CN206974117U - A kind of aircraft cup inwall rapid drying device - Google Patents
A kind of aircraft cup inwall rapid drying device Download PDFInfo
- Publication number
- CN206974117U CN206974117U CN201720754270.0U CN201720754270U CN206974117U CN 206974117 U CN206974117 U CN 206974117U CN 201720754270 U CN201720754270 U CN 201720754270U CN 206974117 U CN206974117 U CN 206974117U
- Authority
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- China
- Prior art keywords
- air
- dispelling wind
- base
- control mainboard
- supply
- 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.)
- Expired - Fee Related
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- 238000001035 drying Methods 0.000 title claims abstract description 26
- 238000010276 construction Methods 0.000 claims abstract description 6
- 210000000744 eyelid Anatomy 0.000 claims description 25
- 238000004891 communication Methods 0.000 claims description 23
- 239000007787 solid Substances 0.000 claims description 4
- 230000005611 electricity Effects 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 claims description 3
- 241000894006 Bacteria Species 0.000 abstract description 3
- 101100327917 Caenorhabditis elegans chup-1 gene Proteins 0.000 description 12
- 230000005055 memory storage Effects 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000036760 body temperature Effects 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 241001269238 Data Species 0.000 description 1
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
- 238000007605 air drying Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000006837 decompression Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005538 encapsulation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000006855 networking Effects 0.000 description 1
- 230000000474 nursing effect Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 230000033764 rhythmic process Effects 0.000 description 1
- 239000000741 silica gel Substances 0.000 description 1
- 229910002027 silica gel Inorganic materials 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 239000000057 synthetic resin Substances 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Landscapes
- Drying Of Solid Materials (AREA)
Abstract
The utility model discloses a kind of aircraft cup inwall rapid drying device, including plummer, base, power supply and dispelling wind device；The plummer is located above base, and plummer center is provided with through hole；Dispelling wind device includes air-supply arrangement, air-supply switch, control mainboard and dispelling wind pipe；Power supply, control mainboard and air-supply arrangement are located in base, and air-supply switch is located at base outer wall, and power supply, air-supply switch, control mainboard and air-supply arrangement sequentially connect；Base top surface center is provided with discharge pipe, and air-supply arrangement is located at below discharge pipe, and dispelling wind ttom of pipe end connects with discharge pipe, and the through hole at dispelling wind tube top end through plummer center upwardly extends.The utility model aircraft cup inwall rapid drying device is simple in construction, it is easy to operate, energy rapid draing aircraft cup inwall, prevent aircraft cup inwall from producing bacterium and mildew under dampness, a healthy use environment is provided for user, and the service life of aircraft cup can be extended.
Description
Technical field
The utility model is to be related to Mature Audiences technical field, concretely relates to a kind of aircraft cup inwall rapid draing
Device.
Background technology
In daily life, people's rhythm of life is accelerated, and pressure is growing day by day, and people are more and more stronger to the demand of decompression,
And simultaneously as the development in pluralism of social thoughts, health treatment for adults nursing materials are increasingly accepted, such as aircraft cup.
Aircraft cup on the market is mainly made of soft synthetic resin or silica gel at present, so that its inwall is flexible
And encapsulation, and general washable, Reusability.Due to the above-mentioned construction of aircraft cup, cause its washing after inwall not
The problem of easily drying, aircraft cup inwall and the space of its parcel is set easily to turn into a moist enclosed environment；Cause aircraft cup
Inwall breed bacteria and mildew, damage to health of people.The service life of aircraft cup has also been damaged simultaneously.
Utility model content
Purpose of utility model：To overcome the shortcomings of the existing technology, the utility model purport is quick in providing a kind of aircraft cup inwall
Drying device.
Technical scheme：In order to solve the above technical problems, the utility model adopts the following technical scheme that：
A kind of aircraft cup inwall rapid drying device, including plummer, base, power supply and dispelling wind device；The plummer is set
Above base, plummer center is provided with through hole；Dispelling wind device includes air-supply arrangement, air-supply switch, control mainboard and dispelling wind pipe；Electricity
Source, control mainboard and air-supply arrangement are located in base, and air-supply switch is located at base outer wall, power supply, air-supply switch, control mainboard and
Air-supply arrangement sequentially connects；Base top surface center is provided with discharge pipe, and air-supply arrangement is located at below discharge pipe, and dispelling wind ttom of pipe end is with going out
Airduct connects, and the through hole at dispelling wind tube top end through plummer center upwardly extends.
Operation principle：The utility model aircraft cup inwall rapid drying device is in use, aircraft cup rim of a cup is socketed in thin
Airduct periphery, by air-supply arrangement by extraneous air by dispelling wind pipeline to aircraft cup inwall most the inside, then by aircraft
The non-penetrating hole shape spatial configuration of cup inwall, make air along the space between cup inwall and dispelling wind pipeline and from aircraft rim of a cup stream
Go out, realize air circulation, reach and accelerate dry purpose.
Above-mentioned discharge pipe is truncated cone-shaped tubular structure, and the small one end of caliber connects with dispelling wind ttom of pipe end upward；Air-supply arrangement
For fan, air-supply switch is two-direction switch, air-supply arrangement is realized blowing and exhausting both of which.Top surface is groove structure, recessed
Groove portion is water storage tank.
The dispelling wind device also includes eyelid retractor, and eyelid retractor is located at dispelling wind pipe periphery, eyelid retractor top and dispelling wind tube top end phase
Connect；Bottom can be in contact with plummer upper surface, can not be also in contact with plummer upper surface.The inwall of cup can be strutted,
It is in open shape to make aircraft cup cup inwall, can accelerate to air-dry cup inwall.
Above-mentioned eyelid retractor making material be plastics, metal or other have the material of support force.
The eyelid retractor is the hard structure of list structure, network structure or solid shape；When eyelid retractor is list structure
When, radially it is distributed in dispelling wind pipe periphery.It can be easy to strut cup inwall.
The dispelling wind pipe outer wall is provided with humidity sensor and temperature sensor, and base outer wall is provided with master switch and display screen；
Display screen, humidity sensor and temperature sensor are sequentially connected in series with power supply, control mainboard, master switch respectively, control mainboard storage
There are temperature threshold and humidity threshold.The cup body temperature of record, humidity data can be sent to control mainboard in real time, and by showing
Shield display data；When display screen shows that cup body temperature, humidity do not meet the default temperature threshold of control mainboard and humidity threshold
When, open air-supply switch and carry out air-drying inwall.
Above-mentioned humidity sensor and temperature sensor can gather the temperature and humidity data in aircraft cup cup inner wall space,
And intelligent control is realized to air-supply arrangement and electrically heated rod by mainboard.Communication module of the present utility model can be with outside simultaneously
Smart machine is connected, and networking control or remote control are carried out by external smart equipment；And can be by humidity sensor and temperature
The data of sensor collection are sent to external smart equipment in real time.This allow air-dry and heating process with little need for
Completed in the case of manual operation, be convenient for people to the operation and maintenance to aircraft cup, save the time.
Above-mentioned humidity sensor and temperature sensor are no more than the space of eyelid retractor covering.
The dispelling wind inside pipe wall is provided with electrically heated rod, and base outer wall is provided with heater switch, power supply, heater switch, control master
Plate, master switch and electrically heated rod series connection.Cup inner wall temperature can be adjusted, comfortable use environment, while energy are provided for user
Cup inwall is dried, increases and dries cup inwall speed.
Above-mentioned electrically heated rod keeps being spaced farther out with temperature sensor, in order to avoid influence the temperature number of temperature sensor collection
According to.
Included in above-mentioned control mainboard and data receiver is carried out to each original paper and sends the program of instruction.
The control mainboard is provided with communication module, and communication module is sequentially connected in series with power supply, control mainboard, master switch；Temperature
Degree threshold value and humidity threshold can be configured by external smart equipment by communication module, changed.
The communication module is Bluetooth chip, WIFI chips or 3G/4G/5G chips；Smart mobile phone can be transferred data to
With the external equipment such as tablet personal computer；Also the data of the external equipments such as smart mobile phone and tablet personal computer can be received, are sent to control master
Plate.
The plummer is discoideus structure, and plate face is engraved structure, and plummer outer peripheral sidewall is fixed provided with two or more
Folder；In use, aircraft cup bottom of cup periphery is located between geometrical clamp, the connected mode of cup and geometrical clamp is to screw or pass through
Geometrical clamp inwardly clamps cup body outer wall and fixes cup.Cup stability can be improved；The plummer of engraved structure can be easy to dredge simultaneously
The gas of discharge in rim of a cup is dissipated, improves drying efficiency.In use, aircraft cup can also be by inwall to eyelid retractor inward pressure
It is fixed.
Dividing plate is provided with the base, chassis interior cavity is divided into two sheaf spaces up and down by dividing plate by centre；Dividing plate is set
There is blow vent, the lower floor of base is communicated with upper strata by blow vent；Power supply, air-supply arrangement, control mainboard are each provided at sheaf space
Interior, air-supply switch, heater switch and master switch are each provided at sheaf space outer wall；Lower layer space side wall is engraved structure, and upper strata is empty
Between side wall be engraved structure or enclosed construction.Extraneous air can be made to enter air-supply arrangement, improve drafting efficiency.
The utility model power supply is dry cell or battery, and the base side wall of position inlays cover plate corresponding to power supply, is easy to
Change power supply；When battery is battery, base side wall is provided with the charge port that connects with power supply, can external charger power supply is entered
Row charging.
The NM technology of the utility model is prior art.
Beneficial effect：The utility model aircraft cup inwall rapid drying device is simple in construction, easy to operate, is avoided that quick
Aircraft cup inwall is dried, prevents aircraft cup inwall from producing bacterium and mildew under dampness, a health is provided for user
Use environment, and the service life of aircraft cup can be extended.
Brief description of the drawings
Fig. 1 is the utility model aircraft cup inwall rapid drying device structural representation；
Fig. 2 is Fig. 1 sectional view；
Fig. 3 is the utility model aircraft cup inwall rapid drying device use state figure；
Fig. 4 is that eyelid retractor and bottom connect view with plummer in embodiment 2；
Fig. 5 is the structural representation that eyelid retractor is network structure in embodiment 3；
Fig. 6 is that eyelid retractor is the structural representation of the hard structure of solid shape in embodiment 4；
Fig. 7 is the utility model aircraft cup inwall rapid drying device circuit diagram；
In figure, 1 be aircraft cup cup, 2 be plummer, 3 be base, 4 be power supply, 5 be air-supply arrangement, 6 be air-supply switch,
7 it is control mainboard, 8 be dispelling wind pipe, 9 be discharge pipe, 10 be eyelid retractor, 11 be humidity sensor, 12 be temperature sensor, 13 is
Master switch, 14 be electrically heated rod, 15 be heater switch, 16 be communication module, 17 be geometrical clamp, 18 be dividing plate, 19 be charge port,
20 be display screen.
Embodiment
In order to more fully understand the utility model, content of the present utility model is furtherd elucidate with reference to embodiment, but
Content of the present utility model is not limited solely to the following examples.
Embodiment 1
As shown in Fig. 1-3 and Fig. 7, a kind of aircraft cup inwall rapid drying device, including plummer 2, base 3, the and of power supply 4
Dispelling wind device；The plummer 2 is located at the top of base 3, and the center of plummer 2 is provided with through hole；Dispelling wind device includes air-supply arrangement 5, air-supply
Switch 6, control mainboard 7 and dispelling wind pipe 8；Power supply 4, control mainboard 7 and air-supply arrangement 5 are located in base 3, and air-supply switch 6 is located at
The outer wall of base 3, power supply 4, air-supply switch 6, control mainboard 7 and air-supply arrangement 5 sequentially connect；The end face center of base 3 is provided with air-out
Pipe 9, air-supply arrangement 5 are located at the lower section of discharge pipe 9, and the bottom of dispelling wind pipe 8 connects with discharge pipe 9, and the top of dispelling wind pipe 8 passes through plummer 2
The through hole at center upwardly extends；Dispelling wind device also includes eyelid retractor 10, and eyelid retractor 10 is located at the periphery of dispelling wind pipe 8, the top of eyelid retractor 10
Connect with the top of dispelling wind pipe 8；Eyelid retractor 10 is list structure, is radially distributed in the periphery of dispelling wind pipe 8；The outer wall of dispelling wind pipe 8 is set
There are humidity sensor 11 and temperature sensor 12, the outer wall of base 3 is provided with master switch 13 and display screen 20；Display screen 20, humidity pass
Sensor 11 and temperature sensor 12 are sequentially connected in series with power supply 4, control mainboard 7, master switch 13 respectively, and control mainboard 7 is stored with temperature
Spend threshold value and humidity threshold；The inwall of dispelling wind pipe 8 is provided with electrically heated rod 14, and the outer wall of base 3 is provided with heater switch 15, power supply 4, heating
Switch 15, control mainboard 7, master switch 13 and electrically heated rod 14 are connected；Control mainboard 7 is provided with communication module 16, communication module
16 are sequentially connected in series with power supply 4, control mainboard 7, master switch 13；Communication module 16 is Bluetooth chip, WIFI chips or 3G/4G/5G
Chip；Plummer 2 is discoideus structure, and plate face is engraved structure, and the outer peripheral sidewall of plummer 2 is provided with two or more geometrical clamp 17；
Dividing plate 18 is provided with base 3, the internal cavities of base 3 are divided into two sheaf spaces up and down by dividing plate 18 by centre；Dividing plate 18 is provided with logical
Gas port, the lower floor of base 3 are communicated with upper strata by blow vent；Power supply 4, air-supply arrangement 5, control mainboard 7 are each provided at sheaf space
Interior, air-supply switch 6, heater switch 15 and master switch 13 are each provided at sheaf space outer wall；Lower layer space side wall is engraved structure, on
Sheaf space side wall is engraved structure or enclosed construction；Power supply 4 is dry cell, and the side wall of base 3 of position corresponding to power supply 4 inlays lid
Plate.
In use, the aircraft cup cup 1 after use is cleaned, the aircraft cup cup 1 after cleaning speckles with water stain；Will be dry
Dry device is placed on the table, the rim of a cup of the aircraft cup after cleaning is inwardly enclosed on eyelid retractor 10, aircraft cup rim of a cup and cup
Plummer 2 contacts, and is gripped by geometrical clamp 17；Now because the support force of eyelid retractor 10, the inwall of aircraft cup cup 1 strut,
And leave space between the pipeline outer wall of dispelling wind pipe 8；Air-supply switch 6 is now opened, extraneous air is passed through base 3 by air-supply arrangement 5
In the engraved structure suction base 3 of lower floor, and it is delivered to by discharge pipe 9 in dispelling wind pipe 8, air passes through the quilt of dispelling wind pipe 8
The inwall innermost portion of aircraft cup cup 1 is delivered to, then by the gap between the inwall of aircraft cup cup 1 and dispelling wind pipe 8, is passed through
The plummer 2 of engraved structure is discharged outside aircraft cup cup 1.The utility model is realized in aircraft cup cup 1 by air circulation
The rapid draing of wall；Meanwhile during air flow, air passes through the electrically heated rod 14 of the inwall of dispelling wind pipe 8, now together
When open heater switch 15, electrically heated rod 14 can to being heated by the air in wind conveying pipe road, heated air pass through
Gap between the inwall of aircraft cup cup 1 and dispelling wind pipe 8, is heated to aircraft inwall；It is empty during air flow
Gas passes through the humidity sensor 11 and temperature sensor 12 positioned at the pipeline outer wall of dispelling wind pipe 8, and the humidity and temperature data of air are by reality
When gather, the data of collection are transferred to control mainboard 7, and mainboard passes through the judgement to real time data, controls air-supply arrangement 5 and electricity
The switch of heating rod 14；Such as in need in actual use, the number that humidity sensor 11 and temperature sensor 12 are gathered
According to can also be transmitted by mainboard to communication module 16, and external smart equipment is further transferred to by communication module 16；It is and logical
Letter module 16 receive simultaneously it is outside can only the instruction that is sent of equipment, control the switch of air-supply arrangement 5 and electrically heated rod 14.Use
Person can also carry out control air-supply switch 6 and heater switch 15 manually according to the display data of display screen 20, and cup inwall is carried out
Dry.
Master switch 13 in the on state, temperature sensor 12, heater switch 15, control mainboard 7, electrically heated rod 14, leads to
Believe that the work-based logic of module 16 is as follows：
1st, the unlatching electrically heated rod 14 sent from heater switch 15 or communication module 16 is not received by control mainboard 7
Instruction before, no matter temperature sensor 12 obtain temperature data be how many, control mainboard 7 controls electrically heated rod 14 to be in
Closed mode；
The 2nd, if control mainboard 7 receives the instruction of the unlatching electrically heated rod 14 from heater switch 15 or communication module 16
When, the temperature data that temperature sensor 12 obtains is greater than or equal to the temperature threshold of the memory storage of control mainboard 7, then control mainboard 7
Electrically heated rod 14 is still controlled to be in closed mode.If control mainboard 7 is received from heater switch 15 or communication module 16
When opening the instruction of electrically heated rod 14, the temperature data that temperature sensor 12 obtains is less than the temperature threshold of the memory storage of control mainboard 7
It is worth, then control mainboard 7 controls electrically heated rod 14 to start working；And the temperature data that temperature sensor 12 obtains in heating process
Once higher than the temperature threshold of the memory storage of control mainboard 7, then control mainboard 7 controls electrically heated rod 14 to be stopped at once；
3rd, when control mainboard 7 receives the instruction for the closing electrically heated rod 14 for coming heater switch 15 or communication module 16, nothing
The temperature data obtained by temperature sensor 12 is how many, and control mainboard 7 controls electrically heated rod 14 to be stopped；
4th, when electrically heated rod 14 is in opening, heat is discharged to ambient heat, is reached to aircraft cup cup
The purpose that the inwall of body 1 is heated.
Master switch 13 in the on state, humidity sensor 11, air-supply switch 6, control mainboard 7, air-supply arrangement 5, communicates
The work-based logic of module 16 is as follows：
1st, in the case where control mainboard 7 is not received by the instruction from air-supply switch 6 or communication module 16：It is if wet
The humidity threshold that the humidity data that sensor 11 obtains is higher than the memory storage of control mainboard 7 is spent, then control mainboard 7 controls air-supply arrangement
5 start working；If the humidity data that humidity sensor 11 obtains is less than or equal to the humidity threshold of the memory storage of control mainboard 7,
Then control mainboard 7 controls air-supply arrangement 5 to be stopped.
The 2nd, if control mainboard 7 receives the instruction of the closing air-supply arrangement 5 from air-supply switch 6 or communication module 16.
Then no matter whether air-supply arrangement 5 is in running order, and mainboard controls air-supply arrangement 5 to be stopped.And mainboard pause receives
The data of humidity sensor 11, until receive restarting from communication module 16 carries out data acquisition to humidity sensor 11
Instruction or master switch 13 are restarted after closing.
If the 3, control mainboard 7 receives the instruction of the unlatching air-supply arrangement 5 from air-supply switch 6 or communication module 16,
Then no matter whether air-supply arrangement 5 is in running order, and mainboard controls air-supply arrangement 5 to start working.
4th, when air-supply arrangement 5 is in opening, hollow out knot of the air-supply arrangement 5 by extraneous air by the lower floor of base 3
In structure suction base 3, and it is delivered to by discharge pipe 9 in dispelling wind pipe 8, air is transported to aircraft cup by dispelling wind pipe 8
The inwall innermost portion of cup 1, then by the gap between the inwall of aircraft cup cup 1 and dispelling wind pipe 8, passes through holding for engraved structure
Microscope carrier 2 is discharged outside aircraft cup cup 1, is reached to the quick-drying purpose of inwall of aircraft cup cup 1.
Under the opening of master switch 13, temperature data that control mainboard 7 can obtain temperature sensor 12, humidity sensor
The real time data information such as 11 humidity datas obtained, the on off state of electrically heated rod 14, the on off state of air-supply arrangement 5, pass through
Communication module 16 is sent to external smart equipment.So that user knows.
In the on state, the temperature threshold and humidity threshold stored in control mainboard 7 can be by the mould that communicates for master switch 13
Block 16 is modified by external smart equipment.
The utility model aircraft cup inwall rapid drying device by aircraft rim of a cup by cup in use, be socketed in dispelling wind pipe 8
Periphery, extraneous air is delivered to cup inwall by dispelling wind pipe 8 by air-supply arrangement 5, then passed through by the non-of cup inwall
Logical hole shape spatial configuration, air is flowed out along the space between cup inwall and dispelling wind pipe 8 and from aircraft rim of a cup, realize air
Circulation, reach and accelerate dry purpose.
Embodiment 2
It is substantially the same manner as Example 1, except that：As shown in figure 4, the bottom of eyelid retractor 10 and the upper surface phase of plummer 2
Connect.
Embodiment 3
It is substantially the same manner as Example 1, except that：As shown in figure 5, eyelid retractor 10 is network structure, power supply 4 is electric power storage
Pond, the side wall of base 3 are provided with the charge port 19 to connect with power supply 4.
Embodiment 4
It is substantially the same manner as Example 1, except that：As shown in fig. 6, eyelid retractor 10 is the hard structure of solid shape.
It the above is only preferred embodiment of the present utility model, it should be pointed out that：For the ordinary skill people of the art
For member, on the premise of the utility model principle is not departed from, each facility locations can also be adjusted, these adjustment also should
It is considered as the scope of protection of the utility model.
Claims (10)
- A kind of 1. aircraft cup inwall rapid drying device, it is characterised in that：Including plummer, base, power supply and dispelling wind device；It is described Plummer is located above base, and plummer center is provided with through hole；Dispelling wind device include air-supply arrangement, air-supply switch, control mainboard and Dispelling wind pipe；Power supply, control mainboard and air-supply arrangement are located in base, and air-supply switch is located at base outer wall, power supply, air-supply switch, Control mainboard and air-supply arrangement sequentially connect；Base top surface center is provided with discharge pipe, and air-supply arrangement is located at below discharge pipe, dispelling wind Ttom of pipe end connects with discharge pipe, and the through hole at dispelling wind tube top end through plummer center upwardly extends.
- 2. aircraft cup inwall rapid drying device according to claim 1, it is characterised in that：The dispelling wind device also includes branch Device is supportted, eyelid retractor is located at dispelling wind pipe periphery, and eyelid retractor top connects with dispelling wind tube top end.
- 3. aircraft cup inwall rapid drying device according to claim 2, it is characterised in that：The eyelid retractor is strip knot The hard structure of structure, network structure or solid shape；When eyelid retractor is list structure, radially it is distributed in outside dispelling wind pipe Enclose.
- 4. aircraft cup inwall rapid drying device according to claim 3, it is characterised in that：The dispelling wind pipe outer wall is provided with Humidity sensor and temperature sensor, base outer wall are provided with master switch and display screen；Display screen, humidity sensor and TEMP Device is sequentially connected in series with power supply, control mainboard, master switch respectively.
- 5. aircraft cup inwall rapid drying device according to claim 4, it is characterised in that：The dispelling wind inside pipe wall is provided with Electrically heated rod, base outer wall are provided with heater switch, and power supply, heater switch, control mainboard, master switch and electrically heated rod are gone here and there successively Connection.
- 6. aircraft cup inwall rapid drying device according to claim 4, it is characterised in that：The control mainboard is provided with Communication module, communication module are sequentially connected in series with power supply, control mainboard, master switch.
- 7. aircraft cup inwall rapid drying device according to claim 6, it is characterised in that：The communication module is bluetooth Chip, WIFI chips or 3G/4G/5G chips.
- 8. the aircraft cup inwall rapid drying device according to claim 1-7 any one, it is characterised in that：The carrying Platform is discoideus structure, and plate face is engraved structure, and plummer outer peripheral sidewall is provided with two or more geometrical clamp.
- 9. aircraft cup inwall rapid drying device according to claim 8, it is characterised in that：Be provided with the base every Chassis interior cavity is divided into two sheaf spaces up and down by plate, dividing plate by centre；Dividing plate is provided with blow vent, the lower floor of base and upper strata Communicated by blow vent；Power supply, air-supply arrangement, control mainboard are each provided in sheaf space, air-supply switch, heater switch and are always opened Pass is each provided at sheaf space outer wall；Lower layer space side wall is engraved structure, and upper strata space wall is engraved structure or enclosed construction.
- 10. the aircraft cup inwall rapid drying device according to claim 1-7 any one, it is characterised in that：The electricity Source is dry cell or battery, and the base side wall of position inlays cover plate corresponding to power supply；When battery is battery, base side wall Provided with the charge port to connect with power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720754270.0U CN206974117U (en) | 2017-06-27 | 2017-06-27 | A kind of aircraft cup inwall rapid drying device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720754270.0U CN206974117U (en) | 2017-06-27 | 2017-06-27 | A kind of aircraft cup inwall rapid drying device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206974117U true CN206974117U (en) | 2018-02-06 |
Family
ID=61405819
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720754270.0U Expired - Fee Related CN206974117U (en) | 2017-06-27 | 2017-06-27 | A kind of aircraft cup inwall rapid drying device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206974117U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107144121A (en) * | 2017-06-27 | 2017-09-08 | 南京秦江网络科技有限公司 | A kind of aircraft cup inwall rapid drying device |
-
2017
- 2017-06-27 CN CN201720754270.0U patent/CN206974117U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107144121A (en) * | 2017-06-27 | 2017-09-08 | 南京秦江网络科技有限公司 | A kind of aircraft cup inwall rapid drying device |
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