric machine assembly of the present invention.
Fig. 7 is the structural schematic diagram of motor cabinet of the present invention.
Fig. 8 is the structural schematic diagram of centrifugal energy nozzle of the present invention.
Fig. 9 is the structural schematic diagram of present invention folding foot prop.
The opposite component names of serial number in figure:
Rack 1, medicine-chest 3, flies control module 4, upper carbon plate 5, lower carbon plate 6, horn 7, electric machine assembly 8, head-shield 9, divides at battery component 2
Battery plate 10, foot prop 12, demarcation plate 101, mounting post 102, wire casing 103, fixture block 104, protects raised 105, outlet end at water pump 11
201, medical liquid container 202, feed liquor lid 203, bottom cover 204, outlet tube 205, forced locking device 206, inlet valve 207, sealing ring
208, shell 209, liquid output element 210, spring 211, motor cabinet 801, motor 802, centrifugal energy nozzle 803, blade 804, horn connection
Portion 805, anticollision rubber 806, fixed strip 807, reinforcing rib 808, upper cover 809, yielding rubber 810, centrifugal energy nozzle shell 811,
Motor fastener 812, motor housing 813, centrifugation motor 814, water proof rubber 815, lower cover 816, centrifugal turntable 817, centrifugal pan
Rotating member 818, front foot frame 1201, rear leg 1202, connecting plate 1203, rubber block 1204.
Specific embodiment
A kind of novel plant protection unmanned plane of the present invention is further described with reference to the accompanying drawings and embodiments.
Embodiment 1
As shown in Figs. 1-2, a kind of novel plant protection unmanned plane of the invention, including rack 1, battery component 2, medicine-chest 3, winged control module
4, horn 7, electric machine assembly 8 and foot prop 12, the battery component 2, medicine-chest 3 and winged control module 4 are arranged in rack 1, the machine
The top of frame 1 is equipped with upper carbon plate 5, and the bottom of the rack 1 is equipped with lower carbon plate 6, one end of the horn 7 and the outside of rack 1
Connection, the other end of the horn 7 are connect with electric machine assembly 8, and the bottom of the lower carbon plate 6 is equipped with section board 10 and water pump 11,
The foot prop 12 is connect with the outside of rack 1, and the front end of the rack 1 is equipped with head-shield 9.
As shown in figure 3, being set in the rack 1 there are two demarcation plate 101, the rear end of the rack 1 is equipped with mounting post 102,
The front end of the rack 1 is equipped with protection protrusion 105, and the bottom of 1 front end of rack is equipped with wire casing 103, and the wire casing 103 is two
It is a, fixture block 104 is equipped between wire casing 103 described in two.
As shown in figure 4, the top of the medicine-chest 3 is outlet end 201, the 201 bottom liquid outlet of outlet end, the liquid out
Mouth is equipped with forced locking device 206, and the lower part of the medicine-chest 3 is equipped with medical liquid container 202, the top of the medicine-chest 3 be equipped with into
Liquid mouth, the inlet are equipped with feed liquor lid 203, and the bottom of the medical liquid container 202 is equipped with leakage fluid dram, sets on the leakage fluid dram
There is bottom cover 204, is equipped with outlet tube 205 in the medicine-chest 3, one end of the outlet tube 205 extends to leakage fluid dram, outlet tube 205
The other end connect with forced locking device 206.
As shown in figure 5, the forced locking device 206 includes inlet valve 207, shell 209, liquid output element 210 and spring
211, the inlet valve 207 is connect with shell 209, and the lower part of shell 209 is arranged in the liquid output element 210, and the spring 211 is set
It sets in the inner cavity of inlet valve 207 Yu 209 junction of shell, the inlet valve 207 is equipped with sealing ring with 209 junction of shell
208。
As shown in fig. 6, the electric machine assembly 8 includes motor cabinet 801, motor 802, centrifugal energy nozzle 803 and blade 804, institute
The top that motor cabinet 801 is arranged in motor 802 is stated, the bottom of motor cabinet 801, the blade is arranged in the centrifugal energy nozzle 803
804 are arranged in the top of motor 802.
As shown in fig. 7, the rear end of the motor cabinet 801 is equipped with horn interconnecting piece 805, the front end of the motor cabinet 801 is set
There is anticollision rubber 806, the anticollision rubber 806 is equipped with fixed strip 807, and the anticollision rubber 806 passes through fixed strip 807
It is connect with motor cabinet 801, the two sides of the horn interconnecting piece 805 are equipped with reinforcing rib 808.
As shown in figure 8, the centrifugal energy nozzle 803 includes upper cover 809, yielding rubber 810, centrifugal energy nozzle shell 811, motor
Fastener 812, centrifugation motor 814 and centrifugal turntable 817, the yielding rubber 810 are arranged in upper cover 809 and centrifugal energy nozzle shell
Between 811, the lower section of centrifugal energy nozzle shell 811 is arranged in the motor fastener 812, is equipped in the motor fastener 812
Motor housing 813, the centrifugation motor 814 are arranged in motor housing 813, and the lower part of the centrifugation motor 814 is equipped with waterproof
Rubber 815, the bottom of the centrifugation motor 814 are equipped with centrifugal pan rotating member 818, and the centrifugal turntable 817 is rotated with centrifugal pan
Part 818 connects, and the bottom of the motor fastener 812 is equipped with lower cover 816.
As shown in figure 9, the cross section of the foot prop 12 is V-shaped structure, the thickness of the foot prop 12 is from top to bottom gradually
Reduce, the foot prop 12 includes front foot frame 1201, rear leg 1202 and connecting plate 1203, the front foot frame 1201 and connecting plate
1203 one end connection, the rear leg 1202 are connect with the other end of connecting plate 1203, the foot prop and connecting plate 1203
Junction is equipped with rubber block 1204.
The horn 7 is circular hollow structure, and the horn 7 is Carbon fibe layer and aluminium alloy layer from outside to inside.
Although the embodiments of the present invention have been disclosed as above, but its is not only in the description and the implementation listed
With it can be fully applied to various fields suitable for the present invention, for those skilled in the art, can be easily
Realize other modification, therefore without departing from the general concept defined in the claims and the equivalent scope, the present invention is simultaneously unlimited
In specific details and legend shown and described herein.
Claims (9)
1. a kind of novel plant protection unmanned plane, it is characterised in that: including rack (1), battery component (2), medicine-chest (3), fly control module
(4), horn (7), electric machine assembly (8) and foot prop (12), the battery component (2), medicine-chest (3) and winged control module (4) setting exist
In rack (1), the top of the rack (1) is equipped with upper carbon plate (5), and the bottom of the rack (1) is equipped with lower carbon plate (6), described
One end of horn (7) is connect with the outside of rack (1), and the other end of the horn (7) is connect with electric machine assembly (8), under described
The bottom of carbon plate (6) is equipped with section board (10) and water pump (11), and the foot prop (12) connect with the outside of rack (1), the machine
The front end of frame (1) is equipped with head-shield (9).
2. a kind of novel plant protection unmanned plane according to claim 1, it is characterised in that: there are two being set on the rack (1)
The rear end of demarcation plate (101), the rack (1) is equipped with mounting post (102), and the front end of the rack (1) is equipped with protection protrusion
(105), the bottom of rack (1) front end is equipped with wire casing (103), and the wire casing (103) is wire casing described in two, two
(103) fixture block (104) are equipped between.
3. a kind of novel plant protection unmanned plane according to claim 1, it is characterised in that: the top of the medicine-chest (3) is
Liquid end (201), outlet end (201) bottom liquid outlet, the liquid outlet are equipped with forced locking device (206), the medicine
The lower part of case (3) is equipped with medical liquid container (202), and the top of the medicine-chest (3) is equipped with inlet, and the inlet is equipped with feed liquor
It covers (203), the bottom of the medical liquid container (202) is equipped with leakage fluid dram, and the leakage fluid dram is equipped with bottom cover (204), the medicine-chest
(3) outlet tube (205) are equipped in, one end of the outlet tube (205) extends to leakage fluid dram, the other end of outlet tube (205) with
Forced locking device (206) connection.
4. a kind of plug-in plant protection drone medicine-chest according to claim 3, it is characterised in that: the forced locking device
It (206) include inlet valve (207), shell (209), liquid output element (210) and spring (211), the inlet valve (207) and shell
(209) it connects, in the lower part of shell (209), the spring (211) is arranged in inlet valve (207) for liquid output element (210) setting
In the inner cavity of shell (209) junction, the inlet valve (207) and shell (209) junction are equipped with sealing ring (208).
5. a kind of novel plant protection unmanned plane according to claim 1, it is characterised in that: the electric machine assembly (8) includes electricity
Base (801), motor (802), centrifugal energy nozzle (803) and blade (804), the motor (802) are arranged in motor cabinet (801)
Top, in the bottom of motor cabinet (801), the blade (804) is arranged in motor (802) for centrifugal energy nozzle (803) setting
Top.
6. a kind of novel plant protection unmanned plane according to claim 5, it is characterised in that: the rear end of the motor cabinet (801)
Equipped with horn interconnecting piece (805), the front end of the motor cabinet (801) is equipped with anticollision rubber (806), the anticollision rubber
(806) fixed strip (807) are equipped with, the anticollision rubber (806) is connect by fixed strip (807) with motor cabinet (801), described
The two sides of horn interconnecting piece (805) are equipped with reinforcing rib (808).
7. a kind of novel plant protection unmanned plane according to claim 5, it is characterised in that: the centrifugal energy nozzle (803) includes
Upper cover (809), yielding rubber (810), centrifugal energy nozzle shell (811), motor fastener (812), centrifugation motor (814) and centrifugation
Turntable (817), the yielding rubber (810) are arranged between upper cover (809) and centrifugal energy nozzle shell (811), and the motor is tight
Firmware (812) setting is equipped with motor housing in the lower section of centrifugal energy nozzle shell (811), the motor fastener (812)
(813), in motor housing (813), the lower part of centrifugation motor (814) is equipped with waterproof for centrifugation motor (814) setting
Rubber (815), it is described centrifugation motor (814) bottom be equipped with centrifugal pan rotating member (818), the centrifugal turntable (817) with from
The bottom of cartridge rotating member (818) connection, the motor fastener (812) is equipped with lower cover (816).
8. a kind of novel plant protection unmanned plane according to claim 1, it is characterised in that: the cross section of the foot prop (12) is
The thickness of V-shaped structure, the foot prop (12) is gradually reduced from top to bottom, the foot prop (12) include front foot frame (1201), after
Foot prop (1202) and connecting plate (1203), the front foot frame (1201) connect with one end of connecting plate (1203), the rear leg
(1202) it is connect with the other end of connecting plate (1203), the junction of the foot prop and connecting plate (1203) is equipped with rubber block
(1204).
9. a kind of novel plant protection unmanned plane according to claim 1, it is characterised in that: the horn (7) is circular hollow
Structure, the horn (7) are Carbon fibe layer and aluminium alloy layer from outside to inside.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811108331.1A CN109110101A (en) | 2018-09-21 | 2018-09-21 | A kind of novel plant protection unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811108331.1A CN109110101A (en) | 2018-09-21 | 2018-09-21 | A kind of novel plant protection unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109110101A true CN109110101A (en) | 2019-01-01 |
Family
ID=64856123
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811108331.1A Pending CN109110101A (en) | 2018-09-21 | 2018-09-21 | A kind of novel plant protection unmanned plane |
Country Status (1)
| Country | Link |
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| CN (1) | CN109110101A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109720559A (en) * | 2019-02-25 | 2019-05-07 | 深圳市翔农创新科技有限公司 | A kind of plant protection drone of novel layouts |
| CN111114744A (en) * | 2020-01-18 | 2020-05-08 | 杭州启飞智能科技有限公司 | Fuselage before unmanned aerial vehicle quick detach and plant protection unmanned aerial vehicle thereof |
| CN113212763A (en) * | 2021-05-21 | 2021-08-06 | 河南易飞农业科技有限公司 | Automatic that detects insect pest spouts medicine plant protection unmanned aerial vehicle voluntarily |
| WO2022067939A1 (en) * | 2020-09-30 | 2022-04-07 | 拓攻（南京）机器人有限公司 | Agricultural unmanned aerial vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109720559A (en) * | 2019-02-25 | 2019-05-07 | 深圳市翔农创新科技有限公司 | A kind of plant protection drone of novel layouts |
| CN111114744A (en) * | 2020-01-18 | 2020-05-08 | 杭州启飞智能科技有限公司 | Fuselage before unmanned aerial vehicle quick detach and plant protection unmanned aerial vehicle thereof |
| WO2022067939A1 (en) * | 2020-09-30 | 2022-04-07 | 拓攻（南京）机器人有限公司 | Agricultural unmanned aerial vehicle |
| CN114514172A (en) * | 2020-12-31 | 2022-05-17 | 深圳市大疆创新科技有限公司 | Unmanned plane |
| CN113212763A (en) * | 2021-05-21 | 2021-08-06 | 河南易飞农业科技有限公司 | Automatic that detects insect pest spouts medicine plant protection unmanned aerial vehicle voluntarily |
| CN113212763B (en) * | 2021-05-21 | 2023-10-13 | 河南易飞农业科技有限公司 | Automatic detect automatic pesticide spraying plant protection unmanned aerial vehicle of insect pest |
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Application publication date: 20190101 |