CN108791886A - A kind of automatic blanking aircraft for fishery - Google Patents
A kind of automatic blanking aircraft for fishery Download PDFInfo
- Publication number
- CN108791886A CN108791886A CN201810523265.8A CN201810523265A CN108791886A CN 108791886 A CN108791886 A CN 108791886A CN 201810523265 A CN201810523265 A CN 201810523265A CN 108791886 A CN108791886 A CN 108791886A
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- CN
- China
- Prior art keywords
- fixedly connected
- aircraft
- hole
- hopper
- automatic blanking
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 239000007787 solid Substances 0.000 claims description 4
- 241000251468 Actinopterygii Species 0.000 abstract description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 15
- 230000005484 gravity Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
Classifications
-
- 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
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01K—ANIMAL HUSBANDRY; AVICULTURE; APICULTURE; PISCICULTURE; FISHING; REARING OR BREEDING ANIMALS, NOT OTHERWISE PROVIDED FOR; NEW BREEDS OF ANIMALS
- A01K61/00—Culture of aquatic animals
- A01K61/80—Feeding devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- 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
- 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
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A40/00—Adaptation technologies in agriculture, forestry, livestock or agroalimentary production
- Y02A40/80—Adaptation technologies in agriculture, forestry, livestock or agroalimentary production in fisheries management
- Y02A40/81—Aquaculture, e.g. of fish
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Environmental Sciences (AREA)
- Remote Sensing (AREA)
- Marine Sciences & Fisheries (AREA)
- Zoology (AREA)
- Animal Husbandry (AREA)
- Biodiversity & Conservation Biology (AREA)
- Mechanical Means For Catching Fish (AREA)
Abstract
The invention discloses a kind of automatic blanking aircraft for fishery, including aircraft, the four corners of the aircraft lower surface have been fixedly connected with connecting rod, the bottom end of the connecting rod is fixedly connected with the upper surface of support plate, and four connecting rods are located at the left and right sides of hopper, the lower surface of the hopper inner wall is fixedly connected with link block.This is used for the automatic blanking aircraft of fishery, by the way that hopper, link block, first through hole, the second through-hole, third through-hole, helical blade, motor, conveying barrel, shaft and discharge nozzle is arranged, so that feed is fallen into conveying barrel, motor is controlled to rotate forward, so that the output shaft of motor drives shaft rotation, so that shaft drives helical blade rotation, so that helical blade drives feed to be moved to the left, so that feed passes sequentially through third through-hole and discharge nozzle falls into the water surface, when the water surface is excessive, fish farther out can normally feed on offshore side, will not seriously affect the growth of fish.
Description
Technical field
The present invention relates to vehicle technology field, specially a kind of automatic blanking aircraft for fishery.
Background technology
Aircraft is the instrument in endoatmosphere or exoatmosphere space flight, and aircraft is divided into 3 classes：Aircraft, space flight
Device, rocket and guided missile.
The cultivation of fishery at present is more and more, and the cultivation of fishery needs to be fed with feed, and traditional feeding patterns are
Feeding apparatus is set on bank, when needing to fish feeding, feeding apparatus spills feed to bank, when the water surface is excessive so that offshore
The fish of side farther out have seriously affected the growth of fish into not food.
Invention content
（One）The technical issues of solution
In view of the deficiencies of the prior art, the present invention provides a kind of automatic blanking aircraft for fishery, solve needs to
When fish feeding, feeding apparatus spills feed to bank, when the water surface is excessive so that the fish of offshore side farther out are into not food, sternly
The problem of affecting the growth of fish again.
（Two）Technical solution
To achieve the above object, the present invention provides the following technical solutions：A kind of automatic blanking aircraft for fishery, including fly
Row device, the four corners of the aircraft lower surface have been fixedly connected with connecting rod, the bottom end of the connecting rod and support plate it is upper
Surface is fixedly connected, and four connecting rods are located at the left and right sides of hopper, and the lower surface of the hopper inner wall is fixedly connected with company
Block is connect, the link block is located between two the second through-holes, and second through-hole is opened in the lower surface of hopper inner wall.
Second through-hole is located at the top of first through hole, and the first through hole is opened in the upper surface of conveying barrel, and two
The upper surface of a conveying barrel is fixedly connected with the lower surface of hopper, and rotating device, the rotating dress are provided in the conveying barrel
The outer surface set is socketed with first bearing and second bearing, and the first bearing and second bearing are respectively engaged with conveying barrel inner wall
Left side and conveying barrel inner wall right side.
The left end of the rotating device is fixedly connected with the output shaft of motor, the lower surface of the motor body and support plate
Upper surface be fixedly connected, the lower surface of the conveying barrel offers third through-hole, the top of the third through-hole and discharge nozzle
It is connected, the discharge nozzle is arranged in the lower surface of support plate.
Preferably, the left side of the connecting rod is fixedly connected with one end of support leg, and the other end of the support leg is solid
Surely it is connected with slide bar, the outer surface of the slide bar is socketed with sliding sleeve, and the sliding sleeve is connected to the upper surface of pressure case, the slide bar
Bottom end is fixedly connected with the upper surface of push plate, and the left and right sides of the push plate have been fixedly connected with sliding block, the sliding block sliding
It is connected in sliding slot, the sliding slot is opened in the left side of pressure chamber interior wall, and the lower surface of the push plate is fixedly connected with that there are two stretch
The bottom end of compression apparatus, the telescopic device is fixedly connected with the lower surface of pressure chamber interior wall, and the lower surface of the pressure case is fixedly connected
There is pressing plate.
Preferably, the rotating device includes shaft, and the shaft is socketed in first bearing and second bearing, described turn
The left end of axis is fixedly connected with the output shaft of motor, and the outer surface of the shaft is fixedly connected with helical blade.
Preferably, the telescopic device includes telescopic rod, and the outer surface of the telescopic rod is socketed with spring, the telescopic rod
It is fixedly connected with the top of spring with the lower surface of push plate, the bottom end and the lower surface of pressure chamber interior wall of the telescopic rod and spring are solid
Fixed connection.
Preferably, the lower surface of the aircraft is fixedly connected with the upper surface of power supply, the lower surface of the power supply with open
The upper surface of pass is fixedly connected.
Preferably, the output end of the power supply is electrically connected with the input terminal of switch, the output end of the switch and motor
Input terminal is electrically connected.
（Three）Advantageous effect
The present invention provides a kind of automatic blanking aircraft for fishery, have following advantageous effect：
1, the automatic blanking aircraft for being used for fishery is logical by the way that hopper, link block, first through hole, the second through-hole, third is arranged
Hole, helical blade, motor, conveying barrel, shaft and discharge nozzle, when needing to fish feeding, feed is poured into material by staff
In case, controls the aircraft and fly above the water surface, the feed in hopper passes sequentially through the second through-hole and first through hole so that feed
It falls into conveying barrel, control motor rotates forward so that the output shaft of motor drives shaft rotation so that shaft drives helical blade rotation
Turn so that helical blade drives feed to be moved to the left so that feed passes sequentially through third through-hole and discharge nozzle falls into the water surface, works as water
When face is excessive, the fish of offshore side farther out can normally feed, and will not seriously affect the growth of fish.
2, automatic blanking aircraft for being used for fishery, by the way that support leg is arranged, sliding sleeve, slide bar, pressure case, push plate, stretches
Bar, spring, sliding block, sliding slot and pressing plate, when the aircraft needs landing so that pressing plate is contacted with ground so that the aircraft
Gravity drive support leg move down so that support leg band moving slide-bar move down so that slide bar drive push plate move down,
So that push plate drives telescopic rod to move down, after the aircraft lands so that tension force of spring drives telescopic rod to move up,
So that telescopic rod drives push plate to move up so that push plate drives support leg to move up so that telescopic rod and spring play
Cushioning effect, internal structure of aircraft will not be ensure that making for the aircraft by larger damage when the aircraft being allowed to decline
Use the service life.
3, automatic blanking aircraft for being used for fishery, by the way that link block, discharge nozzle, third through-hole and helical-blade is arranged
Piece, when staff pours into feed in hopper, due to the left and right sides of hopper inner wall and the left and right sides of link block
It is respectively set to inclined surface so that feed in hopper is significantly more efficient by the second through-hole and first through hole, and knot of the present invention
Structure is compact, reasonable design, highly practical.
Description of the drawings
Fig. 1 is the cross-sectional view that the present invention faces；
Fig. 2 is the structural schematic diagram that the present invention overlooks；
Fig. 3 is the structural schematic diagram amplified at A of the present invention.
In figure：1 support leg, 2 first bearings, 3 conveying barrels, 4 connecting rods, 5 hoppers, 6 first through hole, 7 second through-holes, 8 connect
Connect block, 9 power supplys, 10 switches, 11 aircraft, 12 push plates, 13 slide bars, 14 sliding sleeves, 15 pressure casees, 16 fixed links, 17 second bearings, 18
Rotating device, 181 helical blades, 182 shafts, 19 third through-holes, 20 discharge nozzles, 21 motors, 22 support plates, 23 pressing plates, 24 are stretched
Compression apparatus, 241 springs, 242 telescopic rods, 25 sliding blocks, 26 sliding slots.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
As shown in Figs. 1-3, the present invention provides a kind of technical solution：A kind of automatic blanking aircraft for fishery, including
The lower surface of aircraft 11, aircraft 11 is fixedly connected with the upper surface of power supply 9, passes through and power supply 9 is arranged so that power supply 9 can be with
It powers to motor 21 so that motor 21 can work normally, and the lower surface of power supply 9 is fixedly connected with the upper surface of switch 10, lead to
Setting switch 10 is crossed, so that the work of control motor 21 that staff is more convenient, output end and the switch 10 of power supply 9
Input terminal is electrically connected, and the output end of switch 10 is electrically connected with the input terminal of motor 21, and the four corners of 11 lower surface of aircraft are solid
Surely it is connected with connecting rod 4, the bottom end of connecting rod 4 is fixedly connected with the upper surface of support plate 22, and four connecting rods 4 are located at hopper
The lower surface of 5 left and right sides, 5 inner wall of hopper is fixedly connected with link block 8, one end of the left side and support leg 1 of connecting rod 4
It is fixedly connected, the other end of support leg 1 is fixedly connected with slide bar 13, and the outer surface of slide bar 13 is socketed with sliding sleeve 14, and sliding sleeve 14 blocks
It is connected on the upper surface of pressure case 15, the bottom end of slide bar 13 is fixedly connected with the upper surface of push plate 12, and the left and right sides of push plate 12 are equal
It is fixedly connected with sliding block 25, sliding block 25 is slidably connected in sliding slot 26, and sliding slot 26 is opened in the left side of pressure 15 inner wall of case, push plate
12 lower surface is fixedly connected there are two telescopic device 24, and the bottom end of telescopic device 24 and the lower surface of pressure 15 inner wall of case are fixed and connected
It connects, the lower surface of pressure case 15 is fixedly connected with pressing plate 23, by the way that telescopic rod 242, spring 241 and pressing plate 23 is arranged, when the flight
After device landing so that the tension of spring 241 drives telescopic rod 242 to move up so that telescopic rod 242 drives push plate 12 to moving up
It is dynamic so that push plate 12 drives support leg 1 to move up so that telescopic rod 242 and spring 241 play cushioning effect, this is allowed to fly
Internal structure of aircraft will not be ensure that the service life of the aircraft, telescopic device by larger damage when row device declines
24 include telescopic rod 242, and the outer surface of telescopic rod 242 is socketed with spring 241, the top and push plate of telescopic rod 242 and spring 241
12 lower surface is fixedly connected, and the bottom end of telescopic rod 242 and spring 241 is fixedly connected with the lower surface of pressure 15 inner wall of case, is connected
Block 8 is located between two the second through-holes 7, and the second through-hole 7 is opened in the lower surface of 5 inner wall of hopper.
Second through-hole 7 is located at the top of first through hole 6, and first through hole 6 is opened in the upper surface of conveying barrel 3, passes through setting
First through hole 6 and the second through-hole 7 so that the feed in hopper 5 passes sequentially through the second through-hole 7 and first through hole 6 so that feed is fallen
Enter more convenient in conveying barrel 3, and the upper surface of two conveying barrels 3 is fixedly connected with the lower surface of hopper 5, is set in conveying barrel 3
It is equipped with rotating device 18, rotating device 18 includes shaft 182, and shaft 182 is socketed in first bearing 2 and second bearing 17, is turned
The left end of axis 182 is fixedly connected with the output shaft of motor 21, and the outer surface of shaft 182 is fixedly connected with helical blade 181, passes through
First bearing 2 and second bearing 17 are set, and motor 21 rotates forward so that the output shaft of motor 21 drives shaft 182 to rotate so that turns
It will not be shaken when the drive rotation of helical blade 181 of axis 182 and more laborsaving, the outer surface of rotating device 18 is socketed with first bearing
2 and second bearing 17, first bearing 2 and second bearing 17 are respectively engaged with 3 inner wall of left side and conveying barrel of 3 inner wall of conveying barrel
Right side.
The left end of rotating device 18 is fixedly connected with the output shaft of motor 21, lower surface and the support plate 22 of 21 fuselage of motor
Upper surface be fixedly connected, the lower surface of conveying barrel 3 offers third through-hole 19, the top phase of third through-hole 19 and discharge nozzle 20
Connection, by the way that helical blade 181 is arranged so that shaft 182 drives helical blade 181 to rotate so that helical blade 181, which drives, raises
Material is moved to the left so that feed passes sequentially through third through-hole 19 and discharge nozzle 20 falls into the water surface, when the water surface is excessive, offshore side compared with
Remote fish can normally feed, and discharge nozzle 20 is arranged in the lower surface of support plate 22.
In use, when needing to fish feeding, staff pours into feed in hopper 5, controls the aircraft 11 and flies
Above the water surface, the feed in hopper 5 passes sequentially through the second through-hole 7 and first through hole 6 so that feed is fallen into conveying barrel 3, control
Motor 21 processed rotates forward so that the output shaft of motor 21 drives shaft 182 to rotate so that shaft 182 drives helical blade 181 to revolve
Turn so that helical blade 181 drives feed to be moved to the left so that feed passes sequentially through third through-hole 19 and discharge nozzle 20 falls into water
Face, when the water surface is excessive, the fish of offshore side farther out can normally feed, when the aircraft 11 needs landing so that pressing plate
23 contact with ground so that the gravity of the aircraft 11 drives support leg 1 to move down so that support leg 1 with moving slide-bar 13 to
Lower movement so that slide bar 13 drives push plate 12 to move down so that push plate 12 drives telescopic rod 242 to move down, when the flight
After device 11 lands so that the tension of spring 241 drives telescopic rod 242 to move up so that telescopic rod 242 drives push plate 12 upward
It is mobile so that push plate 12 drives support leg 1 to move up so that telescopic rod 242 and spring 241 play cushioning effect, allow this
11 internal structure of aircraft will not be by larger damage when aircraft 11 declines.
Can to sum up obtain, 1, this be used for the automatic blanking aircraft of fishery, pass through and hopper 5, link block 8, first through hole be set
6, the second through-hole 7, third through-hole 19, helical blade 181, motor 21, conveying barrel 3, shaft 182 and discharge nozzle 20, when needs are given
When fish feeding, staff pours into feed in hopper 5, controls the aircraft 11 and flies above the water surface, the feed in hopper 5
Pass sequentially through the second through-hole 7 and first through hole 6 so that feed is fallen into conveying barrel 3, and control motor 21 rotates forward so that motor 21
Output shaft drive shaft 182 rotate so that shaft 182 drive helical blade 181 rotate so that helical blade 181 drive raise
Material is moved to the left so that feed passes sequentially through third through-hole 19 and discharge nozzle 20 falls into the water surface, when the water surface is excessive, offshore side compared with
Remote fish can normally feed, and will not seriously affect the growth of fish.
2, automatic blanking aircraft for being used for fishery, by the way that support leg 1 is arranged, sliding sleeve 14, slide bar 13, pressure case 15, pushes away
Plate 12, telescopic rod 242, spring 241, sliding block 25, sliding slot 26 and pressing plate 23, when the aircraft 11 needs landing so that pressing plate
23 contact with ground so that the gravity of the aircraft 11 drives support leg 1 to move down so that support leg 1 with moving slide-bar 13 to
Lower movement so that slide bar 13 drives push plate 12 to move down so that push plate 12 drives telescopic rod 242 to move down, when the flight
After device 11 lands so that the tension of spring 241 drives telescopic rod 242 to move up so that telescopic rod 242 drives push plate 12 upward
It is mobile so that push plate 12 drives support leg 1 to move up so that telescopic rod 242 and spring 241 play cushioning effect, allow this
Internal structure of aircraft will not be ensure that the service life of the aircraft 11 by larger damage when aircraft 11 declines.
3, automatic blanking aircraft for being used for fishery, by the way that link block 8, discharge nozzle 20, third through-hole 19 and spiral shell is arranged
Vane piece 181, when staff pours into feed in hopper 5, due to the left and right sides and link block 8 of hopper 5 inner wall
Left and right sides are respectively set to inclined surface so that feed in hopper 5 is significantly more efficient to pass through the second through-hole 7 and first through hole
6, and structure of the invention is compact, reasonable design, it is highly practical.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
Claims (6)
1. a kind of automatic blanking aircraft for fishery, including aircraft（11）, it is characterised in that：The aircraft（11）Under
The four corners on surface have been fixedly connected with connecting rod（4）, the connecting rod（4）Bottom end and support plate（22）Upper surface fix
Connection, and four connecting rods（4）Positioned at hopper（5）The left and right sides, the hopper（5）The lower surface of inner wall is fixedly connected with company
Connect block（8）, the link block（8）Positioned at two the second through-holes（7）Between, second through-hole（7）It is opened in hopper（5）Inner wall
Lower surface；
Second through-hole（7）Positioned at first through hole（6）Top, the first through hole（6）It is opened in conveying barrel（3）Upper table
Face, and two conveying barrels（3）Upper surface and hopper（5）Lower surface be fixedly connected, the conveying barrel（3）Inside it is provided with rotation
Device（18）, the rotating device（18）Outer surface be socketed with first bearing（2）And second bearing（17）, the first bearing
（2）And second bearing（17）It is respectively engaged with conveying barrel（3）The left side of inner wall and conveying barrel（3）The right side of inner wall；
The rotating device（18）Left end and motor（21）Output shaft be fixedly connected, the motor（21）The lower surface of fuselage
With support plate（22）Upper surface be fixedly connected, the conveying barrel（3）Lower surface offer third through-hole（19）, the third
Through-hole（19）With discharge nozzle（20）Top be connected, the discharge nozzle（20）It is arranged in support plate（22）Lower surface.
2. a kind of automatic blanking aircraft for fishery according to claim 1, it is characterised in that：The connecting rod
（4）Left side and support leg（1）One end be fixedly connected, the support leg（1）The other end be fixedly connected with slide bar（13）,
The slide bar（13）Outer surface be socketed with sliding sleeve（14）, the sliding sleeve（14）It is connected to pressure case（15）Upper surface, the cunning
Bar（13）Bottom end and push plate（12）Upper surface be fixedly connected, the push plate（12）Left and right sides be fixedly connected with cunning
Block（25）, the sliding block（25）It is slidably connected at sliding slot（26）It is interior, the sliding slot（26）It is opened in pressure case（15）The left side of inner wall
Face, the push plate（12）Lower surface be fixedly connected there are two telescopic device（24）, the telescopic device（24）Bottom end and pressure
Case（15）The lower surface of inner wall is fixedly connected, the pressure case（15）Lower surface be fixedly connected with pressing plate（23）.
3. a kind of automatic blanking aircraft for fishery according to claim 2, it is characterised in that：The rotating device
（18）Including shaft（182）, the shaft（182）It is socketed in first bearing（2）And second bearing（17）It is interior, the shaft
（182）Left end and motor（21）Output shaft be fixedly connected, the shaft（182）Outer surface be fixedly connected with helical blade
（181）.
4. a kind of automatic blanking aircraft for fishery according to claim 3, it is characterised in that：The telescopic device
（24）Including telescopic rod（242）, the telescopic rod（242）Outer surface be socketed with spring（241）, the telescopic rod（242）With
Spring（241）Top and push plate（12）Lower surface be fixedly connected, the telescopic rod（242）And spring（241）Bottom end with
Press case（15）The lower surface of inner wall is fixedly connected.
5. a kind of automatic blanking aircraft for fishery according to claim 4, it is characterised in that：The aircraft
（11）Lower surface and power supply（9）Upper surface be fixedly connected, the power supply（9）Lower surface and switch（10）Upper surface it is solid
Fixed connection.
6. a kind of automatic blanking aircraft for fishery according to claim 5, it is characterised in that：The power supply（9）
Output end and switch（10）Input terminal electrical connection, the switch（10）Output end and motor（21）Input terminal be electrically connected
It connects.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810523265.8A CN108791886A (en) | 2018-05-28 | 2018-05-28 | A kind of automatic blanking aircraft for fishery |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810523265.8A CN108791886A (en) | 2018-05-28 | 2018-05-28 | A kind of automatic blanking aircraft for fishery |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108791886A true CN108791886A (en) | 2018-11-13 |
Family
ID=64090512
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810523265.8A Withdrawn CN108791886A (en) | 2018-05-28 | 2018-05-28 | A kind of automatic blanking aircraft for fishery |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108791886A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109644919A (en) * | 2019-01-31 | 2019-04-19 | 临沂大学 | A kind of solid granulates scattering mechanism and method |
| CN115500303A (en) * | 2022-11-21 | 2022-12-23 | 射阳县射阳港对虾养殖二公司 | Throwing type throwing device for freshwater fish culture |
-
2018
- 2018-05-28 CN CN201810523265.8A patent/CN108791886A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109644919A (en) * | 2019-01-31 | 2019-04-19 | 临沂大学 | A kind of solid granulates scattering mechanism and method |
| CN115500303A (en) * | 2022-11-21 | 2022-12-23 | 射阳县射阳港对虾养殖二公司 | Throwing type throwing device for freshwater fish culture |
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