CN211184367U - A normal position inspection device for aircraft formation lamp hidden mode operating condition - Google Patents
A normal position inspection device for aircraft formation lamp hidden mode operating condition Download PDFInfo
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- CN211184367U CN211184367U CN201922092139.4U CN201922092139U CN211184367U CN 211184367 U CN211184367 U CN 211184367U CN 201922092139 U CN201922092139 U CN 201922092139U CN 211184367 U CN211184367 U CN 211184367U
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- 230000015572 biosynthetic process Effects 0.000 title claims abstract description 77
- 238000007689 inspection Methods 0.000 title claims abstract description 33
- 238000001514 detection method Methods 0.000 claims abstract description 27
- 238000012360 testing method Methods 0.000 claims abstract description 8
- 238000007405 data analysis Methods 0.000 claims abstract description 5
- 238000005286 illumination Methods 0.000 claims description 28
- 238000011065 in-situ storage Methods 0.000 claims description 14
- 230000000694 effects Effects 0.000 claims description 3
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 230000000737 periodic effect Effects 0.000 abstract description 2
- 230000005855 radiation Effects 0.000 description 5
- 230000005611 electricity Effects 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 238000003384 imaging method Methods 0.000 description 2
- 230000004297 night vision Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
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Abstract
The utility model discloses an normal position inspection device for aircraft formation lamp hidden mode operating condition, including aircraft formation lamp panel, be provided with the infrared shimmer radiance detection module that is used for detecting aircraft formation lamp hidden mode operating condition luminous radiance on the aircraft formation lamp panel, it is right still to be provided with on the aircraft formation lamp panel the test value of infrared shimmer radiance detection module carries out data analysis and state decision's host system. The beneficial effects of the utility model reside in that: compact structure, light in weight, easy operation can carry out quick normal position inspection and periodic fixed inspection to aircraft formation lamp hidden mode operating condition under any ambient light condition, and the radiance gear of aircraft formation lamp hidden mode can be calibrated and markd, shows the inspection result through the pilot lamp, and it is convenient to observe, adopts the totally enclosed design, can be used to outfield complex environment.
Description
Technical Field
The utility model relates to an aircraft night vision compatible lighting system guarantees test technical field outside the aircraft, concretely relates to normal position inspection device that is used for aircraft formation lamp hidden mode operating condition.
Background
With the large number of installations of night vision compatible lighting devices for aircraft, the lighting and detection technology is rapidly developing. Because the light source emits infrared light waves in the concealed mode of the aircraft formation lights, the radiance of the infrared light waves is extremely low, and the infrared light waves cannot be directly observed by human eyes.
At present, equipment for accurately testing the hidden mode radiance of the aircraft formation lights at home and abroad under the environmental condition of a laboratory is provided, but the testing equipment has large volume, heavy weight and strong environmental dependence and needs to be detected in a darkroom environment. For outfield inspection of the hidden mode working state of the airplane formation lamp, the inspection process of the generally adopted infrared low-light-level imaging equipment is easily influenced by the ambient illumination, and when the ambient illumination is higher, the target gray scale contrast is poor, so that the hidden mode working state of the airplane formation lamp cannot be judged according to imaging.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to the above-mentioned not enough and defect of prior art, provide an normal position inspection device for aircraft formation lamp hidden mode operating condition to solve above-mentioned problem.
The utility model provides a technical problem can adopt following technical scheme to realize:
the utility model provides an in situ inspection device for aircraft formation lamp hidden mode operating condition which characterized in that, includes aircraft formation lamp panel, be provided with on the aircraft formation lamp panel and be used for detecting the infrared shimmer radiance detection module of the luminous radiance of aircraft formation lamp hidden mode operating condition, it is right still to be provided with on the aircraft formation lamp panel the test value of infrared shimmer radiance detection module carries out data analysis and state decision's host system.
In a preferred embodiment of the present invention, a light shield for shielding ambient light is further disposed on the light panel of the formation of the airplane.
The utility model discloses a preferred embodiment, still be provided with on the aircraft formation lamp panel and be used for detecting the ambient light illuminance detection module of the shielding effect of lens hood to external ambient light.
In a preferred embodiment of the present invention, an illumination status display module is further disposed on the panel of the aircraft formation light.
In the utility model discloses a preferred embodiment, the host system includes the calibration window that is used for the quantity of electricity pilot lamp of display device electric quantity and is used for the shift knob of controlgear work and is used for the radiance gear inspection precision of calibration equipment, the quantity of electricity pilot lamp with shift knob and the calibration window sets up side by side on the aircraft formation lamp panel.
In a preferred embodiment of the present invention, a visible light cut-off filter is disposed in the infrared low-light radiance detection module.
In a preferred embodiment of the present invention, an infrared cut filter is disposed in the ambient light illuminance detection module.
In the utility model discloses a preferred embodiment, illumination status display module includes the ambient light pilot lamp that is used for instructing the sunshade is to the shielding state of ambient light and the illumination light pilot lamp that is used for the interface that charges to equipment battery and is used for instructing the operating condition of aircraft formation lamp and corresponds the radiance gear, the ambient light pilot lamp with charge the interface and the illumination light pilot lamp interval sets up on the aircraft formation lamp panel.
Due to the adoption of the technical scheme, the beneficial effects of the utility model reside in that: compact structure, light in weight, easy operation can carry out quick normal position inspection and periodic fixed inspection to aircraft formation lamp hidden mode operating condition under any ambient light condition, and the radiance gear of aircraft formation lamp hidden mode can be calibrated and markd, shows the inspection result through the pilot lamp, and it is convenient to observe, adopts the totally enclosed design, can be used to outfield complex environment.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a front view of the in-situ inspection device for hidden mode operation of the lights of the formation of an airplane.
Fig. 2 is a bottom view of the in-situ inspection device for hidden mode operation of the lights of the formation of an airplane.
Fig. 3 is a perspective view of the in-situ inspection device for hidden mode operation of the lights of the formation team of the airplane of the present invention.
Fig. 4 is another perspective view of the in-situ inspection device for hidden mode operation of the lights of the formation of aircraft.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further explained below.
Referring to fig. 1 to 4, an in-situ inspection apparatus for concealed mode operation of an airplane formation light comprises an airplane formation light panel 100, and a wristband 110 is provided on the airplane formation light panel 100 for convenient carrying. The panel 100 of the airplane formation lamp is provided with an infrared dim light and radiation brightness detection module 200, and the infrared dim light and radiation brightness detection module 200 is used for detecting the light and radiation brightness of the hidden mode working state of the airplane formation lamp and determining the on-off state and the radiation brightness gear during on-off of the hidden mode of the airplane formation lamp. The aircraft formation light panel 100 is further provided with a main control module 300 for performing data analysis and state judgment on the test value of the infrared low-light-radiation brightness detection module 200.
Still be provided with the lens hood 400 that is used for sheltering from ambient light on the aircraft formation lamp panel 100, the lens hood 400 hugs closely aircraft formation panel 100 and can effectively shelter from ambient light, reduces external disturbance, improves the accuracy and the reliability that detect.
Still be provided with ambient light illumination detection module 500 on the formation of an airplane team lamp panel 100, ambient light illumination detection module 500 is used for detecting the shielding effect of lens hood 400 to external environment light to the laminating degree of adjustment lens hood 400 and formation of an airplane team lamp panel 100.
The aircraft formation light panel 100 is further provided with an illumination state display module 600, the illumination state display module 600 comprises an ambient light indicator lamp 610 for indicating the shielding state of the light shield 400 to ambient light, a charging interface 620 for charging a device battery, and an illumination light indicator lamp 630 for indicating the working state of the aircraft formation light and corresponding radiation brightness gears, and the ambient light indicator lamp 610, the charging interface 620 and the illumination light indicator lamp 630 are arranged on the aircraft formation light panel 100 at intervals. The illuminating light indicator 630 in this embodiment has three side-by-side and spaced apart lights on the aircraft formation light panel 100.
The main control module 300 includes a power indicator lamp 310 for displaying the power of the device, a switch button 320 for controlling the operation of the device, and a calibration window 330 for calibrating the radiance step check accuracy of the device, wherein the power indicator lamp 310, the switch button 320, and the calibration window 330 are arranged side by side on the aircraft formation lamp panel 100.
A visible light cut-off filter is arranged in the infrared low-light-radiation brightness detection module 200. The visible light cut-off filter cuts off the wave band below 600mm, and can effectively eliminate the interference of ambient light on illumination light inspection when the hidden mode working state of the airplane formation lamp is inspected.
An infrared cut-off filter is disposed in the ambient light illumination detection module 500. The infrared cut-off filter hangs 600 ~ 1000mm wave band and ends, when the detection of ambient light illuminance detection module 500, can get rid of the luminous interference to the ambient light inspection of aircraft formation lamp hidden mode effectively.
The working principle of the utility model is as follows:
the light shield 400 is attached to the airplane formation lamp panel 100 tightly, the ambient light illumination detection module 500 is used for detecting the attachment condition of the light shield 400 and the airplane formation lamp panel 100, and when the attachment is not tight or the shielding of the ambient light illumination detection module 500 is insufficient, the ambient light indicator lamp 610 of the illumination state display module 600 keeps on burning, and the adjustment of the attachment state is prompted. When the adhesion is tight or the shielding of the ambient light illumination detection module 500 is sufficient, the ambient light indicator 610 of the illumination state display module 600 is kept off, at this time, the infrared low-light-level radiance detection module 200 starts to work, when the aircraft formation lamp is in the hidden mode working state, the infrared low-light-level radiance detection module 200 detects the light-level radiance, the main control module 300 performs data analysis and state judgment on the test value, and controls the illumination indicator 630 of the illumination state display module 600 to light up, so as to indicate the working state and the radiance gear of the aircraft formation lamp. When 3 illumination pilot lamps 630 are all in the state of putting out, it is extremely low or do not work to show aircraft formation lamp hidden mode luminance, when 1 illumination pilot lamp 630 lights, it is low to show aircraft formation lamp hidden mode luminance, when 2 illumination pilot lamps 630 lights, it is medium to show aircraft formation hidden mode luminance, when 3 illumination pilot lamps 630 are all lighted, it is high to show aircraft formation lamp hidden mode luminance, calibration window 330 through host system 300, optionally calibration spoke luminance gear state, make the spoke luminance gear when inspection equipment can be more quick accurate inspection aircraft formation lamp hidden mode lights.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (8)
1. The utility model provides an in situ inspection device for aircraft formation lamp hidden mode operating condition which characterized in that, includes aircraft formation lamp panel, be provided with on the aircraft formation lamp panel and be used for detecting the infrared shimmer radiance detection module of the luminous radiance of aircraft formation lamp hidden mode operating condition, it is right still to be provided with on the aircraft formation lamp panel the test value of infrared shimmer radiance detection module carries out data analysis and state decision's host system.
2. The in-situ inspection device for hidden mode operation of aircraft formation lights according to claim 1, wherein the aircraft formation light panel is further provided with a light shield for shielding ambient light.
3. The in-situ inspection device for hidden-mode working status of aircraft formation lights according to claim 1, wherein an ambient light illumination detection module for detecting the shielding effect of the light shield on the external ambient light is further disposed on the aircraft formation light panel.
4. The in-situ inspection device for hidden-mode working condition of aircraft formation lights according to claim 1, wherein an illumination condition display module is further disposed on the panel of the aircraft formation lights.
5. The in-situ inspection device for hidden-mode working state of airplane formation lights according to claim 1, wherein the main control module comprises a power indicator light for displaying the power of the device, a switch button for controlling the device to work and a calibration window for calibrating the radiance step inspection precision of the device, and the power indicator light, the switch button and the calibration window are arranged side by side on the airplane formation light panel.
6. The in-situ inspection device for hidden mode operation of aircraft formation lights as claimed in claim 1, wherein the infrared low light intensity detection module is internally provided with a visible light cut-off filter.
7. The in-situ inspection device for hidden mode operation of aircraft formation lights as claimed in claim 3, wherein an infrared cut-off filter is disposed in the ambient light illumination detection module.
8. The in-situ inspection device for hidden-mode working states of aircraft formation lights according to claim 4, wherein the lighting state display module comprises an ambient light indicator light for indicating the shielding state of the sunshade cover against ambient light, a charging interface for charging a device battery, and an illuminating light indicator light for indicating the working state and corresponding radiance level of the aircraft formation lights, and the ambient light indicator light, the charging interface and the illuminating light indicator light are arranged on the panel of the aircraft formation lights at intervals.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922092139.4U CN211184367U (en) | 2019-11-28 | 2019-11-28 | A normal position inspection device for aircraft formation lamp hidden mode operating condition |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922092139.4U CN211184367U (en) | 2019-11-28 | 2019-11-28 | A normal position inspection device for aircraft formation lamp hidden mode operating condition |
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| CN211184367U true CN211184367U (en) | 2020-08-04 |
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| CN201922092139.4U Active CN211184367U (en) | 2019-11-28 | 2019-11-28 | A normal position inspection device for aircraft formation lamp hidden mode operating condition |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113677070A (en) * | 2021-08-23 | 2021-11-19 | 一飞(海南)科技有限公司 | Method, system, medium and application for locking light processing control of formation airplane |
| CN113702006A (en) * | 2021-08-30 | 2021-11-26 | 上海久航电子有限公司 | Device for detecting working state of off-board infrared illuminating lamp and night vision response radiance calibration method |
-
2019
- 2019-11-28 CN CN201922092139.4U patent/CN211184367U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113677070A (en) * | 2021-08-23 | 2021-11-19 | 一飞(海南)科技有限公司 | Method, system, medium and application for locking light processing control of formation airplane |
| CN113677070B (en) * | 2021-08-23 | 2023-10-31 | 一飞(海南)科技有限公司 | Method, system, medium and application for controlling locking light treatment of formation aircraft |
| CN113702006A (en) * | 2021-08-30 | 2021-11-26 | 上海久航电子有限公司 | Device for detecting working state of off-board infrared illuminating lamp and night vision response radiance calibration method |
| CN113702006B (en) * | 2021-08-30 | 2023-08-22 | 上海久航电子有限公司 | Working state detection equipment for infrared illumination lamp of machine and night vision response radiation brightness calibration method |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: An in situ inspection device for working status of aircraft formation lights in concealed mode Effective date of registration: 20230309 Granted publication date: 20200804 Pledgee: Industrial Bank Co.,Ltd. Shanghai Changning sub branch Pledgor: SHANGHAI JIUHANG ELECTRONICS CO.,LTD. Registration number: Y2023310000053 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Granted publication date: 20200804 Pledgee: Industrial Bank Co.,Ltd. Shanghai Changning sub branch Pledgor: SHANGHAI JIUHANG ELECTRONICS CO.,LTD. Registration number: Y2023310000053 |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: An in-situ inspection device for the working status of aircraft formation lights in concealed mode Granted publication date: 20200804 Pledgee: Industrial Bank Co.,Ltd. Shanghai Changning sub branch Pledgor: SHANGHAI JIUHANG ELECTRONICS CO.,LTD. Registration number: Y2024310000234 |