CN203551825U - Aviation tail gas detection optical filter with central wavelength of 2700 nm - Google Patents
Aviation tail gas detection optical filter with central wavelength of 2700 nm Download PDFInfo
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- CN203551825U CN203551825U CN201320777866.4U CN201320777866U CN203551825U CN 203551825 U CN203551825 U CN 203551825U CN 201320777866 U CN201320777866 U CN 201320777866U CN 203551825 U CN203551825 U CN 203551825U
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Abstract
The utility model provides an aviation tail gas detection optical filter with a central wavelength of 2700 nm which has high test precision and can greatly raise a signal to noise ratio. The aviation tail gas detection optical filter comprises a substrate with G e as a raw material, a first coating layer of G e and S i O and a second coating layer of G e and S i O; the substrate is located between the first coating layer and the second coating layer. The aviation tail gas detection optical filter has a central wavelength of 2700 nm +/- 5 nm, and can substantially raise the signal to noise ratio and test precision in an aviation tail gas detection process. The peak value transmittance Tp of the optical filter is no less than 80%, the bandwidth is 200 +/- 20 nm, 1000-3500 nm (except passband ), and Tavg is smaller than 0.5%.
Description
Technical field
The utility model relates to aviation tail gas gas and detects optical filter, and the aviation tail gas gas of especially a kind of centre wavelength 2700nm detects optical filter.
Background technology
Infrared fileter filters, cut-off visible ray allows to pass through infrared ray simultaneously.Ultrared wavelength penetrates any object easily, and namely infrared ray can not reflect when through object.Utilize ultrared this characteristic, only allow long wavelength's infrared ray pass through, filtering short wavelength's ultraviolet ray and visible ray.Be applied to a lot of fields, the problem existing for the optical filter using in aviation tail gas gas testing process is at present that the signal to noise ratio (S/N ratio) of transmitance and cut-off region is not high, can not meet high-precision measurement requirement.
Utility model content
The purpose of this utility model is the deficiency in order to solve above-mentioned technology and provide that a kind of measuring accuracy is high, the aviation tail gas gas of the centre wavelength 2700nm that can greatly improve signal to noise ratio (S/N ratio) detects optical filter.
In order to achieve the above object, the aviation tail gas gas of the designed centre wavelength 2700nm of the utility model detects optical filter, comprise take Ge as raw-material substrate, with Ge, SiO is the first filming layer and with Ge, SiO is the second film plating layer, and described substrate is between the first filming layer and the second film plating layer, described the first filming layer is arranged in order and includes from inside to outside: the Ge layer of 96nm thickness, the SiO layer of 304nm thickness, the Ge layer of 132nm thickness, the SiO layer of 159nm thickness, the Ge layer of 82nm thickness, the SiO layer of 338nm thickness, the Ge layer of 140nm thickness, the SiO layer of 339nm thickness, the Ge layer of 137nm thickness, the SiO layer of 349nm thickness, the Ge layer of 70nm thickness, the SiO layer of 169nm thickness, the Ge layer of 136nm thickness, the SiO layer of 343nm thickness, the Ge layer of 149nm thickness, the SiO layer of 473nm thickness, the Ge layer of 232nm thickness, the SiO layer of 668nm thickness, the Ge layer of 103nm thickness and the SiO layer of 226nm thickness, described the second film plating layer is arranged in order and includes from inside to outside: the Ge layer of the Ge layer of the Ge layer of the Ge layer of 178nm thickness, the SiO layer of 166nm thickness, 92nm thickness, the SiO layer of 222nm thickness, 102nm thickness, the SiO layer of 277nm thickness, 135nm thickness, SiO layer, the Ge layer of 55nm thickness and the SiO layer of 150nm thickness of 150nm thickness.
Thickness corresponding to above-mentioned each material, its permission changes in margin tolerance, and the scope of its variation belongs to the scope of this patent protection, is identity relation.Conventionally the tolerance of thickness is in 10nm left and right.
The aviation tail gas gas of the centre wavelength 2700nm that the utility model obtains detects optical filter, its centre wavelength 2700 ± 5nm, and it,, in aviation tail gas gas testing process, can improve signal to noise ratio (S/N ratio) greatly, improves accurate testing degree.Peak transmittance Tp >=80% of this optical filter, bandwidth=200 ± 20nm, 1000~3500nm(is except passband), Tavg<0.5%.
Accompanying drawing explanation
Fig. 1 is embodiment one-piece construction schematic diagram;
Fig. 2 is the infrared spectrum transmitance measured curve figure that embodiment provides.
Embodiment
Below by embodiment, the utility model will be further described by reference to the accompanying drawings.
Embodiment 1:
As Fig. 1, shown in Fig. 2, the aviation tail gas gas of the centre wavelength 2700nm that the present embodiment is described detects optical filter, comprise take Ge as raw-material substrate 2, with Ge, SiO is the first filming layer 1 and with Ge, SiO is the second film plating layer 3, and described substrate 2 is between the first filming layer 1 and the second film plating layer 3, described the first filming layer 1 is arranged in order and includes from inside to outside: the Ge layer of 96nm thickness, the SiO layer of 304nm thickness, the Ge layer of 132nm thickness, the SiO layer of 159nm thickness, the Ge layer of 82nm thickness, the SiO layer of 338nm thickness, the Ge layer of 140nm thickness, the SiO layer of 339nm thickness, the Ge layer of 137nm thickness, the SiO layer of 349nm thickness, the Ge layer of 70nm thickness, the SiO layer of 169nm thickness, the Ge layer of 136nm thickness, the SiO layer of 343nm thickness, the Ge layer of 149nm thickness, the SiO layer of 473nm thickness, the Ge layer of 232nm thickness, the SiO layer of 668nm thickness, the Ge layer of 103nm thickness and the SiO layer of 226nm thickness, described the second film plating layer 3 is arranged in order and includes from inside to outside: the Ge layer of the Ge layer of the Ge layer of the Ge layer of 178nm thickness, the SiO layer of 166nm thickness, 92nm thickness, the SiO layer of 222nm thickness, 102nm thickness, the SiO layer of 277nm thickness, 135nm thickness, SiO layer, the Ge layer of 55nm thickness and the SiO layer of 150nm thickness of 150nm thickness.
Claims (1)
1. the aviation tail gas gas of a centre wavelength 2700nm detects optical filter, comprise take Ge as raw-material substrate, with Ge, SiO is the first filming layer and with Ge, SiO is the second film plating layer, and described substrate is between the first filming layer and the second film plating layer, it is characterized in that: described the first filming layer is arranged in order and includes from inside to outside: the Ge layer of 96nm thickness, the SiO layer of 304nm thickness, the Ge layer of 132nm thickness, the SiO layer of 159nm thickness, the Ge layer of 82nm thickness, the SiO layer of 338nm thickness, the Ge layer of 140nm thickness, the SiO layer of 339nm thickness, the Ge layer of 137nm thickness, the SiO layer of 349nm thickness, the Ge layer of 70nm thickness, the SiO layer of 169nm thickness, the Ge layer of 136nm thickness, the SiO layer of 343nm thickness, the Ge layer of 149nm thickness, the SiO layer of 473nm thickness, the Ge layer of 232nm thickness, the SiO layer of 668nm thickness, the Ge layer of 103nm thickness and the SiO layer of 226nm thickness, described the second film plating layer is arranged in order and includes from inside to outside: the Ge layer of the Ge layer of the Ge layer of the Ge layer of 178nm thickness, the SiO layer of 166nm thickness, 92nm thickness, the SiO layer of 222nm thickness, 102nm thickness, the SiO layer of 277nm thickness, 135nm thickness, SiO layer, the Ge layer of 55nm thickness and the SiO layer of 150nm thickness of 150nm thickness.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201320777866.4U CN203551825U (en) | 2013-11-29 | 2013-11-29 | Aviation tail gas detection optical filter with central wavelength of 2700 nm |
Applications Claiming Priority (1)
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CN201320777866.4U CN203551825U (en) | 2013-11-29 | 2013-11-29 | Aviation tail gas detection optical filter with central wavelength of 2700 nm |
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CN203551825U true CN203551825U (en) | 2014-04-16 |
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CN201320777866.4U Withdrawn - After Issue CN203551825U (en) | 2013-11-29 | 2013-11-29 | Aviation tail gas detection optical filter with central wavelength of 2700 nm |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103713346A (en) * | 2013-11-29 | 2014-04-09 | 杭州麦乐克电子科技有限公司 | Aviation tail gas detection filter with central wavelength of 2700 nm |
CN106054300A (en) * | 2016-07-25 | 2016-10-26 | 江苏大学 | Dual channel infrared optical filter for CO2 gas detection and preparation method thereof |
-
2013
- 2013-11-29 CN CN201320777866.4U patent/CN203551825U/en not_active Withdrawn - After Issue
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103713346A (en) * | 2013-11-29 | 2014-04-09 | 杭州麦乐克电子科技有限公司 | Aviation tail gas detection filter with central wavelength of 2700 nm |
CN103713346B (en) * | 2013-11-29 | 2016-02-10 | 杭州麦乐克电子科技有限公司 | The aviation exhaust gas of centre wavelength 2700nm detects optical filter |
CN106054300A (en) * | 2016-07-25 | 2016-10-26 | 江苏大学 | Dual channel infrared optical filter for CO2 gas detection and preparation method thereof |
CN106054300B (en) * | 2016-07-25 | 2018-06-26 | 江苏大学 | A kind of CO2Gas detection binary channels infrared fileter and preparation method thereof |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
AV01 | Patent right actively abandoned |
Granted publication date: 20140416 Effective date of abandoning: 20160210 |
|
C25 | Abandonment of patent right or utility model to avoid double patenting |