CN208887784U - A kind of illumination acquisition device for aircraft landing - Google Patents
A kind of illumination acquisition device for aircraft landing Download PDFInfo
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- CN208887784U CN208887784U CN201821962977.1U CN201821962977U CN208887784U CN 208887784 U CN208887784 U CN 208887784U CN 201821962977 U CN201821962977 U CN 201821962977U CN 208887784 U CN208887784 U CN 208887784U
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- data
- acquisition device
- illumination
- module
- swivel mount
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Abstract
The utility model discloses a kind of illumination acquisition devices for aircraft landing, including data acquisition device, upper cover is provided on the data acquisition device, swivel mount is installed below the upper cover, the side of the swivel mount is equipped with illuminance transducer one, the utility model is scientific and reasonable for structure, it is safe and convenient to use, it is provided with rotating device, pass through rotating device, realize 360 ° of rotations of illuminance transducer, make the acquisition range of illuminance transducer without dead angle, more adapt to the free environments on airport, device is provided with multiple illumination data acquisition devices, it is placed in each corner on airport, realize all standing, guarantee the accuracy of data, it is provided with data processing centre simultaneously, data processing centre is placed in airdrome control room, by summarizing to by illumination data acquisition device data collected, analysis obtains scientific conjunction The data of reason provide accurate data support for the landing of aircraft, guarantee the true and reliable of data.
Description
Technical field
The utility model relates to airline security device technical field, specially a kind of illumination for aircraft landing acquires dress
It sets.
Background technique
Aircraft landing, which is aircraft, glides from safe altitude and is transitioned into the sliding entire retarded motion run up to stopping completely of ground connection
Process.Aircraft landing generally divides downslide, evens up, flat fly, descend slowly and lightly, sliding 5 stages of race and carry out.Because of the reason of its characteristic, aircraft exists
To the more demanding of ground environment when landing, it is necessary to specific good illuminance.Therefore, aircraft is when landing, it is necessary to airport
The actual conditions on airport are fed back to crew by control room, and judge the landing measure that take with this, such as by anti-
The practical illuminance on airport is presented to determine whether landing headlamp should be opened.But illumination acquisition device at present on the market,
There is more apparent defect, the illumination data in one orientation of acquisition that can only be fixed, the illumination data of acquisition has biggish
Error, therefore the reliability of data is not strong, and cannot accomplish all region covering, and data are easy to happen when encountering emergency and are lacked
The situation of mistake.So being badly in need of a kind of illumination acquisition device to solve the problems, such as this.
Utility model content
The utility model provides a kind of illumination acquisition device for aircraft landing, can effectively solve in above-mentioned background technique
The illumination acquisition device at present on the market mentioned, has more apparent defect, the photograph in one orientation of acquisition that can only be fixed
Degree evidence, the illumination data of acquisition has biggish error, therefore the reliability of data is not strong, and cannot accomplish that entire area is covered
The problem of covering, the situation of shortage of data be easy to happen when encountering emergency.
To solve the above-mentioned problems, the utility model provides the following technical solutions: a kind of illumination for aircraft landing is adopted
Acquisition means, including data acquisition device are provided with upper cover on the data acquisition device, rotation are equipped with below the upper cover
Frame, the side of the swivel mount are equipped with illuminance transducer one, and the other side of the swivel mount is equipped with illuminance transducer two, institute
It states and bottom cover is installed below swivel mount, support rod is provided with below the bottom cover, the bottom of the support rod is provided with solid
Reservation.Support frame one is installed, the side of support frame as described above one is equipped with axis, the other end of the axis in the swivel mount
Support frame two is installed, the side of the axis is equipped with transmission shaft, and the side of the transmission shaft is equipped with rotating electric machine, described
Data acquisition device is connected with data processing centre, and the Data processing is provided with protective housing, the protective housing outside in the heart
It is provided with display screen, the side of the display screen is provided with key, and the inside of the protective housing is equipped with data reception module, institute
The side for stating data reception module is equipped with quantity processing module, and the side of the data processing module is equipped with quantity storage mould
Block, the side of the data memory module are provided with control module, and the side of the control module is equipped with emergency power supply, described
The side of emergency power supply is equipped with power supply, and the side of the power supply is provided with power interface.
Preferably, the rotating electric machine, data reception module, data processing module, data memory module, control module are equal
It is electrically connected between power supply and emergency power supply.
Preferably, the data acquisition device surface is black frosted material.
Preferably, the axis is connect with transmission shaft by shaft coupling.
Preferably, the data acquisition device is connect with data processing centre by data transmission cable.
Preferably, fixing bolt is provided in the fixing seat.
Compared with prior art, the utility model has the beneficial effects that the utility model is scientific and reasonable for structure, use is safe
It is convenient:
1, several illumination data acquisition devices are provided with, illumination data acquisition dress is installed by the different parts on airport
It sets, realizes that illumination data acquires all standing, guarantee the Integrity And Reliability of data.
2, it is provided with rotating device, illuminance transducer can be realized 360 ° of automatic rotations by rotating device, guarantee data
It is comprehensive, without dead angle, it is ensured that the accuracy of illumination data.
3, it is provided with data processing centre, data processing centre is placed in airdrome control room, by by illumination data
Acquisition device data collected are summarized, are analyzed and obtained scientific and reasonable data, provide accurate number for the landing of aircraft
According to support, guarantee the true and reliable of data.
Detailed description of the invention
Attached drawing is used to provide a further understanding of the present invention, and constitutes part of specification, practical with this
Novel embodiment is used to understand the utility model together, does not constitute limitations of the present invention.
In the accompanying drawings:
Fig. 1 is the data acquisition device schematic diagram of the utility model；
Fig. 2 is the rotating mechanism schematic diagram of the utility model；
Fig. 3 is data processing centre's schematic diagram of the utility model；
Figure label: 1, data acquisition device；2, upper cover；3, swivel mount；4, illuminance transducer one；5, illuminance transducer
Two；6, bottom cover；7, support rod；8, fixing seat；9, support frame one；10, support frame two；11, axis；12, transmission shaft；13, it rotates
Motor；14, data processing centre；15, protective housing；16, display screen；17, key；18, data reception module；19, data processing
Module；20, data memory module；21, control module；22, emergency power supply；23, power supply；24, power interface.
Specific embodiment
It is illustrated below in conjunction with preferred embodiment of the attached drawing to the utility model, it should be understood that this place is described excellent
It selects embodiment to be only used for describing and explaining the present invention, is not used to limit the utility model.
Embodiment: as shown in Figure 1-3, a kind of illumination acquisition device for aircraft landing, including data acquisition device 1,
Upper cover 2 is provided on data acquisition device 1, the lower section of upper cover 2 is equipped with swivel mount 3, and the side of swivel mount 3 is equipped with illumination biography
Sensor 1, the model YS-CG-J of illuminance transducer 1, the other side of swivel mount 3 is equipped with illuminance transducer 25, illumination
The model YS-CG-J of sensor 25, the lower section of swivel mount 3 are equipped with bottom cover 6, and the lower section of bottom cover 6 is provided with support rod 7, branch
The bottom of strut 7 is provided with fixing seat 8, in order to guarantee the stability of device, is provided with fixing bolt on the fixing seat (8),
Reflective phenomenon occurs for data acquisition device 1 in order to prevent, interferes the work of illuminance transducer, and 1 surface of data acquisition device is black
Color frosted material, is equipped with support frame 1 in swivel mount 3, and the side of support frame 1 is equipped with axis 11, axis 11 it is another
End is equipped with support frame 2 10, and the side of axis 11 is equipped with transmission shaft 12, in order to guarantee the stability of the work of rotating electric machine 13,
Axis 11 is connect with transmission shaft 12 by shaft coupling, and the side of transmission shaft 12 is equipped with rotating electric machine 13, the type of rotating electric machine 13
It number is 4912ZJLS-452-1, data acquisition device 1 is connected with data processing centre 14, is provided in data processing centre 14 anti-
Protecting box 15, display screen 16 is provided on the outside of protective housing 15, and the side of display screen 16 is provided with key 17, the inside peace of protective housing 15
Equipped with data reception module 18, the side of data reception module 18 is equipped with quantity processing module 19, data processing module 19
Side is equipped with quantity memory module 20, and the side of data memory module 20 is provided with control module 21, and the one of control module 21
Side is equipped with emergency power supply 22, and the side of emergency power supply 22 is equipped with power supply 23, and the side of power supply 23 is provided with power interface 24,
Rotating electric machine 13, data reception module 18, data processing module 19, data memory module 20, control module 21 with power supply 23
And be electrically connected between emergency power supply 22, because of the particularity on airport, the interference of wireless signal causes data to be transmitted in order to prevent
It goes wrong, data acquisition device 1 is connect with data processing centre 14 by data transmission cable.
The working principle and process for using of the utility model: when using the present apparatus, data acquisition device 1 is installed first
Data processing centre 14 is mounted in airdrome control room by the suitable position on airport, and passes through conducting wire and data transmission cable
Data acquisition device 1 is connect with data processing centre 14, data acquisition device 1 is made to be powered, at this time illuminance transducer 1 and photograph
It spends sensor 25 to start to work, while rotating electric machine 13 starts slowly to rotate, and drives transmission shaft 12, in the drive of transmission shaft 12
Axis 11, axis 11 rotate swivel mount 3 by support frame 1 and support frame 2 10, and swivel mount 3 drives the photograph for being mounted on its two sides
It spends sensor 1 and illuminance transducer 25 rotates, keep illuminance transducer 1 and the induction range of illuminance transducer 25 bigger.
After illuminance transducer 1 and illuminance transducer 25 collect illumination data, by data transmission cable by data
It is transmitted in the data reception module 18 installed in data processing centre 14, when data reach data reception module 18, data
Processing module 19 can will be analyzed and processed the data summarized, obtain scientific and reasonable synthesis illumination data, and pass through display
Shield 16 real-time displays, data can be stored by data memory module 20, in case later period verification uses.
When in use, user by 17 input data of key, can be controlled by control module 21 according to the actual needs
The revolving speed of rotating electric machine 13, the data transmission frequencies of illuminance transducer 1 and illuminance transducer 25, data memory module 20
Data clear up the control such as time limit item automatically, with user-friendly.Device is provided with emergency power supply 22, can be electrically disconnected in city
In the case where, guarantee the normal operation in device certain time.
Finally, it should be noted that being not limited to this reality the foregoing is merely the preferred embodiment of the utility model
With novel, although the utility model is described in detail with reference to the foregoing embodiments, come for those skilled in the art
Say, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic into
Row equivalent replacement.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on, should all
It is included within the scope of protection of this utility model.
Claims (6)
1. a kind of illumination acquisition device for aircraft landing, including data acquisition device (1), it is characterised in that: the data
It is provided on acquisition device (1) upper cover (2), is equipped with swivel mount (3) below the upper cover (2), the one of the swivel mount (3)
Side is equipped with illuminance transducer one (4), and the other side of the swivel mount (3) is equipped with illuminance transducer two (5), the swivel mount
(3) it is equipped with below bottom cover (6), is provided with support rod (7) below the bottom cover (6), the bottom of the support rod (7) is set
It is equipped with fixing seat (8), support frame one (9) is installed in the swivel mount (3), during the side of support frame as described above one (9) is equipped with
Axis (11), the other end of the axis (11) are equipped with support frame two (10), and the side of the axis (11) is equipped with transmission shaft
(12), the side of the transmission shaft (12) is equipped with rotating electric machine (13), and the data acquisition device (1) is connected with data processing
Center (14) is provided with protective housing (15) on the data processing centre (14), is provided with display on the outside of the protective housing (15)
Shield (16), the side of the display screen (16) is provided with key (17), and the inside of the protective housing (15) is equipped with data receiver
The side of module (18), the data reception module (18) is equipped with quantity processing module (19), the data processing module
(19) side is equipped with quantity memory module (20), and the side of the data memory module (20) is provided with control module
(21), the side of the control module (21) is equipped with emergency power supply (22), and the side of the emergency power supply (22) is equipped with electricity
The side in source (23), the power supply (23) is provided with power interface (24).
2. a kind of illumination acquisition device for aircraft landing according to claim 1, it is characterised in that: the electric rotating
Machine (13), data reception module (18), data processing module (19), data memory module (20), control module (21) with electricity
It is electrically connected between source (23) and emergency power supply (22).
3. a kind of illumination acquisition device for aircraft landing according to claim 1, it is characterised in that: the data are adopted
Acquisition means (1) surface is black frosted material.
4. a kind of illumination acquisition device for aircraft landing according to claim 1, it is characterised in that: the axis
(11) it is connect with transmission shaft (12) by shaft coupling.
5. a kind of illumination acquisition device for aircraft landing according to claim 1, it is characterised in that: the data are adopted
Acquisition means (1) are connect with data processing centre (14) by data transmission cable.
6. a kind of illumination acquisition device for aircraft landing according to claim 1, it is characterised in that: the fixing seat
(8) fixing bolt is provided on.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821962977.1U CN208887784U (en) | 2018-11-26 | 2018-11-26 | A kind of illumination acquisition device for aircraft landing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821962977.1U CN208887784U (en) | 2018-11-26 | 2018-11-26 | A kind of illumination acquisition device for aircraft landing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208887784U true CN208887784U (en) | 2019-05-21 |
Family
ID=66518617
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821962977.1U Expired - Fee Related CN208887784U (en) | 2018-11-26 | 2018-11-26 | A kind of illumination acquisition device for aircraft landing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208887784U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111030721A (en) * | 2019-11-28 | 2020-04-17 | 江苏趋云信息科技有限公司 | Miniature portable information transmission equipment |
| CN114486188A (en) * | 2022-01-04 | 2022-05-13 | 北京华创空港工程有限公司 | Light intensity detection system for airfield lights |
-
2018
- 2018-11-26 CN CN201821962977.1U patent/CN208887784U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111030721A (en) * | 2019-11-28 | 2020-04-17 | 江苏趋云信息科技有限公司 | Miniature portable information transmission equipment |
| CN114486188A (en) * | 2022-01-04 | 2022-05-13 | 北京华创空港工程有限公司 | Light intensity detection system for airfield lights |
| CN114486188B (en) * | 2022-01-04 | 2024-04-09 | 北京华创空港工程有限公司 | Airport light intensity detection system |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190521 Termination date: 20201126 |
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| CF01 | Termination of patent right due to non-payment of annual fee |