CN201152482Y - Aviation red aeroplane fueling lamp - Google Patents
Aviation red aeroplane fueling lamp Download PDFInfo
- Publication number
- CN201152482Y CN201152482Y CNU2007201297612U CN200720129761U CN201152482Y CN 201152482 Y CN201152482 Y CN 201152482Y CN U2007201297612 U CNU2007201297612 U CN U2007201297612U CN 200720129761 U CN200720129761 U CN 200720129761U CN 201152482 Y CN201152482 Y CN 201152482Y
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- China
- Prior art keywords
- lamp
- aviation
- red
- led module
- driving power
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- Expired - Fee Related
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Abstract
The utility model discloses an oil adding lamp for an aerial red airplane, which comprises a screen and an outer casing, and the oil adding lamp is characterized in that an LED module connected with at least two LEDs capable of emitting aerial red light in series and connected with a driving power source is positioned at the bottom part at the inner side of the outer casing. Because the LED module can emit the aerial red light, the accurate positioning of an operator is advantageous. Constant current is provided by the driving power source, so that not only the brightness of the LED maintains a constant and invariable value, but also the service life can be prolonged.
Description
Technical field
The utility model relates to illuminating device, specifically relates to the red aircraft refuelling lamp of a kind of aviation.
Background technology
At present, traditional aircraft refuelling lamp all adopts incandescent lamp, so the white light that the color relation of light is a filament itself to be sent (yellow partially).When aloft refueling, this white light causes that not too easily the operator notes and accurately locatees.
The utility model content
Technical problem to be solved in the utility model is, the deficiency at the aircraft refuelling lamp of prior art provides a kind of operator of making the aircraft refuelling lamp of identification easily.
For solving the problems of the technologies described above, the technical solution of the utility model is, the red aircraft refuelling lamp of a kind of aviation comprises screen, shell, it is characterized in that: the bottom that is positioned at described shell inboard is provided with the led module that is connected with driving power at least and can only sends aviation red-light LED serial connection by two.
The red aircraft refuelling lamp of a kind of aviation, the bottom of described shell inboard are provided with led module by from outer casing bottom extracting power supply cord and driving power and connect.
The red aircraft refuelling lamp of a kind of aviation, described screen adopts transparent glass screen.
Be connected by press seal between the red aircraft refuelling lamp of a kind of aviation, described screen and shell.
The red aircraft refuelling lamp of a kind of aviation, described driving power can provide constant electric current with the driving LED module.
The red aircraft refuelling lamp of a kind of aviation adopts said structure, and the bottom that is positioned at described shell inboard is provided with driving power and is connected at least by the led module that can send aviation red-light LED serial connection more than two.Because led module can send aviation ruddiness, helps operator's accurate location.Driving power provides constant electric current, and it is constant not only to make LED brightness remain on a certain steady state value, and can improve service life.
Description of drawings
Below in conjunction with the drawings and specific embodiments the utility model is described in further detail;
Fig. 1 is the red aircraft refuelling modulated structure of a kind of aviation of a utility model schematic diagram;
Fig. 2 is the red aircraft refuelling lamp power circuit of a kind of aviation of a utility model structural representation;
In Fig. 1～Fig. 2,1, the screen; 2, shell; 3, led module; 4, driving power.
The specific embodiment
As shown in Figure 1 and Figure 2, the red aircraft refuelling lamp of a kind of aviation comprises screen 1, shell 2, led module 3, driving power 4, and described screen 1 and shell 2 press seals are together.Led module 3 can only send the aviation red-light LED by two at least and compose in series, and the bottom of described shell 2 inboards is provided with led module 3 by from outer casing bottom extracting power supply cord and driving power 4 and connect.Screen 1 adopts transparent glass screen.Because led module 3 can send aviation ruddiness, helps operator's accurate location.The input power supply provides constant electric current by driving power 4 to led module 3, and it is constant not only to make LED brightness remain on a certain steady state value, and can improve service life.
Claims (5)
1, the red aircraft refuelling lamp of a kind of aviation, comprise screen (1), shell (2), it is characterized in that: be positioned at: the inboard bottom of described shell (2) is provided with the led module (3) that is connected with driving power (4) by the LED serial connection that can send aviation ruddiness more than two at least.
2, the red aircraft refuelling lamp of a kind of aviation according to claim 1 is characterized in that: the inboard bottom of described shell (2) is provided with led module (3) by from outer casing bottom extracting power supply cord and driving power (4) and connect.
3, the red aircraft refuelling lamp of a kind of aviation according to claim 1 is characterized in that: described screen (1) adopts transparent glass screen.
4, the red aircraft refuelling lamp of a kind of aviation according to claim 1 is characterized in that: be connected by press seal between described screen (1) and the shell (2).
5, the red aircraft refuelling lamp of a kind of aviation according to claim 1 and 2 is characterized in that: described driving power (4) can provide constant electric current with driving LED module (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007201297612U CN201152482Y (en) | 2007-12-28 | 2007-12-28 | Aviation red aeroplane fueling lamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007201297612U CN201152482Y (en) | 2007-12-28 | 2007-12-28 | Aviation red aeroplane fueling lamp |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201152482Y true CN201152482Y (en) | 2008-11-19 |
Family
ID=40128160
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007201297612U Expired - Fee Related CN201152482Y (en) | 2007-12-28 | 2007-12-28 | Aviation red aeroplane fueling lamp |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201152482Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103032796A (en) * | 2012-12-11 | 2013-04-10 | 安徽华东光电技术研究所 | Aircraft refueling lamp and processing method thereof |
-
2007
- 2007-12-28 CN CNU2007201297612U patent/CN201152482Y/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103032796A (en) * | 2012-12-11 | 2013-04-10 | 安徽华东光电技术研究所 | Aircraft refueling lamp and processing method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20081119 Termination date: 20131228 |