CN207773487U - A kind of general-purpose aircraft air-conditioning system that temperature self-adaptation is adjusted - Google Patents
A kind of general-purpose aircraft air-conditioning system that temperature self-adaptation is adjusted Download PDFInfo
- Publication number
- CN207773487U CN207773487U CN201820017208.8U CN201820017208U CN207773487U CN 207773487 U CN207773487 U CN 207773487U CN 201820017208 U CN201820017208 U CN 201820017208U CN 207773487 U CN207773487 U CN 207773487U
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- module
- temperature
- adjusted
- power switching
- conditioning system
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- 238000004378 air conditioning Methods 0.000 title claims abstract description 27
- 230000036413 temperature sense Effects 0.000 claims abstract description 18
- 230000036039 immunity Effects 0.000 claims abstract description 5
- 238000005057 refrigeration Methods 0.000 claims description 23
- 238000010438 heat treatment Methods 0.000 claims description 19
- 238000012544 monitoring process Methods 0.000 claims description 7
- 230000000087 stabilizing effect Effects 0.000 claims description 6
- 230000001939 inductive effect Effects 0.000 claims description 5
- 230000005611 electricity Effects 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 claims 1
- 230000001105 regulatory effect Effects 0.000 abstract 1
- 238000000465 moulding Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000003749 cleanliness Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Air Humidification (AREA)
- Air Conditioning Control Device (AREA)
Abstract
The utility model discloses the general-purpose aircraft air-conditioning systems that a kind of temperature self-adaptation is adjusted; including power switching module; the upper end of the power switching module is equipped with overload protection module; and the side of power switching module is equipped with power module; the other side of the power switching module is equipped with temperature sense module; and the inside inner surface of temperature sense module is equipped with signal receiving module; the side of the signal receiving module is equipped with signal emission module, is equipped with immunity module between the signal receiving module and signal emission module at its top position.The general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation described in the utility model is adjusted, equipped with temperature sense module, humidification module and timing module, the temperature in aircraft can be voluntarily adjusted according to temperature conditions in aircraft, and it can be to being humidified in aircraft, voluntarily start regulating system according to humiture situation, electric energy is saved, is suitable for different operating situation, brings better prospect of the application.
Description
Technical field
The utility model is related to air-conditioning system field, more particularly to a kind of general-purpose aircraft air-conditioning system of temperature self-adaptation adjusting
System.
Background technology
Air-conditioning system is a kind of temperature, system of cleanliness factor and air velocity handling room air with artificial method,
Air-conditioning system application range is very extensive, can be used for the places such as aircraft, automobile and interior；Existing air-conditioning system is when in use
There are certain drawbacks, air-conditioning system can not carry out automatic adjusument, and to the humidification journey of air in temperature adjustment process
Degree can not voluntarily control run time than relatively limited in addition, and certain adverse effect is brought to actual use, for this purpose, I
Propose the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation is adjusted.
Utility model content
The main purpose of the utility model is to provide the general-purpose aircraft air-conditioning systems that a kind of temperature self-adaptation is adjusted, can be with
Effectively solve the problems in background technology.
To achieve the above object, the technical solution that the utility model is taken is：
A kind of general-purpose aircraft air-conditioning system that temperature self-adaptation is adjusted, including power switching module, the power switch mould
The upper end of block is equipped with overload protection module, and the side of power switching module is equipped with power module, the power switching module
The other side is equipped with temperature sense module, and the inside inner surface of temperature sense module is equipped with signal receiving module, and the signal connects
The side for receiving module is equipped with signal emission module, close to its top position between the signal receiving module and signal emission module
Place is equipped with immunity module, and the other side of the signal receiving module is equipped with temperature switch module, and under signal receiving module
Side is equipped with temperature monitoring module, and the lower section of the temperature monitoring module is equipped with temperature display module, the power switching module
Lower section is equipped with humidification module, and the inside inner surface of humidification module is equipped with humidification switch module, described to humidify the upper of switch module
Top is equipped with humidity inductive module, and the side of the humidification module is equipped with timing module, and the inside inner surface of timing module is set
There is timing module, the lower section of the timing module is equipped with time control module, and the top of timing module is equipped with time switch mould
Block is equipped with refrigeration module at another side position of the side far from power switching module of the temperature sense module, and the mould that freezes
The lower section of block is equipped with heating module, and wind direction control is equipped at a side position of the side far from temperature sense module of the refrigeration module
Molding block.
Preferably, the power switching module is internally provided with leakage protection module and Voltage stabilizing module, leakage protection module
It is electrically connected with power switching module with Voltage stabilizing module.
Preferably, the power module is internally provided with earthing module, and power module is alternating current.
Preferably, the wind direction control module is internally provided with power plant module and wind-force adjustment module, power plant module it is defeated
The input terminal of outlet and wind-force adjustment module is electrically connected.
Preferably, the lower section of the humidification switch module is equipped with humidity control module, and humidity control module includes humidity
Display module.
Preferably, the refrigeration module is placed in parallel with heating module, and is equipped with inside refrigeration module and heating module
Frequency-variable module.
Compared with prior art, the utility model has the advantages that：
In the utility model, by the temperature sense module of setting, the temperature conditions in aircraft can be incuded, and according to temperature
Degree situation voluntarily starts refrigeration module and heating module, to realize the automatic adjusument of system, by the humidification module of setting,
The air in aircraft can be humidified simultaneously during temperature is adjusted, avoid air-conditioning system at runtime to passenger
The discomfort brought can control the working time of humidification module, refrigeration module and heating module by the timing module of setting,
When temperature and humidity tend towards stability, humidification module, refrigeration module and heating module can be controlled by time switch module and closed
It closes, when there is temperature with humidity variation, timing module controls the startup of humidification module, refrigeration module and heating module, energy again
Enough save electric energy.
Description of the drawings
Fig. 1 is the overall structure diagram for the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation of the utility model is adjusted.
Fig. 2 is the temperature sense inside modules for the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation of the utility model is adjusted
Structure chart.
Fig. 3 is the humidification module internal structure for the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation of the utility model is adjusted
Figure.
Fig. 4 is the timing module internal structure for the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation of the utility model is adjusted
Figure.
In figure：1, power switching module；2, overload protection module；3, power module；4, temperature sense module；5, signal connects
Receive module；6, signal emission module；7, immunity module；8, temperature switch module；9, temperature monitoring module；10, temperature display
Module；11, humidification module；12, switch module is humidified；13, humidity inductive module；14, humidity control module；15, timing module；
16, timing module；17, time control module；18, time switch module；19, refrigeration module；20, heating module；21, wind direction control
Molding block.
Specific implementation mode
To make the technical means, creative features, achievement of purpose, and effectiveness of the utility model be easy to understand, below
In conjunction with specific implementation mode, the utility model is expanded on further.
As shown in Figs 1-4, the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation is adjusted, including power switching module 1, electricity
The upper end of source switch module 1 is equipped with overload protection module 2, and the side of power switching module 1 is equipped with power module 3, and power supply is opened
The other side for closing module 1 is equipped with temperature sense module 4, and the inside inner surface of temperature sense module 4 is equipped with signal receiving module
5, the side of signal receiving module 5 is equipped with signal emission module 6, close to it between signal receiving module 5 and signal emission module 6
Immunity module 7 is equipped at top position, the other side of signal receiving module 5 is equipped with temperature switch module 8, and signal receives mould
The lower section of block 5 is equipped with temperature monitoring module 9, and the lower section of temperature monitoring module 9 is equipped with temperature display module 10, power switching module
10 lower section is equipped with humidification module 11, and the inside inner surface of humidification module 11 is equipped with humidification switch module 12, humidifies switching molding
The top of block 12 is equipped with humidity inductive module 13, and the side of humidification module 11 is equipped with timing module 15, and timing module 15
Internal inner surface is equipped with timing module 16, and the lower section of timing module 16 is equipped with time control module 17, and timing module 16 is upper
Side is equipped with time switch module 18, and system is equipped at another side position of the side far from power switching module 1 of temperature sense module 4
Chill block 19, and the lower section of refrigeration module 19 is equipped with heating module 20, the side of refrigeration module 19 is far from temperature sense module 4
Wind direction control module 21 is equipped at one side position.
Power switching module 1 is internally provided with leakage protection module and Voltage stabilizing module, leakage protection module and Voltage stabilizing module
It is electrically connected with power switching module 1；Power module 3 is internally provided with earthing module, and power module 3 is alternating current；Wind
It is internally provided with power plant module and wind-force adjustment module, output end and the wind-force adjustment module of power plant module to control module 21
Input terminal is electrically connected；The lower section for humidifying switch module 12 is equipped with humidity control module 14, and humidity control module 14 includes wet
Spend display module；Refrigeration module 19 is placed in parallel with heating module 2, and is equipped with change inside refrigeration module 19 and heating module 2
Frequency module.
It should be noted that the utility model is the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation is adjusted, using
When, power module 3 is powered to air-conditioning system, the switch of power supply is controlled by switch module 1, overload protection module 2 can be in electricity
Circuit is cut off when flowing voltage overload in time, protects system, during system works, degree induction module 4 can be to the temperature in aircraft
Degree is incuded, when temperature drift or it is relatively low when, temperature switch module 8 can be passed through and touch refrigeration module 19 and heating module
20, when temperature is relatively low, heating module 20 starts, so as to make the temperature in aircraft increase, refrigeration module 19 when temperature drift
Start, so as to make the temperature in aircraft reduce, temperature adjust during, wind direction control module 21 can control cold wind with
The wind direction of hot wind, meanwhile, the humidity inductive module 13 in humidification module 11 can incude air humidity, when humidity is relatively low, start
Switch module 12 is humidified, at the same time humidity control module 14 can in real time be monitored humidity variation, pass through timing module
15, can control humidification module 11, refrigeration module 19 and heating module 20 working time, when temperature and humidity tend towards stability
When, humidification module 11 can be controlled by time switch module 18, refrigeration module 19 and heating module 20 are closed, occur temperature with
When humidity changes, timing module 15 controls the startup of humidification module 11, refrigeration module 19 and heating module 20 again, can save
Electric energy is more practical.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above.One's own profession
The technical staff of industry is it should be appreciated that the present utility model is not limited to the above embodiments, described in above embodiments and description
Only illustrate the principles of the present invention, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
It will have various changes and improvements, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (6)
1. the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation is adjusted, including power switching module (1), it is characterised in that：Institute
The upper end for stating power switching module (1) is equipped with overload protection module (2), and the side of power switching module (1) is equipped with power supply mould
The other side of block (3), the power switching module (1) is equipped with temperature sense module (4), and the inside of temperature sense module (4)
Inner surface is equipped with signal receiving module (5), and the side of the signal receiving module (5) is equipped with signal emission module (6), the letter
Immunity module (7), the signal are equipped with number between receiving module (5) and signal emission module (6) at its top position
The other side of receiving module (5) is equipped with temperature switch module (8), and the lower section of signal receiving module (5) is equipped with monitoring temperature mould
The lower section of block (9), the temperature monitoring module (9) is equipped with temperature display module (10), the lower section of the power switching module (1)
Equipped with humidification module (11), and the inside inner surface of humidification module (11) is equipped with humidification switch module (12), the humidification switch
The top of module (12) is equipped with humidity inductive module (13), and the side of the humidification module (11) is equipped with timing module (15),
And the inside inner surface of timing module (15) is equipped with timing module (16), the lower section of the timing module (16) is equipped with time control
Module (17), and the top of timing module (16) is equipped with time switch module (18), the side of the temperature sense module (4) is remote
Refrigeration module (19) is equipped at another side position from power switching module (1), and the lower section of refrigeration module (19) is equipped with heating
Module (20), the side of the refrigeration module (19) control mould far from being equipped with wind direction at a side position of temperature sense module (4)
Block (21).
2. the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation according to claim 1 is adjusted, it is characterised in that：It is described
Power switching module (1) is internally provided with leakage protection module and Voltage stabilizing module, leakage protection module and Voltage stabilizing module with electricity
Source switch module (1) is electrically connected.
3. the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation according to claim 1 is adjusted, it is characterised in that：It is described
Power module (3) is internally provided with earthing module, and power module (3) is alternating current.
4. the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation according to claim 1 is adjusted, it is characterised in that：It is described
Wind direction control module (21) is internally provided with power plant module and wind-force adjustment module, and output end and the wind-force of power plant module adjust mould
The input terminal of block is electrically connected.
5. the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation according to claim 1 is adjusted, it is characterised in that：It is described
The lower section for humidifying switch module (12) is equipped with humidity control module (14), and humidity control module (14) includes humidity display mould
Block.
6. the general-purpose aircraft air-conditioning system that a kind of temperature self-adaptation according to claim 1 is adjusted, it is characterised in that：It is described
Refrigeration module (19) is placed in parallel with heating module (20), and is equipped with frequency conversion inside refrigeration module (19) and heating module (20)
Module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820017208.8U CN207773487U (en) | 2018-01-05 | 2018-01-05 | A kind of general-purpose aircraft air-conditioning system that temperature self-adaptation is adjusted |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820017208.8U CN207773487U (en) | 2018-01-05 | 2018-01-05 | A kind of general-purpose aircraft air-conditioning system that temperature self-adaptation is adjusted |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207773487U true CN207773487U (en) | 2018-08-28 |
Family
ID=63222536
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820017208.8U Active CN207773487U (en) | 2018-01-05 | 2018-01-05 | A kind of general-purpose aircraft air-conditioning system that temperature self-adaptation is adjusted |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207773487U (en) |
-
2018
- 2018-01-05 CN CN201820017208.8U patent/CN207773487U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PP01 | Preservation of patent right | ||
| PP01 | Preservation of patent right |
Effective date of registration: 20240624 Granted publication date: 20180828 |
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| PD01 | Discharge of preservation of patent | ||
| PD01 | Discharge of preservation of patent |
Date of cancellation: 20240805 Granted publication date: 20180828 |