CN109018322A - A kind of transport unmanned plane with heat insulation function - Google Patents
A kind of transport unmanned plane with heat insulation function Download PDFInfo
- Publication number
- CN109018322A CN109018322A CN201810760868.XA CN201810760868A CN109018322A CN 109018322 A CN109018322 A CN 109018322A CN 201810760868 A CN201810760868 A CN 201810760868A CN 109018322 A CN109018322 A CN 109018322A
- Authority
- CN
- China
- Prior art keywords
- heat
- unmanned plane
- valve
- storage box
- insulation function
- 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.)
- Withdrawn
Links
- 238000009413 insulation Methods 0.000 title claims abstract description 25
- 238000010438 heat treatment Methods 0.000 claims abstract description 31
- 238000004321 preservation Methods 0.000 claims abstract description 20
- 230000017525 heat dissipation Effects 0.000 claims abstract description 13
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 239000010687 lubricating oil Substances 0.000 claims description 3
- 235000003140 Panax quinquefolius Nutrition 0.000 claims 1
- 240000005373 Panax quinquefolius Species 0.000 claims 1
- 230000006835 compression Effects 0.000 claims 1
- 238000007906 compression Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 230000007774 longterm Effects 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 239000004677 Nylon Substances 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 229920001778 nylon Polymers 0.000 description 2
- 230000033228 biological regulation Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
-
- 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
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
-
- 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
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Devices That Are Associated With Refrigeration Equipment (AREA)
Abstract
The present invention relates to a kind of transport unmanned plane with heat insulation function, including main body and several power devices, storage box is equipped in main body, heat preservation mechanism and dust-proof mechanism, clamp system is equipped in storage box, heat preservation mechanism includes insulating tube, air admission unit, heating unit and temperature reducing unit, air admission unit includes driving assembly, push plate, compressed pipe, first valve, second valve and air inlet pipe, temperature reducing unit includes air blower, heat dissipation tank and several heat-dissipating pipes, clamp system includes the second motor, nut, clamping plate, screw rod and guide rod, the transport unmanned plane with heat insulation function, pass through heat preservation mechanism, the transport unmanned plane can more be precisely controlled the temperature in storage box, so that cargo can save for a long time, moreover, pass through clamp system, cargo can be effectively fixed in storage box by the transport unmanned plane, to It prevents the cargo of small volume from acutely shaking during transportation, avoids cargo damage.
Description
Technical field
The present invention relates to unmanned plane field, in particular to a kind of transport unmanned plane with heat insulation function.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.
Existing transport unmanned plane needs to transport various cargos, but existing transport unmanned plane does not have attemperator,
Cause some cargos for needing to control temperature rotten or damage, moreover, the volume of different cargos is not quite similar, and leads to volume
Lesser cargo acutely shakes during transportation, causes cargo damage.
Summary of the invention
The technical problem to be solved by the present invention is for overcome the deficiencies in the prior art, providing a kind of with heat insulation function
Transport unmanned plane.
The technical solution adopted by the present invention to solve the technical problems is: a kind of transport unmanned plane with heat insulation function,
Including main body and several power devices, each power device is circumferentially evenly distributed on the periphery of main body, is equipped with and saves in the main body
Case, heat preservation mechanism and dust-proof mechanism, the storage box is interior to be equipped with clamp system；
The heat preservation mechanism includes insulating tube, air admission unit, heating unit and temperature reducing unit, and the insulating tube is wrapped in guarantor
It deposits on case, along the periphery Spiral distribution of storage box, the external of the insulating tube and main body be connected to the insulating tube, the heating
Unit and temperature reducing unit are separately positioned on main intracorporal top and bottom, and the air admission unit setting is single in heating unit and cooling
Between member；
The air admission unit includes driving assembly, push plate, compressed pipe, the first valve, the second valve and air inlet pipe, the drive
Dynamic component and push plate are sequentially connected, and the push plate is arranged in compressed pipe, and the compressed pipe is horizontally disposed, and first valve is set
It sets in the lower section of the second valve, the compressed pipe is connected to by the first valve with the external of main body, and the compressed pipe passes through second
Valve is connected to air inlet pipe, and the air inlet pipe is vertically arranged, the top and bottom end of the air inlet pipe respectively with heating unit and drop
Warm unit connects, and is set in the air inlet pipe there are two third valve, two third valves are separately positioned on the top in air inlet pipe
The bottom and；
The heating unit includes heater box and several heating tubes, and one end of the heater box is connected to air inlet pipe, described
The other end of heater box is connected to insulating tube, and each heating tube is evenly distributed in heater box；
The temperature reducing unit includes air blower, heat dissipation tank and several heat-dissipating pipes, one end of the air blower and main body it is outer
Portion's connection, the other end of the air blower are connected to the top of heat dissipation tank, and the bottom of the heat-dissipating pipe is connected to the external of main body,
Each heat-dissipating pipe is evenly distributed in heat dissipation tank, and each heat-dissipating pipe is vertically arranged, and the top of the heat-dissipating pipe is connected to air inlet pipe, institute
The bottom end for stating heat-dissipating pipe is connected to insulating tube；
The clamp system includes the second motor, nut, clamping plate, screw rod and guide rod, and second motor is vertically arranged
Top in storage box, the screw rod is vertically arranged, and second motor is connect with screw rod transmission, and the nut is set in silk
On bar, the nut is matched with screw rod, and the clamping plate is fixedly connected with nut, and the guide rod is vertically arranged, the guide rod
Top and bottom end be fixedly connected respectively with the top and bottom in storage box, the guide rod pass through clamping plate.
Preferably, the movement in order to realize push plate, the driving component includes air pump, cylinder and piston, the air pump
It is connected to cylinder, the cylinder is horizontally disposed, and one end of the piston is arranged in cylinder, the other end of the piston and push plate
It is fixedly connected.
Preferably, the air return in compressed pipe prevents the air in air inlet pipe from returning to the outside of main body in order to prevent
It flow in compressed pipe, first valve and the second valve are check-valves.
Preferably, in order to accurately control the switch of third valve, the third valve is solenoid valve.
Preferably, in order to enhance the heat transfer effect of heating tube and heat-dissipating pipe, the heating tube and heat-dissipating pipe are copper pipe.
Preferably, dust enters storage box in order to prevent, cargo is prevented to be detached from storage box, the dustproof unit includes the
One motor, turntable, fixed rope, shaft, dustcloth and elevator, the first motor and shaft are separately positioned under storage box
Side and top, the first motor and turntable are sequentially connected, and one end of the fixed rope is arranged on turntable, the fixed rope
It is fixedly connected below the other end and elevator, one end of the dustcloth is arranged in shaft, the other end of the dustcloth
It is fixedly connected with above elevator, torsionspring is equipped between the shaft and main body.
Preferably, in order to enable fixed rope can long-term stable work, the fixed rope be nylon rope.
Preferably, in order to enable first motor and the second motor can long-term stable work, the first motor and
Second motor is servo motor.
Preferably, in order to clamp cargo, the lower section of the clamping plate is equipped with several rubber antiskid items.
Preferably, being coated with lubricating oil between the nut and screw rod to reduce transmission loss between nut and screw rod.
The invention has the advantages that this has the transport unmanned plane of heat insulation function, by heat preservation mechanism, the transport nobody
Machine can more be precisely controlled the temperature in storage box, so that cargo can save for a long time, with existing heat preservation mechanism
It compares, the temperature control of the heat preservation mechanism is more accurate, and moreover, by clamp system, which can be effective
Cargo is fixed in storage box, to prevent the cargo of small volume from acutely shaking during transportation, cargo is avoided to damage
Bad, compared with existing clamp system, the cargo fixed effect of the clamp system is preferable.
Detailed description of the invention
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the structural schematic diagram of the transport unmanned plane with heat insulation function of the invention；
Fig. 2 is the structural schematic diagram of the air admission unit of the transport unmanned plane with heat insulation function of the invention；
Fig. 3 is the structural schematic diagram of the dust-proof mechanism of the transport unmanned plane with heat insulation function of the invention；
Fig. 4 is the structural schematic diagram of the clamp system of the transport unmanned plane with heat insulation function of the invention；
In figure: 1. main bodys, 2. power devices, 3. storage boxes, 4. insulating tubes, 5. air pumps, 6. cylinders, 7. pistons, 8. push plates,
9. compressed pipe, 10. first valves, 11. second valves, 12. air inlet pipe, 13. heater boxes, 14. heating tubes, 15. air blowers, 16.
Heat dissipation tank, 17. heat-dissipating pipes, 18. first motors, 19. turntables, 20. fixed ropes, 21. shafts, 22. dustcloths, 23. elevators,
24. the second motor, 25. nuts, 26. clamping plates, 27. screw rods, 28. guide rods, 29. third valves.
Specific embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These attached drawings are simplified schematic diagram, only with
Illustration illustrates basic structure of the invention, therefore it only shows the composition relevant to the invention.
As described in Figure 1, a kind of transport unmanned plane with heat insulation function, including main body 1 and several power devices 2, it is each dynamic
The circumferential periphery for being evenly distributed on main body 1 of power device 2, the main body 1 is interior to be equipped with storage box 3, heat preservation mechanism and dust-proof mechanism, institute
It states and is equipped with clamp system in storage box 3；
The heat preservation mechanism includes insulating tube 4, air admission unit, heating unit and temperature reducing unit, and the insulating tube 4 is wrapped in
On storage box 3, along the periphery Spiral distribution of storage box 3, the external of the insulating tube 4 and main body 1 be connected to the insulating tube 4,
The heating unit and temperature reducing unit are separately positioned on the top and bottom in main body 1, and the air admission unit setting is single in heating
Between member and temperature reducing unit；
In fact, being additionally provided with temperature sensor and PLC in storage box 3, the temperature sensor is electrically connected with PLC, described
PLC is electrically connected with two third valves 29, and temperature sensor monitors the temperature in storage box 3 in real time, passes through PLC control two the
The switch of three valves 29 realizes the temperature control of storage box 3.
As shown in Fig. 2, the air admission unit includes driving assembly, push plate 8, compressed pipe 9, the first valve 10, the second valve
11 and air inlet pipe 12, the driving component and push plate 8 are sequentially connected, and the push plate 8 is arranged in compressed pipe 9, the compressed pipe 9
Horizontally disposed, the lower section of the second valve 11 is arranged in first valve 10, and the compressed pipe 9 passes through the first valve 10 and main body
1 external connection, the compressed pipe 9 are connected to by the second valve 11 with air inlet pipe 12, and the air inlet pipe 12 is vertically arranged, described
The top and bottom end of air inlet pipe 12 are connect with heating unit and temperature reducing unit respectively, are set in the air inlet pipe 12 there are two third valve
Door 29, two third valves 29 are separately positioned on the top and bottom in air inlet pipe 12；
The heating unit includes heater box 13 and several heating tubes 14, and one end of the heater box 13 and air inlet pipe 12 connect
Logical, the other end of the heater box 13 is connected to insulating tube 4, and each heating tube 14 is evenly distributed in heater box 13；
The temperature reducing unit includes air blower 15, heat dissipation tank 16 and several heat-dissipating pipes 17, one end of the air blower 15 with
The external connection of main body 1, the other end of the air blower 15 are connected to the top of heat dissipation tank 16, the bottom of the heat-dissipating pipe 17 and
The external connection of main body 1, each heat-dissipating pipe 17 are evenly distributed in heat dissipation tank 16, and each heat-dissipating pipe 17 is vertically arranged, the heat dissipation
The top of pipe 17 is connected to air inlet pipe 12, and the bottom end of the heat-dissipating pipe 17 is connected to insulating tube 4；
When heat preservation mechanism is run, air admission unit work, driving assembly driving push plate 8 moves back and forth in compressed pipe 9, passes through
The air of the outside of main body 1 is pressed into air inlet pipe 12, when needing to heat up, heating unit by the first valve 10 and the second valve 11
Hot-air is pressed into insulating tube 4 by work, the air in 14 electrified regulation heater box 13 of heating tube, the air-flow in air inlet pipe 12, from
And storage box 3 is heated, when needing to cool down, the air of body exterior is pressed into heat dissipation tank 16 by temperature reducing unit work, air blower 15,
So that the heat in air in several heat-dissipating pipes 17 is taken away, cold air enters insulating tube 4, realizes the cooling of storage box 3.
By heat preservation mechanism, which can more be precisely controlled the temperature in storage box 3, so that cargo
It can save for a long time, compared with existing heat preservation mechanism, the temperature control of the heat preservation mechanism is more accurate.
As shown in figure 4, the clamp system includes the second motor 24, nut 25, clamping plate 26, screw rod 27 and guide rod 28,
Second motor 24 is vertically provided at the top in storage box 3, and the screw rod 27 is vertically arranged, second motor 24 and silk
Bar 27 is sequentially connected, and the nut 25 is set on screw rod 27, and the nut 25 is matched with screw rod 27, the clamping plate 26 and nut
25 are fixedly connected, and the guide rod 28 is vertically arranged, the top and bottom end of the guide rod 28 respectively with the top in storage box 3
It is fixedly connected with bottom, the guide rod 28 passes through clamping plate 26.
Second motor 24 drives screw rod 27 to rotate, so that nut 25 declines, clamping plate 26 is allowed to move down, by goods clamping,
Prevent cargo from sliding.
By clamp system, which can be effectively fixed on cargo in storage box 3, to prevent volume
Lesser cargo acutely shakes during transportation, avoids cargo damage, compared with existing clamp system, the clamp system
Cargo fixed effect is preferable.
Preferably, the movement in order to realize push plate 8, the driving component includes air pump 5, cylinder 6 and piston 7, described
Air pump 5 is connected to cylinder 6, and the cylinder 6 is horizontally disposed, and one end of the piston 7 is arranged in cylinder 6, the piston 7 it is another
One end is fixedly connected with push plate 8.Air pump 5 is stretched out or is withdrawn, push away to realize by changing the air pressure in cylinder 6, driving piston 7
The movement of plate 8.
Preferably, the air return in compressed pipe 9 prevents the sky in air inlet pipe 12 to the outside of main body 1 in order to prevent
Gas is back in compressed pipe 9, and first valve 10 and the second valve 11 are check-valves.
Preferably, in order to accurately control the switch of third valve 29, the third valve 29 is solenoid valve.
Preferably, in order to enhance the heat transfer effect of heating tube 14 and heat-dissipating pipe 17, the heating tube 14 and heat-dissipating pipe 17
It is copper pipe.
As shown in figure 3, the dustproof unit includes first motor 18, turntable 19, fixed rope 20, shaft 21, dustcloth 22
With elevator 23, the first motor 18 and shaft 21 are separately positioned on the following above and of storage box 3, the first motor 18
It is sequentially connected with turntable 19, one end of the fixed rope 20 is arranged on turntable 19, the other end of the fixed rope 20 and lifting
The lower section of block 23 is fixedly connected, and one end of the dustcloth 22 is arranged in shaft 21, the other end and liter of the dustcloth 22
The top of drop block 23 is fixedly connected, and torsionspring is equipped between the shaft 21 and main body 1.First motor 18 drives 19 turns of turntable
It is dynamic, fixed rope 20 is tightened or loosened, when fixed rope 20 is tightened, drives the decline of dustcloth 22 to block storage box 3 elevator 23,
Dust enters storage box 3 in order to prevent, and when fixed rope 20 loosens, torsionspring rotates shaft 21, and dustcloth 22 is received
It returns, consequently facilitating cargo is put into storage box 3 by people.
Preferably, in order to enable fixed rope 20 can long-term stable work, the fixed rope 20 be nylon rope.
Preferably, in order to enable first motor 18 and the second motor 24 can long-term stable work, first electricity
Machine 18 and the second motor 24 are servo motor.
Preferably, in order to clamp cargo, the lower section of the clamping plate 26 is equipped with several rubber antiskid items.
Preferably, being applied between the nut 25 and screw rod 27 to reduce transmission loss between nut 25 and screw rod 27
There is lubricating oil.
The working principle of the transport unmanned plane with heat insulation function: when heat preservation mechanism is run, air admission unit work will be led
The air of the outside of body 1 is pressed into air inlet pipe 12, and when needing to heat up, storage box 3 is heated in heating unit work, when needing to cool down
When, the cooling of storage box 3 is realized in temperature reducing unit work, in addition, the second motor 24 drives 27 turns of screw rod when clamp system is run
It is dynamic, so that nut 25 declines, allows clamping plate 26 to move down, by goods clamping, prevent cargo from sliding.
Compared with prior art, the transport unmanned plane with heat insulation function passes through heat preservation mechanism, the unmanned function of the transport
Enough temperature being more precisely controlled in storage box 3, so that cargo can save for a long time, with existing heat preservation mechanism phase
Than the temperature control of the heat preservation mechanism is more accurate, and moreover, by clamp system, which can be effective
Cargo is fixed in storage box 3, to prevent the cargo of small volume from acutely shaking during transportation, cargo is avoided to damage
Bad, compared with existing clamp system, the cargo fixed effect of the clamp system is preferable.
Taking the above-mentioned ideal embodiment according to the present invention as inspiration, through the above description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property range is not limited to the contents of the specification, it is necessary to which the technical scope thereof is determined according to the scope of the claim.
Claims (10)
1. a kind of transport unmanned plane with heat insulation function, which is characterized in that including main body (1) and several power devices (2), respectively
Power device (2) is circumferentially evenly distributed on the periphery of main body (1), be equipped in the main body (1) storage box (3), heat preservation mechanism and
Dust-proof mechanism, the storage box (3) is interior to be equipped with clamp system；
The heat preservation mechanism includes insulating tube (4), air admission unit, heating unit and temperature reducing unit, and the insulating tube (4) is wrapped in
On storage box (3), the insulating tube (4) along storage box (3) periphery Spiral distribution, the insulating tube (4) and main body (1)
Outside connection, the heating unit and temperature reducing unit are separately positioned on the top and bottom in main body (1), and the air admission unit is set
It sets between heating unit and temperature reducing unit；
The air admission unit include driving assembly, push plate (8), compressed pipe (9), the first valve (10), the second valve (11) and into
Tracheae (12), the driving component and push plate (8) are sequentially connected, and push plate (8) setting is in compressed pipe (9), the compression
It manages (9) to be horizontally disposed with, in the lower section of the second valve (11), the compressed pipe (9) passes through first for the first valve (10) setting
Valve (10) is connected to the external of main body (1), and the compressed pipe (9) is connected to by the second valve (11) with air inlet pipe (12), institute
State that air inlet pipe (12) is vertically arranged, the top and bottom end of the air inlet pipe (12) are connect with heating unit and temperature reducing unit respectively,
It is set in the air inlet pipe (12) there are two third valve (29), two third valves (29) are separately positioned in air inlet pipe (12)
Top and bottom；
The heating unit includes heater box (13) and several heating tubes (14), one end of the heater box (13) and air inlet pipe
(12) it is connected to, the other end of the heater box (13) is connected to insulating tube (4), and each heating tube (14) is evenly distributed on heater box
(13) in；
The temperature reducing unit includes air blower (15), heat dissipation tank (16) and several heat-dissipating pipes (17), and the one of the air blower (15)
It holds and is connected to the external of main body (1), the other end of the air blower (15) is connected to the top of heat dissipation tank (16), the heat-dissipating pipe
(17) bottom is connected to the external of main body (1), and each heat-dissipating pipe (17) is evenly distributed in heat dissipation tank (16), each heat-dissipating pipe (17)
Vertically arranged, the top of the heat-dissipating pipe (17) is connected to air inlet pipe (12), the bottom end of the heat-dissipating pipe (17) and insulating tube
(4) it is connected to；
The clamp system includes the second motor (24), nut (25), clamping plate (26), screw rod (27) and guide rod (28), described
Second motor (24) is vertically provided at the top in storage box (3), and the screw rod (27) is vertically arranged, second motor (24)
It is sequentially connected with screw rod (27), the nut (25) is set on screw rod (27), and the nut (25) matches with screw rod (27), institute
It states clamping plate (26) to be fixedly connected with nut (25), the guide rod (28) is vertically arranged, the top and bottom of the guide rod (28)
End is fixedly connected with the top and bottom in storage box (3) respectively, and the guide rod (28) passes through clamping plate (26).
2. as described in claim 1 with the transport unmanned plane of heat insulation function, which is characterized in that the driving component includes gas
Pump (5), cylinder (6) and piston (7), the air pump (5) are connected to cylinder (6), and the cylinder (6) is horizontally disposed, the piston
(7) in cylinder (6), the other end of the piston (7) is fixedly connected with push plate (8) for one end setting.
3. as described in claim 1 with heat insulation function transport unmanned plane, which is characterized in that first valve (10) and
Second valve (11) is check-valves.
4. as described in claim 1 with the transport unmanned plane of heat insulation function, which is characterized in that the third valve (29) is
Solenoid valve.
5. as described in claim 1 with the transport unmanned plane of heat insulation function, which is characterized in that the heating tube (14) and scattered
Heat pipe (17) is copper pipe.
6. as described in claim 1 with the transport unmanned plane of heat insulation function, which is characterized in that the dustproof unit includes the
One motor (18), turntable (19), fixed rope (20), shaft (21), dustcloth (22) and elevator (23), the first motor
(18) and shaft (21) is separately positioned on the following above and of storage box (3), and the first motor (18) and turntable (19) are driven
One end of connection, the fixed rope (20) is arranged on turntable (19), the other end of the fixed rope (20) and elevator (23)
Lower section be fixedly connected, one end of the dustcloth (22) is arranged on shaft (21), the other end of the dustcloth (22) with
Elevator is fixedly connected above (23), and torsionspring is equipped between the shaft (21) and main body (1).
7. as claimed in claim 6 with the transport unmanned plane of heat insulation function, which is characterized in that the fixed rope (20) is Buddhist nun
Long Sheng.
8. as claimed in claim 6 with heat insulation function transport unmanned plane, which is characterized in that the first motor (18) and
Second motor (24) is servo motor.
9. as described in claim 1 with the transport unmanned plane of heat insulation function, which is characterized in that the lower section of the clamping plate (26)
Equipped with several rubber antiskid items.
10. as described in claim 1 with the transport unmanned plane of heat insulation function, which is characterized in that the nut (25) and silk
Bar is coated with lubricating oil between (27).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810760868.XA CN109018322A (en) | 2018-07-12 | 2018-07-12 | A kind of transport unmanned plane with heat insulation function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810760868.XA CN109018322A (en) | 2018-07-12 | 2018-07-12 | A kind of transport unmanned plane with heat insulation function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109018322A true CN109018322A (en) | 2018-12-18 |
Family
ID=64641961
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810760868.XA Withdrawn CN109018322A (en) | 2018-07-12 | 2018-07-12 | A kind of transport unmanned plane with heat insulation function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109018322A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110626503A (en) * | 2019-10-29 | 2019-12-31 | 南京茗淇信息科技有限公司 | Heat dissipation type express delivery unmanned aerial vehicle with reinforcement function |
| CN112269417A (en) * | 2020-10-29 | 2021-01-26 | 湖南库里斯智能科技有限公司 | Heat recovery system of mobile power supply for unmanned aerial vehicle |
-
2018
- 2018-07-12 CN CN201810760868.XA patent/CN109018322A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110626503A (en) * | 2019-10-29 | 2019-12-31 | 南京茗淇信息科技有限公司 | Heat dissipation type express delivery unmanned aerial vehicle with reinforcement function |
| CN112269417A (en) * | 2020-10-29 | 2021-01-26 | 湖南库里斯智能科技有限公司 | Heat recovery system of mobile power supply for unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109018322A (en) | A kind of transport unmanned plane with heat insulation function | |
| CN1902087A (en) | Cooling system for the cooling of heat-producing devices in an aircraft | |
| CN106545391B (en) | A kind of boat diesel engine waste heat from tail gas thermal gradient energy utilizes device | |
| SE458715B (en) | AIR CONDITIONING AIR CONDITIONING SYSTEM | |
| US20180266742A1 (en) | Dc heating and cooling systems and methods | |
| CN110481412B (en) | Refrigerator carriage and refrigerator car with temperature field dynamic regulation and control function | |
| CN103691500A (en) | Simulation system for high-low-temperature environment of controlled flexible cavity body | |
| CN109944768A (en) | Electric drive gas booster | |
| CN107709161A (en) | Blended electric power | |
| CN108321997A (en) | Continuous vacuum dipping lacquer production line | |
| CN207969258U (en) | A kind of electronic engineering switch board | |
| CN109606666A (en) | A kind of stable type unmanned flight's device with function of temperature control for logistics | |
| SG175852A1 (en) | Motor vehicle | |
| CN206172550U (en) | Large capacity piston granule pump | |
| DE102008029853A1 (en) | Cooling system for a van with several cooling chambers | |
| CN108657050A (en) | The hydraulic lifting system and dumper of dumper | |
| US20160097605A1 (en) | Hydraulic Closure Unit and Retrofit System for a Plate Heat Exchanger | |
| CN113752371B (en) | Be used for new material board pressurization to evaporate pressure curing means | |
| CN213020453U (en) | Movable refrigeration house | |
| CN2529173Y (en) | Automatic continuous vacuum freeze drying device | |
| EP2426393A1 (en) | Pressure-reducing gas storage devic, gas injection system and automobile | |
| CN206599199U (en) | A kind of cold chain distribution robot | |
| CN116142644B (en) | Automatic change on-vehicle container of keeping in of beasts and birds that die of illness | |
| CN208648602U (en) | A kind of cooling device of hoist engine | |
| CN219691701U (en) | Vacuum pump pressure reducing device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20200225 Address after: 518000 Nanshan Software Park B2110, No. 10128, Shennan Avenue, Liancheng community, Nantou street, Nanshan District, Shenzhen City, Guangdong Province Applicant after: Shenzhen Best New Energy Technology Development Co Ltd Address before: 518000 Dongta 3004, Nanshan Digital Culture Industry Base, Nanshan District, Shenzhen City, Guangdong Province Applicant before: Work in peace and contentment Science and Technology Ltd. in Shenzhen |
|
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181218 |