CN209192253U - A kind of auxiliary monitoring system for being docked in the air by oil - Google Patents
A kind of auxiliary monitoring system for being docked in the air by oil Download PDFInfo
- Publication number
- CN209192253U CN209192253U CN201821559533.3U CN201821559533U CN209192253U CN 209192253 U CN209192253 U CN 209192253U CN 201821559533 U CN201821559533 U CN 201821559533U CN 209192253 U CN209192253 U CN 209192253U
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- China
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- monitoring system
- display
- auxiliary monitoring
- oil
- fuel filling
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- Length Measuring Devices By Optical Means (AREA)
Abstract
The utility model belongs to technical field of aerospace, and in particular to a kind of in the air by the auxiliary monitoring system of oil docking.Big aircraft mostly uses soft oiling to big aircraft refuelling at present, and since fuel filling taper sleeve and refueling hose are generated by airflow influence and swung, driver is visually unable to judge accurately refueled aircraft by beam hanger and fuel filling taper sleeve relative positional relationship.The utility model provides on display picture for driver fuel filling taper sleeve at a distance from by beam hanger and location information, facilitates pilot's completion and is docked by oil；Add in the air under the complicated weather condition of raising/by oil environment adaptability, system, which has, uses two kinds of display patterns of visible light/near-infrared, can be under complicated weather condition, fuselage outfield scape when accurate display is docked；Fuel filling taper sleeve and the relative distance by beam hanger, location information can be accurately measured, when being visually unable to accurate judgement, gives driver's accurate reference；It can be prompted when being not suitable for docking to driver；Video pictures playback can carry out debriefing.
Description
Technical field
The utility model belongs to technical field of aerospace, and in particular to a kind of in the air by the Lookout assist system of oil docking
System.
Background technique
It is mainly used in big aircraft by oil in the air at present to refuel to flivver, is relied primarily on driver's mesh by oily docking operation
Depending on docking.Big aircraft mostly uses soft oiling to big aircraft refuelling, since fuel filling taper sleeve and refueling hose are generated by airflow influence
It swinging, driver is visually unable to judge accurately refueled aircraft by beam hanger and fuel filling taper sleeve relative positional relationship, it influences to dock success rate,
And difficult in bad weather or night refueling, risk is higher.
Utility model content
The utility model proposes it is a kind of based on machine vision optical measuring technique complete to the detection of fuel filling taper sleeve, with
Track, measurement, auxiliary driver complete auxiliary monitoring system aerial plus by oily task.
The utility model is achieved through the following technical solutions: the system includes camera, processor, headlamp, control
Equipment and display.Camera mainly completes the acquisition by oil docking scene, and headlamp is provided in camera whenever necessary needed for it
Light environment, processor complete image procossing, and control equipment completes the control operation to other units of this system, and display provides
Man-machine interface is completed image and is shown.
Camera acquisition outer scene is sent to display and shows after processor image procossing, while controlling as needed
Control operation is carried out on control equipment, can open headlamp as needed.Simultaneity factor receives electronics by ARINC429 bus and flies
The basic flight information and fuel oil information that row instrument system and fuel system are sent, including posture, course, air speed, height, oil mass
Etc. information, and shown together over the display with fuel filling taper sleeve metrical information.In fuel charger and refueled aircraft rendezvous phase, machine is connected
Upper self-holding switch opens the power switch in control equipment, and system starts power up starting, and system electrification self-test is normally shown just afterwards
Normal picture.In fuel filling taper sleeve distance by oily feeler lever front end 20m or so, system optics measurement function starts automatically, shows on picture
There is tapered sleeve capture frame and the opposite orientation by beam hanger of tapered sleeve, range information；When being not suitable for docking, alarm prompt function is to drive
The person of sailing provides voice prompting, display alarm prompting character on display.When fuel charger is docked with refueled aircraft, driver passes through sight
It examines and shows that fuel filling taper sleeve is relative to the distance and location information by beam hanger on picture, while alarm prompt provides for driver
Voice prompting, auxiliary driver complete to be docked by oil in the air.System also has writing function and ground is supported to play back.
The utility model has the advantages that the utility model provides a kind of for being docked auxiliary monitoring system by oil in the air, showing
Provide fuel filling taper sleeve at a distance from by beam hanger and location information for driver on picture, facilitate pilot complete it is right by oil
It connects；Add in the air under the complicated weather condition of raising/by oil environment adaptability, system has to be shown using two kinds of visible light/near-infrared
Show mode, can be under complicated weather condition, fuselage outfield scape when accurately display is docked；Can accurately measure fuel filling taper sleeve with
Relative distance, location information by beam hanger give driver's accurate reference when being visually unable to accurate judgement；It can be not suitable for
In the case of docking, prompted to driver；Video pictures playback can carry out debriefing.
Detailed description of the invention
Fig. 1 is the functional block diagram of the utility model auxiliary monitoring system.
Specific embodiment
It elaborates in conjunction with the attached drawing auxiliary monitoring system in the air by oil docking a kind of to the utility model:
A kind of auxiliary monitoring system for being docked in the air by oil is provided, is made of five Field Replaceable Unit (LRU),
Each Field Replaceable Unit (LRU) is described as follows:
1) camera mainly realizes the acquisition of video during by oil in the air, by optical window, thermal control module, supervision camera mould
The composition such as block and power module.In view of the speed, height, refueling hose length by fuel charger in oily docking operation and by oil
The angle of attack of machine by beam hanger length and adds/refueled aircraft relative positional relationship, camera is installed on by below beam hanger, and make camera
Optical axis with by beam hanger axis, at 5 ° of angles, field angle is 40 ° × 30 °, this installation site can satisfy camera add/by oil
Machine pre-mate position completes the tracking measurement to fuel filling taper sleeve；
2) headlamp acquires video for camera and provides necessary light environment under IFR conditions or night-environment,
Mainly it is made of 4 translucent cover, LED lamp component, driving assembly and power supply module parts.Headlamp is installed under by beam hanger
Side, diffusion angle are not less than 40 °, optical axis with by beam hanger axis, at 2 ° of angles, illumination range includes viewing field of camera angle；
3) processor handles the video that camera acquires, and in by oily docking operation, real-time resolving goes out tapered sleeve phase
For the location information by oily feeler lever, at the same other airborne equipments are sent basic flight information, fuel oil information and itself
Tapered sleeve metrical information, the status information calculated is superimposed upon on scenery picture, and display is sent to show, while sending control equipment note
Record.It is mainly made of main processing block, graph and image processing module, optical measurement module and power module；
4) control equipment realizes system electrification and operating mode selection, and completes the record storage by oil monitoring video.
It is mainly made of 4 light guide panel, main processing block, data storage card and power module parts；
5) vision signal that display display processor is sent.Its mainly by display control module, power module, guide rail mechanism,
Locking/part of support dual--purpose mechamism 4 forms.Display is unfolded when by oily task using fold mechanism for display；?
It is non-by oily task when, display is folded.Display is apolegamy item, if there is head up display on machine, processor can send vision signal
It is shown to head up display system.
Claims (9)
1. a kind of in the air by the auxiliary monitoring system of oil docking, it is characterised in that: the system includes connecting with processor
Camera, headlamp, control equipment and display, the control signal of the processor receiving control apparatus to camera, display and
Headlamp is controlled, and the processor will be sent to display by the received flight information of bus and fuel oil information, and will
Display is sent to by the collected outer scene of camera.
2. auxiliary monitoring system according to claim 1, it is characterised in that: after the processor is handled to display transmission
Picture.
3. auxiliary monitoring system according to claim 1, it is characterised in that: be directed toward docking area in the direction of the headlamp
Domain.
4. auxiliary monitoring system according to claim 1, it is characterised in that: the bus is ARINC429 bus.
5. auxiliary monitoring system according to claim 1, it is characterised in that: the flight information includes posture, course, sky
Speed and elevation information.
6. auxiliary monitoring system according to claim 1, it is characterised in that: also show fuel filling taper sleeve on the display
Metrical information captures frame and the opposite orientation by beam hanger of tapered sleeve, range information including tapered sleeve.
7. auxiliary monitoring system according to claim 1, it is characterised in that: in fuel filling taper sleeve distance by oily feeler lever front end
20m or so, system optics measurement function start automatically.
8. auxiliary monitoring system according to claim 1, it is characterised in that: also there is the system phonic warning to prompt function
Energy.
9. auxiliary monitoring system according to claim 8, it is characterised in that: the system also has writing function and supports ground
Face playback.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821559533.3U CN209192253U (en) | 2018-09-25 | 2018-09-25 | A kind of auxiliary monitoring system for being docked in the air by oil |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821559533.3U CN209192253U (en) | 2018-09-25 | 2018-09-25 | A kind of auxiliary monitoring system for being docked in the air by oil |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209192253U true CN209192253U (en) | 2019-08-02 |
Family
ID=67406564
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821559533.3U Active CN209192253U (en) | 2018-09-25 | 2018-09-25 | A kind of auxiliary monitoring system for being docked in the air by oil |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209192253U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113184202A (en) * | 2021-05-17 | 2021-07-30 | 湖北怡辉河天科技有限公司 | Image recognition technology-based aerial tanker oil delivery hose early warning method and system |
| CN115424496A (en) * | 2022-08-31 | 2022-12-02 | 北京蓝天航空科技股份有限公司 | Air refueling training simulation system |
-
2018
- 2018-09-25 CN CN201821559533.3U patent/CN209192253U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113184202A (en) * | 2021-05-17 | 2021-07-30 | 湖北怡辉河天科技有限公司 | Image recognition technology-based aerial tanker oil delivery hose early warning method and system |
| CN115424496A (en) * | 2022-08-31 | 2022-12-02 | 北京蓝天航空科技股份有限公司 | Air refueling training simulation system |
| CN115424496B (en) * | 2022-08-31 | 2023-09-26 | 北京蓝天航空科技股份有限公司 | Aerial refueling training simulation system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 723213 Liulin Town, Chenggu County, Hanzhong City, Shaanxi Province Patentee after: Shaanxi Aircraft Industry Co.,Ltd. Address before: 723213 box 34, Hanzhong City, Shaanxi Province Patentee before: Shaanxi Aircraft INDUSTRY(GROUP) Co.,Ltd. |
|
| CP03 | Change of name, title or address |