CN109899708A - A kind of video monitoring dual-mode illumination system for rigid fuel charger - Google Patents
A kind of video monitoring dual-mode illumination system for rigid fuel charger Download PDFInfo
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- CN109899708A CN109899708A CN201711302693.XA CN201711302693A CN109899708A CN 109899708 A CN109899708 A CN 109899708A CN 201711302693 A CN201711302693 A CN 201711302693A CN 109899708 A CN109899708 A CN 109899708A
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- illuminatian plate
- fuselage
- head
- led light
- video monitoring
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- 238000005286 illumination Methods 0.000 title claims abstract description 24
- 239000000446 fuel Substances 0.000 title claims abstract description 22
- 238000012544 monitoring process Methods 0.000 title claims abstract description 17
- 238000013461 design Methods 0.000 claims abstract description 3
- 239000012530 fluid Substances 0.000 abstract description 5
- 230000009286 beneficial effect Effects 0.000 abstract description 4
- 238000003032 molecular docking Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000004297 night vision Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000012549 training Methods 0.000 description 1
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Abstract
The present invention discloses a kind of video monitoring dual-mode illumination system for rigid fuel charger, include, head illuminatian plate and fuselage illuminatian plate, the head illuminatian plate and the fuselage illuminatian plate are modularized design, the two is fixed into V-shaped structure by connecting angle support, the head illuminatian plate is used to illuminate the head section of refueled aircraft, there is the first visible LED light bar and the first infrared light LED light strip on the light-emitting surface of the head illuminatian plate, the fuselage illuminatian plate is used to illuminate the fuselage sections of refueled aircraft, there is the second visible LED light bar and the second infrared light LED light strip on the light-emitting surface of the fuselage illuminatian plate.The luminous intensity of visible LED light bar and infrared light LED light strip, which can be realized, to be continuously adjusted, and head illuminatian plate can work or work at the same time respectively with fuselage illuminatian plate, to adapt to by hydraulic fluid port in head or the refueled aircraft of fuselage different location.The beneficial effects of the present invention are: for it is camera supervised plus, refueled aircraft docking local floodlighting is provided.
Description
Technical field
The present invention relates to a kind of video monitoring dual-mode illumination systems for rigid fuel charger.
Background technique
In initial rigid refueling process, the refueling operation person on fuel charger is seen by the backsight window on rear side of ventral
It examines by the refueled aircraft of back lower place Step wise approximation, when refueled aircraft arrives at predetermined position, is docked, refueling operation.With technology
Be constantly progressive, the operating condition of oiling operator is greatly improved, on the rigid fuel charger of modernization, oiling console
It moves in the cabin of fuel charger, refueling operation person observes docking, refueling for oiling hard tube and refueled aircraft by video monitoring picture
Operation.The system relates generally to monitor camera, monitoring interface and provides the lighting system of ambient lighting for video camera, they
Play the role of for the safety of rigid oiling, reliability vital, is the important component in fuel loading system.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of video monitoring dual-mode illumination for rigid fuel charger
System.
In order to realize the purpose, technical scheme is as follows: a kind of video monitoring for rigid fuel charger is double
Mode illumination system includes head illuminatian plate and fuselage illuminatian plate, and the head illuminatian plate and the fuselage illuminatian plate are common
It is arranged in V-shaped structure, the head illuminatian plate is used to illuminate the head section of refueled aircraft, the light-emitting surface of the head illuminatian plate
Upper to have the first visible LED light bar and the first infrared light LED light strip, the fuselage illuminatian plate is used to illuminate the fuselage of refueled aircraft
Part has the second visible LED light bar and the second infrared light LED light strip on the light-emitting surface of the fuselage illuminatian plate.
As a kind of preferred embodiment of video monitoring dual-mode illumination system for rigid fuel charger, also include, even
Connect angle support, have first while and when second, first side is mutually fixably coupled with the head illuminatian plate, described second
Side is mutually fixably coupled with the fuselage illuminatian plate, by connect angle support can determine head illuminatian plate and fuselage illuminatian plate it
Between angle.
As a kind of preferred embodiment of video monitoring dual-mode illumination system for rigid fuel charger, described first is visible
Extending direction of the light LED light strip with the first infrared light LED light strip along the head illuminatian plate is uniformly and alternately distributed,
Luminous intensity continuously adjustable.
As a kind of preferred embodiment of video monitoring dual-mode illumination system for rigid fuel charger, described second is visible
Extending direction of the light LED light strip with the second infrared light LED light strip along the fuselage illuminatian plate is uniformly and alternately distributed,
Luminous intensity continuously adjustable.
Compared with prior art, beneficial effects of the present invention at least that: lighting system is mounted on the rear side of oiling ventral,
Under low environment illumination conditions, especially in night refueling, for it is camera supervised plus, refueled aircraft docking floodlighting is provided.
According to the position on refueled aircraft by hydraulic fluid port, the illumination region of lighting system it is adjustable to head illumination or frame sections illumination,
Visible light close friend light illumination mode is used when safety zone is refueled, and uses infrared cove lighting mode in nearly enemy's war danger area, two kinds
It will not influence the observation using effect of night vision goggles under operating mode.No cascade may be implemented in luminous intensity under both of which
It is continuous to adjust, to adapt to the individual observation demand difference of different refueling operation personnel under various ambient light illuminations.
In addition to it is described above present invention solves the technical problem that, constitute technical solution technical characteristic and by these
Except beneficial effect brought by the technical characteristic of technical solution, other technologies problem, technical solution that the present invention can solve
In include other technical characteristics and these technical characteristic bring beneficial effects, will be made in conjunction with attached drawing further details of
Explanation.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of one embodiment of the invention.
Fig. 2 is that the lighting module of one embodiment of the invention splices schematic diagram.
Fig. 3 is the usage state diagram of lighting system and refueled aircraft in one embodiment of the invention.(A is by hydraulic fluid port)
Fig. 4 is the usage state diagram of one embodiment of the invention fuel charger and refueled aircraft.(A is by hydraulic fluid port)
Fig. 5 is the circuit diagram of one embodiment of the invention.
Specific embodiment
Below by specific embodiment combination attached drawing, invention is further described in detail.It needs to illustrate herein
It is the explanation of these embodiments to be used to help to understand the present invention, but do not constitute a limitation of the invention.In addition, below
Involved technical characteristic as long as they do not conflict with each other can phase in the described each embodiment of the present invention
Mutually combination.
Referring to Figure 1 to 4, a kind of video monitoring dual-mode illumination system for rigid fuel charger is shown in the figure.
The lighting system is mainly made of head illuminatian plate 1, fuselage illuminatian plate 2, the connection components such as angle support 3 and control device.Institute
It states head illuminatian plate and the fuselage illuminatian plate is mounted on the downside of the tail of fuel charger.Control device is mounted in cabin.
The head illuminatian plate and the fuselage illuminatian plate Common arrangements are at V-shaped structure.The head illuminatian plate is used for
Illuminate the head section of refueled aircraft.It is infrared with the first visible LED light bar and first on the light-emitting surface of the head illuminatian plate
Light LED light strip.The first visible LED light bar 11 is with the first infrared light LED light strip 12 along the head illuminatian plate
Extending direction is uniformly and alternately distributed.The fuselage illuminatian plate is used to illuminate the fuselage sections of refueled aircraft.The fuselage illumination
There is the second visible LED light bar 21 and the second infrared light LED light strip 22 on the light-emitting surface of plate.The second visible LED lamp
Extending direction of the band with the second infrared light LED light strip along the fuselage illuminatian plate is uniformly and alternately distributed.The connection
Angle support have first while and when second.First side is mutually fixably coupled with the head illuminatian plate, second side with
The fuselage illuminatian plate is mutually fixably coupled.
Fig. 5 is referred to again, it is seen that light LED light strip is driven with infrared light LED light strip by constant-current driven module.
Function narration:
(1) head illuminatian plate, fuselage illuminatian plate use visible LED and infrared LED for light source, have environmental protection, energy conservation, longevity
The advantages that life, highly reliable, vibration resistance.Two kinds of light sources replace array arrangement on light source printed board component, guarantee in each mode
Under can realize Uniform Illumination.
(2) friendly illumination operating mode is realized by visible LED, the oiling training or manoeuvre suitable for peacetime；
It realizes that cove lighting operating mode avoids being found by enemy suitable for the air refuelling in the period of operation by infrared LED, improves
The safety of oiling.
(3) friendly, the hidden operating mode of lighting system is realized by the switching of control device, and the hair of each pattern
Luminous intensity can continuous electrodeless adjustment, to adapt to different combat duties, varying environment lighting condition and different operation personnel
Individual demand.
(4) head illuminatian plate, fuselage illuminatian plate are modular construction, can increase number of segment according to actual needs, and
It is fixed by the connection angle support (such as 90 °, 120 °, 150 °) of different size according to required angle.
(5) lighting device is two-part structure, can illuminate head and fuselage respectively, and the two can individually or simultaneously work
Make, suitable for being located at the refueled aircraft of head or fuselage different location by hydraulic fluid port.
(6) system applies also for hatch door, the cargo handling, maintenance of such as transporter in addition to being applied to fuel charger
Purposes.
Embodiments of the present invention are only expressed above, and the description thereof is more specific and detailed, but and cannot therefore understand
For the limitation to patent of invention range.It should be pointed out that for those of ordinary skill in the art, not departing from this hair
Under the premise of bright design, various modifications and improvements can be made, and these are all within the scope of protection of the present invention.Therefore, this hair
The scope of protection shall be subject to the appended claims for bright patent.
Claims (5)
1. a kind of video monitoring dual-mode illumination system for rigid fuel charger, which is characterized in that include head illuminatian plate
And fuselage illuminatian plate, the head illuminatian plate and the fuselage illuminatian plate Common arrangements are at V-shaped structure, the head illuminatian plate
For illuminating the head section of refueled aircraft, there is the first visible LED light bar and first on the light-emitting surface of the head illuminatian plate
Infrared light LED light strip, the fuselage illuminatian plate are used to illuminate the fuselage sections of refueled aircraft, on the light-emitting surface of the fuselage illuminatian plate
With the second visible LED light bar and the second infrared light LED light strip.
2. a kind of video monitoring dual-mode illumination system for rigid fuel charger according to claim 1, feature exist
In, also include to connect angle support, have first while and when second, first side is mutually fixed with the head illuminatian plate
Ground combines, and second side is mutually fixably coupled with the fuselage illuminatian plate.
3. a kind of video monitoring dual-mode illumination system for rigid fuel charger according to claim 1, feature exist
In head illuminatian plate and fuselage illuminatian plate use modularized design, after angle between the two is adjusted, with the company of corresponding angle
It connects angle support to fix, and according to the usage requirement, continuously expands splicing using multiple lighting modules.
4. a kind of video monitoring dual-mode illumination system for rigid fuel charger according to claim 1 or 2, feature
It is, the first visible LED light bar is equal along the extending direction of the head illuminatian plate with the first infrared light LED light strip
Even and be alternately distributed, luminous intensity can continuously adjust.
5. a kind of video monitoring dual-mode illumination system for rigid fuel charger according to claim 1 or 2, feature
It is, the second visible LED light bar is equal along the extending direction of the fuselage illuminatian plate with the second infrared light LED light strip
Even and be alternately distributed, luminous intensity can continuously adjust.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711302693.XA CN109899708A (en) | 2017-12-08 | 2017-12-08 | A kind of video monitoring dual-mode illumination system for rigid fuel charger |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711302693.XA CN109899708A (en) | 2017-12-08 | 2017-12-08 | A kind of video monitoring dual-mode illumination system for rigid fuel charger |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109899708A true CN109899708A (en) | 2019-06-18 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711302693.XA Pending CN109899708A (en) | 2017-12-08 | 2017-12-08 | A kind of video monitoring dual-mode illumination system for rigid fuel charger |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050017130A1 (en) * | 2003-07-25 | 2005-01-27 | Shelly Mark A. | Methods and apparatus for illumination of refueling hoses |
| US20090140099A1 (en) * | 2006-04-13 | 2009-06-04 | The Boeing Company | Device, method, and aircraft for illuminating in-flight operations |
| EP2535273A1 (en) * | 2011-06-17 | 2012-12-19 | EADS Construcciones Aeronauticas, S.A. | Aircraft refueling boom with a nozzle illuminating module |
| CN207729325U (en) * | 2017-12-08 | 2018-08-14 | 上海航空电器有限公司 | A kind of video monitoring dual-mode illumination system for rigid fuel charger |
-
2017
- 2017-12-08 CN CN201711302693.XA patent/CN109899708A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050017130A1 (en) * | 2003-07-25 | 2005-01-27 | Shelly Mark A. | Methods and apparatus for illumination of refueling hoses |
| US20090140099A1 (en) * | 2006-04-13 | 2009-06-04 | The Boeing Company | Device, method, and aircraft for illuminating in-flight operations |
| EP2535273A1 (en) * | 2011-06-17 | 2012-12-19 | EADS Construcciones Aeronauticas, S.A. | Aircraft refueling boom with a nozzle illuminating module |
| CN207729325U (en) * | 2017-12-08 | 2018-08-14 | 上海航空电器有限公司 | A kind of video monitoring dual-mode illumination system for rigid fuel charger |
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