CN201081159Y - Aircraft fueling lamp - Google Patents
Aircraft fueling lamp Download PDFInfo
- Publication number
- CN201081159Y CN201081159Y CNU2007200430715U CN200720043071U CN201081159Y CN 201081159 Y CN201081159 Y CN 201081159Y CN U2007200430715 U CNU2007200430715 U CN U2007200430715U CN 200720043071 U CN200720043071 U CN 200720043071U CN 201081159 Y CN201081159 Y CN 201081159Y
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- CN
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- Prior art keywords
- glass
- lamp
- aircraft
- glass panel
- saucer
- 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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Abstract
The utility model discloses an aircraft fueling lamp which comprises a glass envelope, a lamp wick and a contact piece connected to a glass panel. The utility model is characterized in that the glass panel is a special shaped avail red glass panel which has unequal heights of the two ends but matches the aircraft configuration, the bottom of the outer side of the glass envelope is provided with a small saucer connected to the lamp wick, the contact piece is welded on the small saucer and is connected to the power cord. In the structure, as the glass panel adopts avail red glass, the color of the emitting light is aviation red, and precise positioning can be achieved by operators easily. The inside surface of the glass panel is grid-shaped which contributes to the improvement of the scattering angles of light and thus enlarges the illuminating areas. The glass panel adopts special shaped panel which matches the aircraft configuration, and thus is advantageous to improve the aerodynamic performance of aircraft. Meanwhile, the friction force between the fueling lamp and air in flying is reduced and the use environment of fueling lamp is improved and the service life is also improved.
Description
Technical field
The utility model relates to illuminating device, specifically relates to a kind of aircraft refuelling lamp.
Background technology
At present, traditional aircraft refuelling lamp all adopts transparent sphere screen.Owing to adopt transparent screen, 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.In addition, adopt the sphere screen not exclusively to mate, in the aircraft high-speed flight, influence the aeroperformance of aircraft with the airframe appearance curved surface.
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 identification of being convenient to, and the aircraft refuelling lamp that is complementary with the fuselage appearance curved surface.
For solving the problems of the technologies described above, the technical solution of the utility model is: a kind of aircraft refuelling lamp, comprise the glass awl, wick, the contact chip that are connected with the glass screen, it is characterized in that: described glass screen does not wait the special-shaped aviation red glass face screen that is complementary with the airframe profile for the two ends height, the bottom that is positioned at the glass awl outside is provided with the saucer that is connected with wick, and contact chip is welded on the saucer and is connected with power line.The glass screen adopts the aviation red colored glasses, and making the light color that sends is that aviation is red.The glass screen adopts the Special-Shaped Surface screen, is complementary with the airframe profile, helps improving the aeroperformance of aircraft.
A kind of aircraft refuelling lamp, the inner surface of described glass screen are provided with and improve scattering of light angle fenestral fabric., help improving the scattering of light angle, improved and added the oil lamp identifiability.
A kind of aircraft refuelling lamp, described glass screen is connected by sealing by fusing with the glass awl.
A kind of aircraft refuelling lamp, described wick place glass awl inside and saucer by being welded to connect.
A kind of aircraft refuelling lamp adopts said structure, because the glass screen adopts the aviation red glass, making the light color that sends is that aviation is red, helps operator's accurate location.The inner surface of glass screen is latticed, helps improving the scattering of light angle, thereby strengthens the field of illumination.Glass screen adopts the antarafacial screen, is complementary with the airframe profile, favourable and the aeroperformance that improves aircraft.Also reduce simultaneously the frictional force of flight refueling lamp and air, improve the environment for use that adds oil lamp, 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 a kind of aircraft refuelling modulated structure of the utility model schematic diagram;
In Fig. 1,1, glass screen; 2, glass awl; 3, wick; 4, saucer; 5, contact chip.
The specific embodiment
As shown in Figure 1, a kind of aircraft refuelling lamp comprises glass screen 1, glass awl 2, wick 3, saucer 4, contact chip 5, is positioned at described glass and bores 2 outer bottoms and be provided with the saucer 4 that is connected with external power source.Contact chip 5 is welded on and is used for connecting power line on the saucer 4.Wick 3 places glass awl 2 inside to weld together with saucer 4.Glass screen 1 adopts the aviation red glass, and making the light color that sends is that aviation is red.The accurate location that helps the operator.The inner surface of glass screen 1 is latticed, helps improving the scattering of light angle.Enlarge the field of illumination.The antarafacial screen that glass screen 1 is complementary with the airframe profile for the two ends height does not wait, the aeroperformance of favourable and raising aircraft.
Claims (4)
1. aircraft refuelling lamp, comprise glass awl (2), the wick (3), the contact chip (5) that are connected with glass screen (1), it is characterized in that: the special-shaped aviation red glass face that is complementary with the airframe profile that described glass screen (1) does not wait for the two ends height shields, the bottom that is positioned at glass awl (2) outside is provided with the saucer (4) that is connected with wick (3), and contact chip (5) is welded on saucer (4) and upward is connected with power line.
2. a kind of aircraft refuelling lamp according to claim 1 is characterized in that: the inner surface of described glass screen (1) is provided with and improves scattering of light angle fenestral fabric.
3. a kind of aircraft refuelling lamp according to claim 1 is characterized in that: described glass screen (1) is connected by sealing by fusing with glass awl (2).
4. a kind of aircraft refuelling lamp according to claim 1 is characterized in that: described wick (3) places glass awl (2) inside and saucer (4) by being welded to connect.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200430715U CN201081159Y (en) | 2007-08-03 | 2007-08-03 | Aircraft fueling lamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200430715U CN201081159Y (en) | 2007-08-03 | 2007-08-03 | Aircraft fueling lamp |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201081159Y true CN201081159Y (en) | 2008-07-02 |
Family
ID=39614831
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007200430715U Expired - Fee Related CN201081159Y (en) | 2007-08-03 | 2007-08-03 | Aircraft fueling lamp |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201081159Y (en) |
Cited By (2)
| 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 |
| CN108928495A (en) * | 2018-07-13 | 2018-12-04 | 安徽华夏显示技术股份有限公司 | A kind of profiling aircraft positive camber type oiling lamp and preparation method thereof |
-
2007
- 2007-08-03 CN CNU2007200430715U patent/CN201081159Y/en not_active Expired - Fee Related
Cited By (2)
| 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 |
| CN108928495A (en) * | 2018-07-13 | 2018-12-04 | 安徽华夏显示技术股份有限公司 | A kind of profiling aircraft positive camber type oiling lamp and preparation 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: 20080702 Termination date: 20130803 |