CN207443168U - Airfield aid light temperature controls automatic protective system - Google Patents
Airfield aid light temperature controls automatic protective system Download PDFInfo
- Publication number
- CN207443168U CN207443168U CN201720315370.3U CN201720315370U CN207443168U CN 207443168 U CN207443168 U CN 207443168U CN 201720315370 U CN201720315370 U CN 201720315370U CN 207443168 U CN207443168 U CN 207443168U
- Authority
- CN
- China
- Prior art keywords
- temperature
- wick
- signal
- aid light
- airfield aid
- 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
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
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B20/00—Energy efficient lighting technologies, e.g. halogen lamps or gas discharge lamps
- Y02B20/30—Semiconductor lamps, e.g. solid state lamps [SSL] light emitting diodes [LED] or organic LED [OLED]
Landscapes
- Arrangement Of Elements, Cooling, Sealing, Or The Like Of Lighting Devices (AREA)
Abstract
The utility model provides a kind of airfield aid light temperature control automatic protective system; temperature sensor module, master board including circuit connection; automatic protection circuit; the temperature sensor module is used to sense the temperature of airfield aid light wick; temperature signal is converted into analog signal output; master board is used to receive the temperature signal that temperature sensor transmits; it sends cut-out or opens the signal of wick power supply, automatic protection circuit receives signal wick to be protected not burn out lamp bead because of overheat.Implement the technical solution of the utility model, can break down to avoid navigational lighting aid when causing the LED lamp to be always on temperature excessively high the phenomenon that burning out lamp body, whole system is more safe and reliable, the service life more lengthens.
Description
Technical field
The utility model is applied to airport field, especially airfield aid light temperature control automatic protective system.
Background technology
Airfield aid light on the market is usually controlled without temperature protection at present, the usual working environment of airfield aid light
Compare badly, it is largely to be operated in height in the air, also some are mounted on airfield runway, big on runway indoors to be not
Underground is partly embedded into, is exposed to the weather in outdoor severe outdoor environment, so light integrally needs to do sealed waterproof effect
It is very good, but so also bring drawback to lamp body, the shine heat of generation of lamp source does not allow easy heat radiation, and work long hours meeting
Thermal accumlation is easily generated into bigger influence to the service life of lamp source together, in addition, most of light is according to certain
Frequency is flashed, and light can be caused to be always on when such light generally occurs within failure, and many heats will be generated by being always on, this
Lamp source may be burnt out or even burn entire lamps and lanterns by a little heats within one or two minutes, seriously can fire hazard.
The content of the invention
More than in view of, it is necessary to a kind of airfield aid light temperature control automatic protective system be provided, make airfield aid
Light can automatically cut off wick power supply when lamp source temperature is excessively high, automatically turn on wick power supply when the temperature will return back to normal,
Function above is all achieved by the following technical solution:
Airfield aid light temperature controls automatic protective system, temperature sensor module, main control including circuit connection
Plate, automatic protection circuit, the temperature sensor module are used to sense the temperature of airfield aid light wick, temperature signal conversion
Into analog signal output, master board sends cut-out or unlatching wick for receiving the temperature signal that temperature sensor transmits
The signal of power supply, automatic protection circuit receive signal wick to be protected not burn out lamp bead because of overheat.
The master board carries out processing analysis for receiving the analog signal that temperature sensor transmits.
The signal cut or open wick power supply that the automatic protection circuit is sent by master control borad, when temperature mistake
It cuts off the power when high, temperature is powered back up source to wick when returning normal, has achieved the purpose that protect lamp bead.
There is no temperature control protection on traditional technology, be easily damaged lamp source, implement the technical solution of the utility model, it can be automatic
Temperature detection is carried out to airfield aid light, automatically cuts off wick power supply when the temperature is excessively high, achievees the purpose that protect lamp source, make
Obtain light longer life expectancy.
Description of the drawings
Fig. 1 is the functional block diagram cut-away view of airfield aid light temperature control automatic protective system.
Specific embodiment
The embodiment of the utility model is described in detail below in conjunction with attached drawing, but the utility model can be by right
It is required that the multitude of different ways for limiting and covering is implemented.
As shown in Figure 1, Fig. 1 is the cut-away view of the utility model airfield aid light temperature control automatic protective system
Airfield aid light temperature controls automatic protective system by temperature sensor module, master board, automatic protection circuit composition, root
According to the signal break-make of master board, temperature sensor is mounted on the radiator of lamp source, can real-time monitor the temperature of wick
Degree, and temperature signal is converted into analog signal output, master board receives the analog signal from temperature sensor, and carries out
Processing, controls the power supply of LED lamp after the completion of processing, the power supply of cut-out LED lamp is waited when the temperature is excessively high, after cut-out
Temperature will be gradually reduced, and when falling to a certain temperature instantly, master controller reopens LED lamp power supply, be achieved in that pair
The function of airfield aid light automatic protection.LED lamp continuous firing under high-temperature situation can greatly shorten lamp life, because
This, when the temperature is excessively high, the working time of LED lamp under the condition of high temperature can effectively be reduced by cutting off the power, and can improve the use of lamps and lanterns
Service life.
It these are only the preferred embodiment of the utility model, be not intended to limit the utility model, for this field
Technical staff for, various modifications and changes may be made to the present invention.Within the spirit and principle of the utility model,
Any modifications, equivalent replacements and improvements are made should be included within the scope of protection of this utility model.
Claims (4)
1. airfield aid light temperature controls automatic protective system, temperature sensor module, master board including circuit connection,
Automatic protection circuit, the temperature sensor module are used to sense the temperature of airfield aid light wick, and temperature signal is converted into
Analog signal output, master board send cut-out or unlatching wick electricity for receiving the temperature signal that temperature sensor transmits
The signal in source, automatic protection circuit receive signal wick to be protected not burn out lamp bead because of overheat.
2. airfield aid light temperature according to claim 1 controls automatic protective system, which is characterized in that the temperature
Sensor assembly is used to sense the temperature of airfield aid light wick, and temperature signal is converted into analog signal output.
3. airfield aid light temperature according to claim 2 controls automatic protective system, which is characterized in that master board
For receiving the analog signal that temperature sensor transmits, for carrying out processing analysis to analog signal.
4. airfield aid light temperature according to claim 1 controls automatic protective system, which is characterized in that it is described from
The signal cut or open wick power supply that dynamic protection circuit is sent by master control borad, cut off the power when the temperature is excessively high, temperature
Degree is powered back up source to wick when returning normal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720315370.3U CN207443168U (en) | 2017-03-29 | 2017-03-29 | Airfield aid light temperature controls automatic protective system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720315370.3U CN207443168U (en) | 2017-03-29 | 2017-03-29 | Airfield aid light temperature controls automatic protective system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207443168U true CN207443168U (en) | 2018-06-01 |
Family
ID=62394576
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720315370.3U Active CN207443168U (en) | 2017-03-29 | 2017-03-29 | Airfield aid light temperature controls automatic protective system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207443168U (en) |
-
2017
- 2017-03-29 CN CN201720315370.3U patent/CN207443168U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103527978B (en) | A kind of induction LED lamp | |
| TW201342998A (en) | Lamp remote control system | |
| WO2009046615A1 (en) | Light fixture | |
| CN202209661U (en) | High-power LED lighting fixture temperature control system | |
| CN207443168U (en) | Airfield aid light temperature controls automatic protective system | |
| CN104696811A (en) | Street lamp | |
| CN102022677A (en) | LED (Light Emitting Diode) street lamp | |
| CN201256463Y (en) | LED lamp having landscape lighting function | |
| CN202634788U (en) | Emergency evacuation lighting system based on Internet of things | |
| CN206018343U (en) | A kind of LED illumination device with radiator fan | |
| CN204201509U (en) | A kind of LED projector lamp | |
| CN110397869B (en) | Stage lamp control system and control method capable of protecting security of illuminated object | |
| CN202494000U (en) | Automatic overheat protection LED (Light-Emitting Diode) lamp | |
| FI12223U1 (en) | Lamp | |
| CN201892136U (en) | Light-emitting diode (LED) bulb with escape indication | |
| CN206055246U (en) | A kind of bulkhead lamp | |
| CN201061582Y (en) | Common electric welding mask | |
| CN203656860U (en) | Intelligent LED (Light-emitting Diode) light source temperature control device | |
| CN202747191U (en) | High-power LED (light-emitting diode) colored crystal chandelier with radiating medium LED bulb | |
| CN203273554U (en) | LED lamp used at tail end of airport runway | |
| CN219499600U (en) | Public lighting control circuit beneficial to energy conservation | |
| CN212207717U (en) | Special equipment tail flame simulation device capable of remotely adjusting brightness | |
| CN202546406U (en) | Light-emitting diode (LED) lamp with human body induction device | |
| CN209262784U (en) | A kind of intelligence bulkhead lamp | |
| CN205424598U (en) | Adopt radiating shot -light of smart fan |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |