CN207374680U - A kind of cold and hot air interchanger of ground cockpit - Google Patents
A kind of cold and hot air interchanger of ground cockpit Download PDFInfo
- Publication number
- CN207374680U CN207374680U CN201721244516.6U CN201721244516U CN207374680U CN 207374680 U CN207374680 U CN 207374680U CN 201721244516 U CN201721244516 U CN 201721244516U CN 207374680 U CN207374680 U CN 207374680U
- Authority
- CN
- China
- Prior art keywords
- housing
- cold
- cockpit
- hot
- ground
- 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.)
- Active
Links
Abstract
A kind of cold and hot air interchanger of ground cockpit, including housing, switch, handle, power interface and Air Filter, switch is arranged on the forepart of housing, handle is arranged on the top of housing, power interface is arranged on the rear portion of housing upper surface, Air Filter is arranged on the rear portion of housing, further include cold chamber, cooling fin, semiconductor chilling plate, fan, resistance wire and hot chamber, cold chamber sets left side inside housings, hot chamber sets right side inside housings, cooling fin is arranged on wall surface both sides among two inner cavity of housing, semiconductor chilling plate is arranged among two inner cavity of housing inside wall surface, the refrigeration side of semiconductor chilling plate is located at cold chamber heating side and is located at hot chamber.Cockpit cold and hot ventilation device structure in ground is compact, light-weight, price is low, easy to use for this, needs, into during cockpit work, as long as powering on, just persistently to cool down or heat to cockpit, suitable working environment is provided to ground crew in ground crew.
Description
Technical field
The utility model is related to a kind of air interchanger, more particularly to a kind of air interchanger for having refrigeration and heating effect.
Background technology
In the hot weather of summer, the temperature being parked in the aircraft cockpit on airport can be higher, cockpit temperature one
As up to 50 DEG C or more.In such a case, along with cabin interior narrow space, ground crew can go out when entering cockpit work
The now discomfort of extreme, seriously affects work efficiency.Equally also it is present with the situation that temperature is extremely low in cockpit in cold winter.For
It does not influence ground crew and carries out routine work, it is necessary to which the temperature in cockpit is adjusted to suitable temperature.
At present, the measure generally taken is to be adjusted with ground air-conditioning car by being filled with cold air or hot gas to cockpit to suitable
Temperature.But there are problems that, first, airport is equipped with, ground air-conditioning car ratio is too low, and some is directly not equipped with；Second is that ground
Air-conditioned coach volume is big, it is necessary to which the time prepared is long；Third, need specially safeguard air-conditioned coach personnel, it is necessary to operating personnel's mistake
It is more；It is fourth, expensive.
Utility model content
In order to solve the above technical problems, the utility model provides, one kind is simple in structure, and easy to operation, saving electric energy carries
The cold and hot air interchanger of ground cockpit of high workload efficiency.
A kind of cold and hot air interchanger of ground cockpit, including housing, switch, handle, power interface and Air Filter, switch is set
In the forepart of housing, handle is arranged on the top of housing, and power interface is arranged on the rear portion of housing upper surface, and Air Filter is arranged on
The rear portion of housing, further includes cold chamber, cooling fin, semiconductor chilling plate, fan, resistance wire and hot chamber, and cold chamber is arranged in housing
On the left of portion, hot chamber sets right side inside housings, and cooling fin is arranged on wall surface both sides, semiconductor chilling plate among two inner cavity of housing
It is arranged among two inner cavity of housing inside wall surface, the refrigeration side of semiconductor chilling plate is located at cold chamber heating side and is located at hot chamber, fan
It is arranged on middle part in housing and is located at Air Filter front end, resistance wire is arranged on hot chamber forward position, semiconductor refrigerating on the right side of housing
Piece and resistance wire are connected by the converted switch of cable with power supply, and fan is connected by cable with power supply.
Further, which further includes air deflector, and air deflector is mounted on the front end interface of housing
Place.
Further, the lower housing portion of the cold and hot air interchanger of ground cockpit is additionally provided with hook.
Have the beneficial effect that the cold and hot ventilation device structure of ground cockpit is small by what the technological means the utility model obtained
Ingeniously, it is light-weight, price is low, easy to use, ground crew need into cockpit work when, as long as powering on, just can persistently
Cool down to cockpit or heat, suitable working environment is provided to ground crew.
Description of the drawings
Fig. 1 is the outline structural diagram of the utility model.
Fig. 2 is the internal structure schematic diagram of the utility model.
In the figure 1, air deflector；2nd, housing；3rd, change-over switch；4th, handle；5th, power interface；6th, Air Filter；7th, cold chamber；
8th, cooling fin；9th, semiconductor chilling plate；10th, fan；11st, resistance wire 12, hot chamber.
Specific embodiment
The principle and feature of the utility model are described below in conjunction with attached drawing, example is served only for explaining practical new
Type is not intended to limit the scope of the utility model.
A kind of cold and hot air interchanger of ground cockpit, including housing 2, change-over switch 3, handle 4, power interface 5 and Air Filter
6, change-over switch 3 is arranged on the forepart of housing 2, and handle 4 is arranged on the top of housing 2, and power interface 5 is arranged on 2 upper table of housing
The rear portion in face, Air Filter 6 are arranged on the rear portion of housing 2, it is characterised in that：The cold and hot air interchanger of ground cockpit further include cold chamber 7,
Cooling fin 8, semiconductor chilling plate 9, fan 10, resistance wire 11 and hot chamber 12, cold chamber 7 are arranged on 2 inside left of housing, hot chamber 12
2 inner right side of housing is arranged on, cooling fin 8 is arranged on wall surface both sides among 2 liang of inner cavities of housing, and semiconductor chilling plate 9 is arranged on
Among 2 liang of inner cavities of housing inside wall surface, the refrigeration side of semiconductor chilling plate 9 is located at cold chamber 7 heating side and is located at hot chamber 12, fan 10
It is arranged on middle part in housing 2 and is located at 6 front end of Air Filter, resistance wire 11 is arranged on 2 hot 12 forward position of chamber in right side of housing, partly leads
Body cooling piece 9 and resistance wire 11 are connected by the converted switch 3 of cable with power supply, and fan 10 is connected by cable with power supply.
The cold and hot air interchanger of ground cockpit further includes air deflector 1, and air deflector 1 is mounted at the front end interface of housing 2.Its
Effect is the interface installation site of adjustment air deflector 1 as needed, the hot gas or cold air of needs is imported cockpit, another way is led
Go out out of my cabin.
2 lower part of housing of the cold and hot air interchanger of ground cockpit is additionally provided with hook.For being suspended on cockpit apperture fame,
It can be easy to use on ground and aircraft cockpit.
The operation principle of the utility model be can be hung on cockpit apperture fame by the hook on housing 2 or directly
Ground is placed in, aspirating air from 2 rear portion of housing by fan 10 enters housing 2, is divided into two-way in housing 2, between two-way mutually
It does not connect.Semiconductor chilling plate 9 is the heat absorption exothermic semiconductor in one side in one side after a kind of energization, and refrigeration and heating generate simultaneously,
It is a kind of Refrigeration Technique of negative thermal resistance.Semiconductor chilling plate 9 has that size is small, simple in structure, without movable member and from completely negative
Lotus refrigeration at full capacity heating when control the advantages that easy.Refrigeration that semiconductor chilling plate 9 in housing 2 generates after being powered and
Heating effect is conducted to the air in housing 2 by thermally conductive sheet, and cold and hot two-way air-flow is formed in housing 2, then by preceding
The cold air or hot gas of needs are passed to cockpit, refrigeration or heating cabin air by the air deflector 1 at end.Since semiconductor chilling plate 9 exists
Refrigeration can also generate substantial amounts of heat simultaneously, and semiconductor chilling plate change-over switch 3 can be disconnected when needing heating effect, connect
The change-over switch 3 of resistance wire 11, just only heating effect, it is possible to reduce the consuming of electricity.
Above-mentioned technical proposal only embodies the optimal technical scheme of technical solutions of the utility model, the technology of the art
Personnel embody some variations that some of which part may be made the principle of the utility model, belong to the utility model
Protection domain within.
Claims (3)
1. a kind of cold and hot air interchanger of ground cockpit, including housing (2), change-over switch (3), handle (4), power interface (5) and
Air Filter (6), the change-over switch (3) are arranged on the forepart of housing (2), and the handle (4) is arranged on the top of housing (2),
The power interface (5) is arranged on the rear portion of housing (2) upper surface, and the Air Filter (6) is arranged on the rear portion of housing (2),
It is characterized in that：The cold and hot air interchanger of ground cockpit further includes cold chamber (7), cooling fin (8), semiconductor chilling plate (9), fan
(10), resistance wire (11) and hot chamber (12), the cold chamber (7) are arranged on housing (2) inside left, and the hot chamber (12) is arranged on
Housing (2) inner right side, the cooling fin (8) are arranged on wall surface both sides, the semiconductor chilling plate among (2) two inner cavity of housing
(9) it is arranged among (2) two inner cavity of housing inside wall surface, the refrigeration side of the semiconductor chilling plate (9) is located at cold chamber (7) heating
Side is located at hot chamber (12), and the fan (10) is arranged on middle part in housing (2) and is located at Air Filter (6) front end, the resistance wire
(11) hot chamber (12) forward position on the right side of housing (2) is arranged on, the semiconductor chilling plate (9) and resistance wire (11) pass through cable
Converted switch (3) is connected with power supply, and the fan (10) is connected by cable with power supply.
2. cockpit cold and hot air interchanger in ground according to claim 1, it is characterised in that：The cold and hot ventilation of ground cockpit
Device further includes air deflector (1), and the air deflector (1) is mounted at the front end interface of housing (2).
3. cockpit cold and hot air interchanger in ground according to claim 1 or 2, it is characterised in that：Housing (2) lower part is also
It is provided with hook.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721244516.6U CN207374680U (en) | 2017-09-26 | 2017-09-26 | A kind of cold and hot air interchanger of ground cockpit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721244516.6U CN207374680U (en) | 2017-09-26 | 2017-09-26 | A kind of cold and hot air interchanger of ground cockpit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207374680U true CN207374680U (en) | 2018-05-18 |
Family
ID=62341037
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721244516.6U Active CN207374680U (en) | 2017-09-26 | 2017-09-26 | A kind of cold and hot air interchanger of ground cockpit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207374680U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108849108A (en) * | 2018-06-01 | 2018-11-23 | 刘启标 | A kind of incubator of the agricultural convenient for adjusting temperature |
| CN110834733A (en) * | 2019-11-14 | 2020-02-25 | 中国商用飞机有限责任公司 | Air preparation system |
-
2017
- 2017-09-26 CN CN201721244516.6U patent/CN207374680U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108849108A (en) * | 2018-06-01 | 2018-11-23 | 刘启标 | A kind of incubator of the agricultural convenient for adjusting temperature |
| CN110834733A (en) * | 2019-11-14 | 2020-02-25 | 中国商用飞机有限责任公司 | Air preparation system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204020475U (en) | Automobile paltie effect air conditioner | |
| CN204032549U (en) | A kind of Portable semiconductor refrigerating air conditioning umbrella | |
| CN203690448U (en) | System for heating and cooling battery pack through vehicle air conditioner system | |
| CN207374680U (en) | A kind of cold and hot air interchanger of ground cockpit | |
| CN205316736U (en) | Multiaxis manned vehicle | |
| CN206544444U (en) | For the conditioner of vehicle and the vehicle with it | |
| CN202521760U (en) | Air-conditioning device suspended on bucket of bucket arm truck | |
| CN202324712U (en) | Energy-saving base station machine room without air conditioners | |
| CN204885367U (en) | Electronic public transit vehicle battery box constant temperature system | |
| CN203246285U (en) | Refrigeration cooling system for automobile | |
| CN206648179U (en) | Energy-saving communication base station computer room | |
| CN201957385U (en) | Directly ventilated and heat-dissipated outdoor equipment cabinet | |
| CN203637561U (en) | Air-inlet cabin door cooling and waterproofing structure of new-energy bus | |
| CN106723773A (en) | A kind of parasols based on semiconductor chilling plate | |
| CN205358385U (en) | Intelligence air conditioner safety helmet | |
| CN104051814A (en) | Nickel-hydrogen battery pack box body heat radiating structure of pure-electric bus | |
| CN209449143U (en) | A kind of great-power electromagnetic heating control cabinet | |
| CN206254939U (en) | A kind of electric motor car air cooling system | |
| CN208075436U (en) | A kind of wolfram steel knife production radiator | |
| CN206690872U (en) | A kind of engine cabin of passenger car radiation ventilator | |
| CN201703228U (en) | Heat pipe radiating electronic air conditioner for cab | |
| CN214189450U (en) | Unmanned vehicle heat preservation refrigerating plant based on solar energy | |
| CN209605348U (en) | JDJN-MC2 series central air conditioner cooling water energy-saving control cabinet | |
| CN205185848U (en) | New energy automobile cooling device | |
| CN203413754U (en) | Air conditioner without compressor |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |