CN107367373A - A kind of optical cable wire harness assembly connecting fault check device and inspection method - Google Patents
A kind of optical cable wire harness assembly connecting fault check device and inspection method Download PDFInfo
- Publication number
- CN107367373A CN107367373A CN201610314630.5A CN201610314630A CN107367373A CN 107367373 A CN107367373 A CN 107367373A CN 201610314630 A CN201610314630 A CN 201610314630A CN 107367373 A CN107367373 A CN 107367373A
- Authority
- CN
- China
- Prior art keywords
- optical cable
- wire harness
- cable wire
- harness assembly
- module
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M11/00—Testing of optical apparatus; Testing structures by optical methods not otherwise provided for
- G01M11/30—Testing of optical devices, constituted by fibre optics or optical waveguides
- G01M11/33—Testing of optical devices, constituted by fibre optics or optical waveguides with a light emitter being disposed at one fibre or waveguide end-face, and a light receiver at the other end-face
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- General Physics & Mathematics (AREA)
- Investigating Materials By The Use Of Optical Means Adapted For Particular Applications (AREA)
Abstract
The invention belongs to Computer Control Technology field, more particularly to a kind of optical cable wire harness assembly connecting fault check device and inspection method, by using the mode of controlled in wireless, the inspection to the connecting fault of connector and optical cable in airborne optical cable wire harness assembly is realized, efficiently solves connector and the technical problem of diagnosis and the positioning of the connecting fault of optical cable to occurring during airborne optical cable wire harness assembly use；Simultaneously, it is possible to achieve detection is synchronized to all signalling channels of airborne optical cable wire harness assembly, greatly improves airborne optical cable wire harness assembly connecting fault positioning and maintenance efficiency；The present invention, it is simple and easy, airborne optical cable wire harness assembly connecting fault analysis can be simplified and differentiate operating process, avoid unnecessary manual intervention, improve networking component maintenance quality and efficiency, the characteristics of with versatility, it can be promoted the use of in the Generation of Airborne FC data communication bus application of net such as airborne, vehicle-mounted and boat-carrying field.
Description
Technical field
The invention belongs to Computer Control Technology field, and in particular to a kind of optical cable wire harness assembly connecting fault check device and inspection method.
Background technology
The advanced operational aircraft in home and abroad, largely using FC optical-fibre channels bus network, realize airborne avionics information and the height of process resource is warm.Airborne optical cable wire harness assembly as the physical connection for realizing FC optical-fibre channel bus network equipment critical product, must assure that its daily possesses intact working condition.The connector and the connecting fault of optical cable being likely to occur during airborne optical cable wire harness assembly use mainly include connector contact failure and optical cable with broken point failure.Two kinds of failures will all cause the optical signal transmission transmitted in airborne optical cable wire harness assembly abnormal, influence the network communication failure of equipment room.
At present, it is to utilize independent spot light and light power meter to commonly use airborne optical cable wire harness assembly inspection method, according to the stitch order of cable assembly connector, from component both ends by checking.However, this test mode has trivial operations, the problem of working strength is big is checked.
The content of the invention
The purpose of the present invention be overcome complex operation present in existing airborne optical cable wire harness assembly inspection method, the problem of working strength is big, efficiency is low.
Therefore, the invention provides a kind of optical cable wire harness assembly connecting fault check device and inspection method：
Wherein, optical cable wire harness assembly connecting fault check device includes data processing equipment, transmitting photocontrol module, image capture module；The transmitting photocontrol module is connected by the first connection camera bellows with the connector at optical cable wire harness assembly A ends；Described image acquisition module is connected by the second connection camera bellows with the connector at optical cable wire harness assembly B ends；The data processing equipment sends remote control commands by communication module to transmitting photocontrol module, image capture module, and the communication module is wireless WIFI modules.
A kind of above-mentioned optical cable wire harness assembly connecting fault check device, the data processing equipment includes the first invisible antenna, data processor, the display module being sequentially connected by data/address bus, and the display module is data and image display.
A kind of above-mentioned optical cable wire harness assembly connecting fault check device, the transmitting photocontrol module includes the second invisible antenna, the first instruction control module, first switch, LED light source, the first connection camera bellows being sequentially connected by control line, and the first instruction control module, first switch, LED light source are connected with the first battery.
A kind of above-mentioned optical cable wire harness assembly connecting fault check device, described image acquisition module includes the 3rd invisible antenna, the second instruction control module, second switch, image acquisition device, the second connection camera bellows being sequentially connected by control line, and the second instruction control module, second switch, image acquisition device are connected with the second battery.
The connector at a kind of above-mentioned optical cable wire harness assembly connecting fault check device, the first connection camera bellows and optical cable wire harness assembly A ends, described second are connected camera bellows and are threadedly connected with the connector at optical cable wire harness assembly B ends.
Wherein, optical cable wire harness assembly connecting fault inspection method, specifically comprises the following steps：
Step 1: the data processor of data processing equipment is sent by the first invisible antenna starts LED light sourse instruction；
Step 2: the first instruction control module of transmitting photocontrol module starts first switch by the startup LED light sourse instruction in the second invisible antenna receiving step one, the first instruction control module, LED light source is opened；
Step 3: the data processor of data processing equipment is sent by the first invisible antenna starts image capture instruction；
Step 4: the second instruction control module of image capture module passes through the startup image capture instruction in the 3rd invisible antenna receiving step three, second instruction control module opens second switch, and image capture instruction will be started and be sent to image acquisition device, and then image acquisition device starts to gather the end face figure like of optical cable wire harness assembly connector；
Step 5: the data processor of data processing equipment is sent by the first invisible antenna starts image transmission instruction；
Step 6: the second instruction control module of image capture module sends instruction by the startup image in the 3rd invisible antenna receiving step five, second instruction control module opens second switch, while the end face figure like of the optical cable wire harness assembly connector collected in step 4 is sent to the second instruction control module by image acquisition device；
Step 7: the data processor of data processing equipment receives the end face figure like data for the optical cable wire harness assembly connector that the second instruction control module is sent by the first invisible antenna；
Step 8: the end face figure like data of optical cable wire harness assembly connector of the data processor of data processing equipment to receiving carry out hot spot gray proces, and the order descending according to hot spot gradation data, the conduction light intensity levels data that optical cable wire harness assembly connects optical fiber are converted to successively；
Step 9: the conduction light intensity levels data transfer that optical cable wire harness assembly is connected optical fiber by the data processor of data processing equipment is completed data and shown with image, while use the working condition of different colours nominal light cable tread assembly interface channel to display module.
Beneficial effects of the present invention：This optical cable wire harness assembly connecting fault check device provided by the invention, by using the mode of controlled in wireless, the inspection to the connecting fault of connector and optical cable in airborne optical cable wire harness assembly is realized, efficiently solves connector and the technical problem of diagnosis and the positioning of the connecting fault of optical cable to occurring during airborne optical cable wire harness assembly use；Simultaneously, it is possible to achieve detection is synchronized to all signalling channels of airborne optical cable wire harness assembly, greatly improves airborne optical cable wire harness assembly connecting fault positioning and maintenance efficiency.Therefore, the optical cable wire harness assembly connecting fault check device, it is simple and easy, airborne optical cable wire harness assembly connecting fault analysis can be simplified and differentiate operating process, unnecessary manual intervention is avoided, improve networking component maintenance quality and efficiency；Meanwhile using controlled in wireless and intensive data treatment technology, flexibly control for airborne optical cable wire harness assembly connecting fault fail-safe analysis and device and provide technical guarantee.
The present invention is described in further details below with reference to drawings and Examples.
Brief description of the drawings
Fig. 1 is a kind of connection diagram of optical cable wire harness assembly connecting fault check device of the present invention.
Fig. 2 is the connection block diagram of data processing equipment in a kind of optical cable wire harness assembly connecting fault check device of the present invention.
Fig. 3 is to launch the connection block diagram of optical module and its connection diagram with optical cable wire harness assembly connector in a kind of optical cable wire harness assembly connecting fault check device of the present invention.
Fig. 4 is the connection block diagram of image capture module and its connection diagram with optical cable wire harness assembly connector in a kind of optical cable wire harness assembly connecting fault check device of the present invention.
Fig. 5 is the schematic diagram that in step 8 the end face figure like data that receive are carried out with hot spot gray proces in a kind of optical cable wire harness assembly connecting fault inspection method of the present invention.
Description of reference numerals：1st, data processing equipment；2nd, photocontrol module is launched；3rd, image capture module；4th, the first connection camera bellows；5th, the second connection camera bellows.
Embodiment
For the technological means and effect that the present invention reaches predetermined purpose and taken is expanded on further, embodiment, architectural feature and its effect below in conjunction with drawings and Examples to the present invention, describe in detail as follows.
A kind of connection diagram of optical cable wire harness assembly connecting fault check device as shown in Figure 1, data processing equipment 1, transmitting photocontrol module 2, image capture module 3；Transmitting photocontrol module 2 is connected by the first connection camera bellows 4 with the connector at optical cable wire harness assembly A ends；Image capture module 3 is connected by the second connection camera bellows 5 with the connector at optical cable wire harness assembly B ends, and first connects the connector at camera bellows 4 and optical cable wire harness assembly A ends, second is connected camera bellows 5 and can threadedly be connected with the connector at optical cable wire harness assembly B ends；Data processing equipment 1 sends remote control commands by communication module to transmitting photocontrol module 2, image capture module 3, realize that the LED light source ON/OFF control of transmitting photocontrol module 2 and the image zooming-out of image capture module 3 control with uploading, in addition, communication module can be wireless WIFI modules.
As shown in Fig. 2 data processing equipment 1 includes the first invisible antenna, data processor, the display module being sequentially connected by data/address bus, display module is data and image display；As shown in Figure 3, transmitting photocontrol module 2 includes the second invisible antenna, the first instruction control module, first switch, LED light source, the first connection camera bellows 4 being sequentially connected by control line, and the first instruction control module, first switch, LED light source are connected with the first battery；As shown in Figure 4, image capture module 3 includes the 3rd invisible antenna, the second instruction control module, second switch, image acquisition device, the second connection camera bellows 5 being sequentially connected by control line, and the second instruction control module, second switch, image acquisition device are connected with the second battery.
The device specifically comprises the following steps when checking the connecting fault of airborne cable line tread assembly：Step 1: the data processor of data processing equipment 1 is sent by the first invisible antenna starts LED light sourse instruction；Step 2: the first instruction control module of transmitting photocontrol module 2 starts first switch by the startup LED light sourse instruction in the second invisible antenna receiving step one, the first instruction control module, LED light source is opened；Step 3: the data processor of data processing equipment 1 is sent by the first invisible antenna starts image capture instruction；Step 4: the second instruction control module of image capture module 3 passes through the startup image capture instruction in the 3rd invisible antenna receiving step three, second instruction control module opens second switch, and image capture instruction will be started and be sent to image acquisition device, and then image acquisition device starts to gather the end face figure like of optical cable wire harness assembly connector；Step 5: after waiting 1~2 second, the data processor of data processing equipment 1 is sent by the first invisible antenna starts image transmission instruction；Step 6: the second instruction control module of image capture module 3 sends instruction by the startup image in the 3rd invisible antenna receiving step five, second instruction control module opens second switch, while the end face figure like of the optical cable wire harness assembly connector collected in step 4 is sent to the second instruction control module by image acquisition device；Step 7: the data processor of data processing equipment 1 receives the end face figure like data for the optical cable wire harness assembly connector that the second instruction control module is sent by the first invisible antenna；Step 8: as shown in Figure 5, the end face figure like data of optical cable wire harness assembly connector of the data processor of data processing equipment 1 to receiving carry out hot spot gray proces, using brightness and the light intensity table of comparisons, the order descending according to hot spot gradation data, hot spot gradation data is converted to the conduction light intensity levels data of optical cable wire harness assembly connection optical fiber successively；Step 9: optical cable wire harness assembly is connected the conduction light intensity levels data transfer of optical fiber to display module by the data processor of data processing equipment, data are completed to show with image, simultaneously using the working condition of different colours nominal light cable tread assembly interface channel, red is failure, and green is normal.
After the present invention, it is possible to achieve synchronize detection to all signalling channels of airborne optical cable wire harness assembly, simplify the operating process of airborne optical cable wire harness assembly inspection, improve the efficiency for checking work.
Exemplified as above is only that the same or analogous design of the every and present invention is belonged within protection scope of the present invention for example, not forming the limitation to protection scope of the present invention to of the invention.
Claims (8)
- A kind of 1. optical cable wire harness assembly connecting fault check device, it is characterised in that：Including data processing equipment（1）, transmitting photocontrol module（2）, image capture module（3）；The transmitting photocontrol module（2）Pass through the first connection camera bellows（4）It is connected with the connector at optical cable wire harness assembly A ends；Described image acquisition module（3）Pass through the second connection camera bellows（5）It is connected with the connector at optical cable wire harness assembly B ends；The data processing equipment（1）By communication module to transmitting photocontrol module（2）, image capture module（3）Send remote control commands.
- A kind of 2. optical cable wire harness assembly connecting fault check device according to claim 1, it is characterised in that：The data processing equipment（1）Including the first invisible antenna, data processor, the display module being sequentially connected by data/address bus.
- A kind of 3. optical cable wire harness assembly connecting fault check device according to claim 2, it is characterised in that：The display module is data and image display.
- A kind of 4. optical cable wire harness assembly connecting fault check device according to claim 1, it is characterised in that：The transmitting photocontrol module（2）Including the second invisible antenna, the first instruction control module, first switch, LED light source, the first connection camera bellows being sequentially connected by control line（4）, and the first instruction control module, first switch, LED light source are connected with the first battery.
- A kind of 5. optical cable wire harness assembly connecting fault check device according to claim 1, it is characterised in that：Described image acquisition module（3）Including the 3rd invisible antenna, the second instruction control module, second switch, image acquisition device, the second connection camera bellows being sequentially connected by control line（5）, and the second instruction control module, second switch, image acquisition device are connected with the second battery.
- A kind of 6. optical cable wire harness assembly connecting fault check device according to claim 1, it is characterised in that：The first connection camera bellows（4）Connector with optical cable wire harness assembly A ends, described second are connected camera bellows（5）Threadedly it is connected with the connector at optical cable wire harness assembly B ends.
- A kind of 7. optical cable wire harness assembly connecting fault check device according to claim 1, it is characterised in that：The communication module is wireless WIFI Module.
- A kind of 8. optical cable wire harness assembly connecting fault inspection method, it is characterised in that：Specifically comprise the following steps：Step 1: data processing equipment（1）Data processor pass through the first invisible antenna send start LED light sourse instruction；Step 2: transmitting photocontrol module（2）The first instruction control module pass through the startup LED light sourse instruction in the second invisible antenna receiving step one, the first instruction control module start first switch, open LED light source；Step 3: data processing equipment（1）Data processor pass through the first invisible antenna send start image capture instruction；Step 4: image capture module（3）The second instruction control module pass through the startup image capture instruction in the 3rd invisible antenna receiving step three, second instruction control module opens second switch, and image capture instruction will be started and be sent to image acquisition device, and then image acquisition device starts to gather the end face figure like of optical cable wire harness assembly connector；Step 5: data processing equipment（1）Data processor pass through the first invisible antenna send start image send instruction；Step 6: image capture module（3）The second instruction control module instruction is sent by startup image in the 3rd invisible antenna receiving step five, second instruction control module opens second switch, while the end face figure like of the optical cable wire harness assembly connector collected in step 4 is sent to the second instruction control module by image acquisition device；Step 7: data processing equipment（1）Data processor pass through the first invisible antenna receive the second instruction control module send optical cable wire harness assembly connector end face figure like data；Step 8: data processing equipment（1）Data processor hot spot gray proces, and the order descending according to hot spot gradation data are carried out to the end face figure like data of optical cable wire harness assembly connector received, be converted to the conduction light intensity levels data of optical cable wire harness assembly connection optical fiber successively；Step 9: data processing equipment（1）Data processor optical cable wire harness assembly is connected into optical fiber conduction light intensity levels data transfer to display module, complete data and show with image, while the working condition of use different colours nominal light cable tread assembly interface channel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610314630.5A CN107367373A (en) | 2016-05-13 | 2016-05-13 | A kind of optical cable wire harness assembly connecting fault check device and inspection method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610314630.5A CN107367373A (en) | 2016-05-13 | 2016-05-13 | A kind of optical cable wire harness assembly connecting fault check device and inspection method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107367373A true CN107367373A (en) | 2017-11-21 |
Family
ID=60304414
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610314630.5A Pending CN107367373A (en) | 2016-05-13 | 2016-05-13 | A kind of optical cable wire harness assembly connecting fault check device and inspection method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107367373A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS63108243A (en) * | 1986-10-24 | 1988-05-13 | Nippon Telegr & Teleph Corp <Ntt> | Inspecting method for freaking of optical fiber cable |
| JP2005241398A (en) * | 2004-02-26 | 2005-09-08 | Fujikura Ltd | Test method for optical fiber connector end face |
| CN1938580A (en) * | 2004-03-30 | 2007-03-28 | 富士胶片株式会社 | Apparatus and method for detecting defect in optical fiber, and plastic optical fiber manufacturing apparatus |
| CN102047162A (en) * | 2008-05-29 | 2011-05-04 | 泛达公司 | Method and apparatus for verifying the termination quality of an optical fiber interface in a fiber optic cable connector |
| CN204535958U (en) * | 2014-11-14 | 2015-08-05 | 深圳市亚派光电器件有限公司 | Fiber end inspection Apparatus and system |
| CN104897370A (en) * | 2015-05-27 | 2015-09-09 | 广东高聚激光有限公司 | Fiber welding quality monitoring method and system |
-
2016
- 2016-05-13 CN CN201610314630.5A patent/CN107367373A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS63108243A (en) * | 1986-10-24 | 1988-05-13 | Nippon Telegr & Teleph Corp <Ntt> | Inspecting method for freaking of optical fiber cable |
| JP2005241398A (en) * | 2004-02-26 | 2005-09-08 | Fujikura Ltd | Test method for optical fiber connector end face |
| CN1938580A (en) * | 2004-03-30 | 2007-03-28 | 富士胶片株式会社 | Apparatus and method for detecting defect in optical fiber, and plastic optical fiber manufacturing apparatus |
| CN102047162A (en) * | 2008-05-29 | 2011-05-04 | 泛达公司 | Method and apparatus for verifying the termination quality of an optical fiber interface in a fiber optic cable connector |
| CN204535958U (en) * | 2014-11-14 | 2015-08-05 | 深圳市亚派光电器件有限公司 | Fiber end inspection Apparatus and system |
| CN104897370A (en) * | 2015-05-27 | 2015-09-09 | 广东高聚激光有限公司 | Fiber welding quality monitoring method and system |
Non-Patent Citations (4)
| Title |
|---|
| 席庆奎等: "基于图像处理的光纤测量方法研究", 《半导体光电》 * |
| 沈亚强等: "基于数字全息显微术的光纤连接器端面形貌检测技术", 《浙江师范大学学报（自然科学版）》 * |
| 赵伟杰等: "机器视觉在光纤端面缺陷检测中的应用", 《现代电子技术》 * |
| 赵新彦等: "光纤端面参数自动化测量系统的研究", 《光学仪器》 * |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104853503B (en) | The collection system and lamp control system of light fixture operating state data | |
| CN106829668B (en) | A kind of elevator long distance adjustment method and device | |
| CN104486146A (en) | Communication method for testing console and testing equipment | |
| CN105680938A (en) | High-definition video fiber transmission self checking method and device | |
| CN104104519B (en) | A kind of power-off restarting method, apparatus and system | |
| CN103840879B (en) | A kind of optical fiber office is to recognition methods, device and system | |
| CN103544104B (en) | Testing method for power distribution terminal remote control functional software module | |
| CN107367373A (en) | A kind of optical cable wire harness assembly connecting fault check device and inspection method | |
| CN108227684A (en) | LED display control system fault monitoring device | |
| CN105388891A (en) | Fault diagnosis device and method for fieldbus system | |
| CN203645747U (en) | Wireless monitoring camera | |
| CN206710860U (en) | Common control equipment | |
| CN102336355A (en) | Elevator monitoring system | |
| CN205384483U (en) | Sewing machine mechanical breakdown report and remote diagnosis system | |
| CN107920230A (en) | Video monitoring image secondary-confirmation system and method | |
| CN110763927A (en) | In-situ equipment debugging method based on wireless communication | |
| CN104021064A (en) | Serial communication data monitoring method | |
| CN207560208U (en) | Coal mine screen monitoring system | |
| CN209070742U (en) | A kind of intelligence wire cable communication transfer traffic light systems | |
| CN202077191U (en) | Judging device for fiber and power failure fault of baseband processing unit-remote radio unit | |
| CN102072772B (en) | Wireless color acquisition system and method of same | |
| CN113050898B (en) | Display screen control method, device, equipment, system and medium | |
| CN105281972B (en) | The comparison acquisition structure and comparison acquisition method of 1553B buses | |
| CN109194556A (en) | A kind of thermal power plant bus redundancy control system | |
| CN109240075A (en) | A kind of thermal power plant bus redundancy control system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171121 |
|
| RJ01 | Rejection of invention patent application after publication |