CN108248878A - A kind of unmanned plane Master Control Center device mechanically automatically controlled - Google Patents
A kind of unmanned plane Master Control Center device mechanically automatically controlled Download PDFInfo
- Publication number
- CN108248878A CN108248878A CN201810057663.5A CN201810057663A CN108248878A CN 108248878 A CN108248878 A CN 108248878A CN 201810057663 A CN201810057663 A CN 201810057663A CN 108248878 A CN108248878 A CN 108248878A
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- China
- Prior art keywords
- fixedly connected
- wall
- protective casing
- control center
- unmanned plane
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- 238000013016 damping Methods 0.000 claims abstract description 46
- 230000001681 protective effect Effects 0.000 claims abstract description 45
- 239000004065 semiconductor Substances 0.000 claims abstract description 21
- 238000012545 processing Methods 0.000 claims abstract description 19
- 230000017525 heat dissipation Effects 0.000 claims abstract description 12
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 claims abstract description 7
- 239000007788 liquid Substances 0.000 claims description 10
- 238000003860 storage Methods 0.000 claims description 10
- 238000001035 drying Methods 0.000 claims description 7
- 230000006835 compression Effects 0.000 claims description 6
- 238000007906 compression Methods 0.000 claims description 6
- 239000010720 hydraulic oil Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 14
- 238000010438 heat treatment Methods 0.000 abstract description 3
- 238000009434 installation Methods 0.000 description 6
- 238000012423 maintenance Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000003139 buffering effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000005057 refrigeration Methods 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
- B64D47/00—Equipment not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Mechanical Engineering (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The invention discloses a kind of Master Control Center devices driven for unmanned plane, including protective casing, the screw top of the protective casing is connected with protective cover, the inner bottom wall of protective casing is fixedly connected with radiator fan, the inner bottom wall of protective casing is fixedly connected with damping tube, the inner bottom wall of damping tube is fixedly connected with damping spring, decoupling rod is fixedly connected at the top of damping spring, the top of decoupling rod is run through and extends to the upper surface of damping tube, vibration damper plate is fixedly connected at the top of decoupling rod, the upper surface of vibration damper plate is provided with central processing unit.This is used for the Master Control Center device that unmanned plane drives, achieve the effect that mechanically to automatically control radiator fan and semiconductor chilling plate, when the temperature rise in protective casing, alcohol expanded by heating, the lower contact for jacking up lower skateboard upper surface is electrically connected with upper contact, and then radiator fan and semiconductor chilling plate is controlled to start heat dissipation, so as to effectively solve the problems, such as that unmanned aerial vehicle (UAV) control center increases load.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specially a kind of unmanned plane Master Control Center dress mechanically automatically controlled
It puts.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft or fully or intermittently independently operated by car-mounted computer.
Compared with manned aircraft, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Nobody
Machine press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane
Sector application, be that unmanned plane has really just needed；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster are rescued
It helps, observe wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc.
The purposes of unmanned plane in itself has greatly been expanded in the application in field, and developed country is also in actively extension sector application and development nothing
Man-machine technology.
The field of unmanned plane application at present is more and more extensive, and the requirement controlled it is also higher and higher, now most of
Unmanned plane Nei Douyou control centres, and control centre can shake with the vibrations of unmanned plane, and its heat for generating also all by
Control centre is individually controlled, this is easy to the calculated load for increasing control centre, so needing a kind of mechanical automatic control
The unmanned plane Master Control Center device of system.
Invention content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the present invention provides a kind of unmanned plane Master Control Center dresses mechanically automatically controlled
It puts, solves the problems, such as unmanned aerial vehicle (UAV) control center easily vibrations and increase load.
(2) technical solution
In order to achieve the above object, the present invention is achieved by the following technical programs：A kind of nothing mechanically automatically controlled
Man-machine Master Control Center device, including protective casing, the screw top of the protective casing is connected with protective cover, the protective casing
Inner bottom wall be fixedly connected with radiator fan, the inner bottom wall of the protective casing is fixedly connected with damping tube, the damping tube
Inner bottom wall is fixedly connected with damping spring, and decoupling rod, the top of the decoupling rod are fixedly connected at the top of the damping spring
Run through and extend to the upper surface of damping tube, vibration damper plate, the upper table of the vibration damper plate are fixedly connected at the top of the decoupling rod
Face is provided with central processing unit, and the bottom end side of the central processing unit is fixedly connected with link block, the upper table of the link block
Middle face offers jack, and the upper surface both ends of the vibration damper plate have been fixedly connected with inserting column, the surface of the inserting column and jack
Inner wall grafting, the upper surface of link block is extended at the top of the inserting column, the top interior of the inserting column offers telescopic hole,
The inner wall of the telescopic hole slidably connects snap-gauge, and the surface of the snap-gauge and the inner wall of telescopic hole are slidably connected, the snap-gauge
End surface be fixedly connected with compression spring, one end of the snap-gauge extends to the outside of telescopic hole, the following table of the snap-gauge
The upper surface slide connection of the link block of face and inserting column.
The outer surface of the protective casing is fixedly connected with refrigerator pipes, and the inner bottom wall of the refrigerator pipes offers air admission hole,
The inner wall of the refrigerator pipes is fixedly connected with semiconductor chilling plate, and the radiating end of the semiconductor chilling plate runs through and extends to system
The outer surface of cold pipe, the inner wall of the protective casing offer gas port, and one end of the gas port extends to the interior of refrigerator pipes
Portion, the other end of the gas port extend to the inner bottom wall of protective casing.
The inner wall of the protective casing has been respectively fixedly connected with liquid storage pipe and telescoping tube, the inner bottom wall of the telescoping tube and storage
The inner roof wall of liquid pipe, which is fixed, to be connected, and the inside of the liquid storage pipe and telescoping tube is both provided with alcohol, the inner wall point of the telescoping tube
Upper slide and lower skateboard are not slidably connected, and the lower surface of the upper slide and the upper surface of lower skateboard have been respectively fixedly connected with down
Contact and upper contact, the lower contact and upper contact electrical connection, the upper contact respectively with radiator fan and semiconductor chilling plate
Electrical connection.
Preferably, the inner bottom wall of the protective casing offers oil-through-hole, the both ends of the oil-through-hole with damping tube
Inner bottom wall connects, and the inside of the damping tube and oil-through-hole is both provided with hydraulic oil.
Preferably, another end surfaces triangular shape of the snap-gauge, the quantity of the snap-gauge is two.
Preferably, the inner roof wall of the protective cover offers heat dissipation outlet, and the inner wall of the heat dissipation outlet is provided with protection
Net.
Preferably, the inner wall of the air admission hole is fixedly connected with filter screen, and the other end inner wall of the gas port, which is fixed, to be connected
Drying layer is connected to, the drying layer is internally provided with drier.
Preferably, the upper surface of the inner wall of the telescoping tube, upper slide and lower skateboard offers threading hole, the threading
The one end in hole extends respectively to the inside of upper contact and lower contact.
Preferably, the upper surface of the upper slide is fixedly connected with tension spring, and the top of the tension spring is with stretching
The inner roof wall of pipe is fixedly connected.
(3) advantageous effect
The present invention provides a kind of unmanned plane Master Control Center devices mechanically automatically controlled, have following advantageous effect：
(1), the unmanned plane Master Control Center device mechanically automatically controlled is fixed by the inner bottom wall for setting damping tube and connected
Damping spring is connected to, decoupling rod is fixedly connected at the top of damping spring, the top of decoupling rod is run through and extends to damping tube
Upper surface is fixedly connected with vibration damper plate at the top of decoupling rod, and the upper surface of vibration damper plate is provided with central processing unit, has reached centering
Central processor carries out the effect of damping, and when protective casing shakes, central processing unit passes through decoupling rod bottom on vibration damper plate
The damping spring at end carries out bumper and absorbing shock, so as to effectively solve the problems, such as that unmanned aerial vehicle (UAV) control center is easily shaken.
(2), unmanned plane Master Control Center device mechanically automatically controlled, by the lower surface and the downslide that set upper slide
The upper surface of plate has been respectively fixedly connected with lower contact and upper contact, lower contact and upper contact electrical connection, upper contact respectively with heat dissipation
Fan and semiconductor chilling plate electrical connection, have reached the effect mechanically automatically controlled to radiator fan and semiconductor chilling plate
Fruit, when the temperature rise in protective casing, alcohol expanded by heating, the lower contact for jacking up lower skateboard upper surface is electrically connected with upper contact
It connects, and then radiator fan and semiconductor chilling plate is controlled to start heat dissipation, so as to effectively solve the increase of unmanned aerial vehicle (UAV) control center
The problem of load.
(3), the unmanned plane Master Control Center device mechanically automatically controlled, by the surface and the telescopic hole that set snap-gauge
Inner wall is slidably connected, and the end surface of snap-gauge is fixedly connected with compression spring, and one end of snap-gauge extends to the outside of telescopic hole, card
The upper surface slide of the lower surface of plate and the link block of inserting column connects, and can effectively enhance the installation speed and dimension of central processing unit
Easy-to-dismount effect when repairing, jack and inserting column grafting on link block, snap-gauge is to bouncing back at inserting column center, when jack slides to card
During plate lower surface, snap-gauge is skidded off to be connect, and then be easy for installation and maintenance with the upper surface slide of link block.
Description of the drawings
Fig. 1 is schematic structural view of the invention；
Fig. 2 is enlarged drawing at A in Fig. 1 of the present invention；
Fig. 3 is flexible pipe structure sectional view of the present invention.
In figure：1 protective casing, 2 protective covers, 3 radiator fans, 4 damping tubes, 5 damping springs, 6 decoupling rods, 7 vibration damper plates, 8
Central processing unit, 9 link blocks, 10 jacks, 11 inserting columns, 12 telescopic holes, 13 snap-gauges, 14 compression springs, 15 refrigerator pipes, 16 air inlets
Hole, 17 semiconductor chilling plates, 18 gas ports, 19 liquid storage pipes, 20 telescoping tubes, 21 upper slides, 22 lower skateboards, 23 lower contacts, on 24
Contact, 25 oil-through-holes, 26 heat dissipation outlets, 27 protection networks, 28 filter screens, 29 drying layers, 30 threading holes, 31 tension springs.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other without making creative work
Embodiment shall fall within the protection scope of the present invention.
- 2 are please referred to Fig.1, the present invention provides a kind of technical solution：A kind of unmanned plane Master Control Center mechanically automatically controlled
Device, including protective casing 1, the screw top of protective casing 1 is connected with protective cover 2, and the inner roof wall of protective cover 2 offers heat dissipation
Outlet 26, the inner wall of heat dissipation outlet 26 are provided with protection network 27, and the inner bottom wall of protective casing 1 is fixedly connected with radiator fan 3, prevents
The inner bottom wall of protective case body 1 is fixedly connected with damping tube 4, and the inner bottom wall of protective casing 1 offers oil-through-hole 25, and the two of oil-through-hole 25
The inner bottom wall with damping tube 4 is held to connect, damping tube 4 and the inside of oil-through-hole 25 are both provided with hydraulic oil, can be effectively right
4 top of damping tube carries out damping, buffering, and the inner bottom wall of damping tube 4 is fixedly connected with damping spring 5, and the top of damping spring 5 is consolidated
Surely decoupling rod 6 is connected with, the top of decoupling rod 6 is run through and extends to the upper surface of damping tube 4, and the top of decoupling rod 6, which is fixed, to be connected
Vibration damper plate 7 is connected to, the upper surface of vibration damper plate 7 is provided with central processing unit 8, is fixedly connected by the inner bottom wall for setting damping tube 4
There is damping spring 5, the top of damping spring 5 is fixedly connected with decoupling rod 6, and the top of decoupling rod 6 is run through and extends to damping tube 4
Upper surface, the top of decoupling rod 6 is fixedly connected with vibration damper plate 7, and the upper surface of vibration damper plate 7 is provided with central processing unit 8, reaches
The effect of damping is carried out to central processing unit 8, when protective casing 1 shakes, central processing unit 8 is logical on vibration damper plate 7
The damping spring 5 for crossing 6 bottom end of decoupling rod carries out bumper and absorbing shock, so as to effectively solve what unmanned aerial vehicle (UAV) control center was easily shaken
Problem, the bottom end side of central processing unit 8 are fixedly connected with link block 9, and the upper surface middle part of link block 9 offers jack 10,
The upper surface both ends of vibration damper plate 7 have been fixedly connected with inserting column 11, the surface of inserting column 11 and the inner wall grafting of jack 10, inserting column 11
Top extends to the upper surface of link block 9, and the top interior of inserting column 11 offers telescopic hole 12, and the inner wall of telescopic hole 12, which slides, to be connected
Snap-gauge 13 is connected to, the surface of snap-gauge 13 and the inner wall of telescopic hole 12 are slidably connected, and the end surface of snap-gauge 13 is fixedly connected with pressure
Power spring 14, one end of snap-gauge 13 extend to the outside of telescopic hole 12, another end surfaces triangular shape of snap-gauge 13, snap-gauge 13
Quantity for two, the lower surface of snap-gauge 13 is connect with the upper surface slide of the link block 9 of inserting column 11, by setting snap-gauge 13
Surface and the inner wall of telescopic hole 12 are slidably connected, and the end surface of snap-gauge 13 is fixedly connected with compression spring 14, and the one of snap-gauge 13
End extends to the outside of telescopic hole 12, and the lower surface of snap-gauge 13 is connect with the upper surface slide of the link block 9 of inserting column 11, Neng Gouyou
The installation speed and easy-to-dismount effect during repair of effect enhancing central processing unit 8, the jack 10 on link block 9 are inserted with inserting column 11
It connects, snap-gauge 13 is to retraction at 11 center of inserting column, and when jack 10 slides to 13 lower surface of snap-gauge, snap-gauge 13 skids off and link block 9
Upper surface slide connects, and then is easy for installation and maintenance.
The outer surface of protective casing 1 is fixedly connected with refrigerator pipes 15, and the inner bottom wall of refrigerator pipes 15 offers air admission hole 16, system
The inner wall of cold pipe 15 is fixedly connected with semiconductor chilling plate 17, and the radiating end of semiconductor chilling plate 17 runs through and extends to refrigerator pipes
15 outer surface, the inner wall of protective casing 1 offer gas port 18, and one end of gas port 18 extends to the inside of refrigerator pipes 15,
The other end of gas port 18 extends to the inner bottom wall of protective casing 1, and the inner wall of air admission hole 16 is fixedly connected with filter screen 28, air guide
The other end inner wall in hole 18 is fixedly connected with drying layer 29, and drying layer 29 is internally provided with drier, can reach to refrigeration
The effect of removing is dried in the air quenched rear moisture generated in pipe 2.
The inner wall of protective casing 1 has been respectively fixedly connected with liquid storage pipe 19 and telescoping tube 20, the inner bottom wall of telescoping tube 20 and storage
The inner roof wall of liquid pipe 19, which is fixed, to be connected, and the inside of liquid storage pipe 19 and telescoping tube 20 is both provided with alcohol, the inner wall point of telescoping tube 20
Upper slide 21 and lower skateboard 22 are not slidably connected, and the lower surface of upper slide 21 and the upper surface of lower skateboard 22 are respectively fixedly connected with
Have lower contact 23 and upper contact 24, lower contact 23 and upper contact 24 are electrically connected, upper contact 24 respectively with radiator fan 3 and semiconductor
Cooling piece 17 is electrically connected, and the upper surface of the inner wall of telescoping tube 20, upper slide 21 and lower skateboard 22 offers threading hole 30, is threaded
The one end in hole 30 extends respectively to the inside of upper contact 24 and lower contact 23, and the upper surface of upper slide 21 is fixedly connected with pulling force bullet
Spring 31, the top of tension spring 31 are fixedly connected with the inner roof wall of telescoping tube 20, by setting the lower surface of upper slide 21 under
The upper surface of slide plate 22 has been respectively fixedly connected with lower contact 23 and upper contact 24, and lower contact 23 and upper contact 24 are electrically connected, upper to touch
Point 24 is electrically connected with radiator fan 3 and semiconductor chilling plate 17 respectively, reached to radiator fan 3 and semiconductor chilling plate 17 into
The effect that row mechanically automatically controls, when the temperature rise in protective casing 1, alcohol expanded by heating is jacked up on lower skateboard 22
The lower contact 23 on surface is electrically connected with upper contact 24, and then radiator fan 3 and semiconductor chilling plate 17 is controlled to start heat dissipation, so as to
It is effective to solve the problems, such as that unmanned aerial vehicle (UAV) control center increases load.
In conclusion the unmanned plane Master Control Center device mechanically automatically controlled, by set the surface of snap-gauge 13 with
The inner wall of telescopic hole 12 is slidably connected, and the end surface of snap-gauge 13 is fixedly connected with compression spring 14, one end extension of snap-gauge 13
To the outside of telescopic hole 12, the lower surface of snap-gauge 13 is connect with the upper surface slide of the link block 9 of inserting column 11, can effectively be enhanced
Easy-to-dismount effect when the installation speed of central processing unit 8 and repair, jack 10 and 11 grafting of inserting column on link block 9, card
Plate 13 is to retraction at 11 center of inserting column, and when jack 10 slides to 13 lower surface of snap-gauge, snap-gauge 13 skids off the upper surface with link block 9
It is slidably connected, and then is easy for installation and maintenance, damping spring 5, damping bullet are fixedly connected with by the inner bottom wall for setting damping tube 4
The top of spring 5 is fixedly connected with decoupling rod 6, and the top of decoupling rod 6 is run through and extends to the upper surface of damping tube 4, decoupling rod 6
Top is fixedly connected with vibration damper plate 7, and the upper surface of vibration damper plate 7 is provided with central processing unit 8, reached to central processing unit 8 into
The effect of row damping, when protective casing 1 shakes, the subtracting by 6 bottom end of decoupling rod on vibration damper plate 7 of central processing unit 8
It shakes spring 5 and carries out bumper and absorbing shock, so as to effectively solve the problems, such as that unmanned aerial vehicle (UAV) control center is easily shaken, by sliding in setting
The lower surface of plate 21 and the upper surface of lower skateboard 22 have been respectively fixedly connected with lower contact 23 and upper contact 24, lower contact 23 and upper touch
24 electrical connection of point, upper contact 24 are electrically connected with radiator fan 3 and semiconductor chilling plate 17, have reached to 3 He of radiator fan respectively
The effect that semiconductor chilling plate 17 is mechanically automatically controlled, when the temperature rise in protective casing 1, alcohol is heated swollen
Swollen, the lower contact 23 for jacking up 22 upper surface of lower skateboard is electrically connected with upper contact 24, and then controls radiator fan 3 and semiconductor refrigerating
Piece 17 starts heat dissipation, so as to effectively solve the problems, such as that unmanned aerial vehicle (UAV) control center increases load.
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 (7)
1. a kind of Master Control Center device driven for unmanned plane, including protective casing (1), the top of the protective casing (1)
Protective cover (2) is threaded with, the inner bottom wall of the protective casing (1) is fixedly connected with radiator fan (3), it is characterised in that：
The inner bottom wall of the protective casing (1) is fixedly connected with damping tube (4), and the inner bottom wall of the damping tube (4), which is fixedly connected with, to be subtracted
Spring (5) is shaken, decoupling rod (6) is fixedly connected at the top of the damping spring (5), the top of the decoupling rod (6) is through simultaneously
The upper surface of damping tube (4) is extended to, vibration damper plate (7), the vibration damper plate (7) are fixedly connected at the top of the decoupling rod (6)
Upper surface be provided with central processing unit (8), the bottom end side of the central processing unit (8) is fixedly connected with link block (9), institute
The upper surface middle part for stating link block (9) offers jack (10), and the upper surface both ends of the vibration damper plate (7) have been fixedly connected with slotting
Column (11), the surface of the inserting column (11) and the inner wall grafting of jack (10) extend to link block at the top of the inserting column (11)
(9) upper surface, the top interior of the inserting column (11) offer telescopic hole (12), and the inner wall of the telescopic hole (12), which slides, to be connected
Snap-gauge (13) is connected to, the surface of the snap-gauge (13) and the inner wall of telescopic hole (12) are slidably connected, one end of the snap-gauge (13)
Surface is fixedly connected with compression spring (14), and one end of the snap-gauge (13) extends to the outside of telescopic hole (12), the snap-gauge
(13) lower surface is connect with the upper surface slide of the link block (9) of inserting column (11)；
The outer surface of the protective casing (1) is fixedly connected with refrigerator pipes (15), and the inner bottom wall of the refrigerator pipes (15) offers
Air admission hole (16), the inner wall of the refrigerator pipes (15) are fixedly connected with semiconductor chilling plate (17), the semiconductor chilling plate
(17) radiating end runs through and extends to the outer surface of refrigerator pipes (15), and the inner wall of the protective casing (1) offers gas port
(18), one end of the gas port (18) extends to the inside of refrigerator pipes (15), and the other end of the gas port (18) extends to
The inner bottom wall of protective casing (1)；
The inner wall of the protective casing (1) has been respectively fixedly connected with liquid storage pipe (19) and telescoping tube (20), the telescoping tube (20)
The fixation of inner bottom wall and the inner roof wall of liquid storage pipe (19) connect, the inside of the liquid storage pipe (19) and telescoping tube (20) is both provided with
Alcohol, the inner wall of the telescoping tube (20) slidably connect upper slide (21) and lower skateboard (22), the upper slide (21) respectively
Lower surface and the upper surface of lower skateboard (22) be respectively fixedly connected with lower contact (23) and upper contact (24), the lower contact
(23) it is electrically connected respectively with radiator fan (3) and semiconductor chilling plate (17) with upper contact (24) electrical connection, the upper contact (24)
It connects.
2. a kind of Master Control Center device driven for unmanned plane according to claim 1, it is characterised in that：The protection
The inner bottom wall of housing (1) offers oil-through-hole (25), and the both ends of the oil-through-hole (25) connect with the inner bottom wall of damping tube (4)
Logical, the damping tube (4) and the inside of oil-through-hole (25) are both provided with hydraulic oil.
3. a kind of Master Control Center device driven for unmanned plane according to claim 1, it is characterised in that：The snap-gauge
(13) another end surfaces triangular shape, the quantity of the snap-gauge (13) is two.
4. a kind of Master Control Center device driven for unmanned plane according to claim 1, it is characterised in that：The protection
The inner roof wall of lid (2) offers heat dissipation outlet (26), and the inner wall of the heat dissipation outlet (26) is provided with protection network (27).
5. a kind of Master Control Center device driven for unmanned plane according to claim 1, it is characterised in that：The air inlet
The inner wall in hole (16) is fixedly connected with filter screen (28), and the other end inner wall of the gas port (18) is fixedly connected with drying layer
(29), the drying layer (29) is internally provided with drier.
6. a kind of Master Control Center device driven for unmanned plane according to claim 1, it is characterised in that：It is described flexible
The upper surface for managing the inner wall of (20), upper slide (21) and lower skateboard (22) offers threading hole (30), the threading hole (30)
One end extend respectively to the inside of upper contact (24) and lower contact (23).
7. a kind of Master Control Center device driven for unmanned plane according to claim 1, it is characterised in that：The upper cunning
The upper surface of plate (21) is fixedly connected with tension spring (31), the top of the tension spring (31) and the interior top of telescoping tube (20)
Wall is fixedly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810057663.5A CN108248878B (en) | 2018-01-22 | 2018-01-22 | Mechanical automatic control unmanned aerial vehicle main control center device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810057663.5A CN108248878B (en) | 2018-01-22 | 2018-01-22 | Mechanical automatic control unmanned aerial vehicle main control center device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108248878A true CN108248878A (en) | 2018-07-06 |
| CN108248878B CN108248878B (en) | 2021-08-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810057663.5A Expired - Fee Related CN108248878B (en) | 2018-01-22 | 2018-01-22 | Mechanical automatic control unmanned aerial vehicle main control center device |
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| CN (1) | CN108248878B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109301716A (en) * | 2018-10-19 | 2019-02-01 | 崔保山 | A kind of heat radiating type electric power box convenient for control |
| CN110772810A (en) * | 2019-09-24 | 2020-02-11 | 扬州市鑫磊工艺品有限公司 | Wireless Bluetooth connection electric toy capable of playing music |
| CN110848301A (en) * | 2019-11-23 | 2020-02-28 | 李道飞 | Multilayer buffering damping device |
| CN111010502A (en) * | 2019-12-24 | 2020-04-14 | 吴文娟 | Automatic radiating shock-proof type image processor |
| CN111640465A (en) * | 2020-04-28 | 2020-09-08 | 温州医科大学附属眼视光医院 | Medical equipment shell anti-disassembly structure |
| CN112224415A (en) * | 2020-10-19 | 2021-01-15 | 黄远杰 | Pollination unmanned aerial vehicle with cooling and anti-deterioration functions |
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| CN109301716A (en) * | 2018-10-19 | 2019-02-01 | 崔保山 | A kind of heat radiating type electric power box convenient for control |
| CN110772810A (en) * | 2019-09-24 | 2020-02-11 | 扬州市鑫磊工艺品有限公司 | Wireless Bluetooth connection electric toy capable of playing music |
| CN110848301A (en) * | 2019-11-23 | 2020-02-28 | 李道飞 | Multilayer buffering damping device |
| CN110848301B (en) * | 2019-11-23 | 2021-02-02 | 李道飞 | Multilayer buffering damping device |
| CN111010502A (en) * | 2019-12-24 | 2020-04-14 | 吴文娟 | Automatic radiating shock-proof type image processor |
| CN111640465A (en) * | 2020-04-28 | 2020-09-08 | 温州医科大学附属眼视光医院 | Medical equipment shell anti-disassembly structure |
| CN111640465B (en) * | 2020-04-28 | 2021-08-17 | 温州医科大学附属眼视光医院 | Medical equipment shell anti-disassembly structure |
| CN112224415A (en) * | 2020-10-19 | 2021-01-15 | 黄远杰 | Pollination unmanned aerial vehicle with cooling and anti-deterioration functions |
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