CN106342410B - Radio system comprehensive detection device - Google Patents
Radio system comprehensive detection deviceInfo
- Publication number
- CN106342410B CN106342410B CN200610120590.7A CN200610120590A CN106342410B CN 106342410 B CN106342410 B CN 106342410B CN 200610120590 A CN200610120590 A CN 200610120590A CN 106342410 B CN106342410 B CN 106342410B
- Authority
- CN
- China
- Prior art keywords
- aircraft
- control cabinet
- radio system
- wireless device
- cable
- 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.)
- Expired - Fee Related
Links
- 238000001514 detection method Methods 0.000 title claims abstract description 15
- 238000004088 simulation Methods 0.000 claims abstract description 5
- 238000009434 installation Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000013024 troubleshooting Methods 0.000 description 1
Landscapes
- Monitoring And Testing Of Transmission In General (AREA)
Abstract
The present invention relates to a kind of checkout gear of aircraft radio system, mainly formed by stube cable and detection control cabinet. Connection cable and detection control cabinet are to make by radio system line simulation on aircraft, detect different wireless device simulations produce different connection cables according to need. In the time that on aircraft, radio system has fault, circuit on wireless device and aircraft is disconnected, use cable that corresponding tested equipment is connected with display lamp with detection change-over switch, logical upper working power, whether display lamp just can indicate without equipment work normal. Correctly judging is the fault of circuit on equipment or aircraft.
Description
Affiliated technical field
The present invention relates to the checkout equipment of aircraft radio system, specifically aircraft radio system lineComprehensive detection device with the fault detect of airborne radio installation.
Background technology
For a long time, in Aircraft Production and ground service maintenance, the ground check after the installation of airborne wireless electric systemWork is all to utilize relevant gauge tap, display lamp (or instrument) in aircraft cockpit, and aircraft circuit and machineThe common work of the equipment of carrying is carried out. Though this mode is simple, once system break down, owing to flyingThe limitation of machine structure, each equipment of same system often can not be installed on same position, and sameEach equipment that install at position often belongs to again different systems, and searching of fault is difficult very large, oftenTo expend much more very time and efforts all can not to determine the end be that aircraft line fault or equipment are originally dieBarrier, the fault that has a strong impact on aircraft is got rid of, and bungles the chance of winning a battle, and causes immeasurable loss.
Summary of the invention
The technical problem solving:
In order to solve the fault detect difficulty causing due to the limitation of aircaft configuration, shorten investigation fault timeBetween the cycle, the invention provides a kind of simulated aircraft radio system circuit, can fast detecting failure judgement portionThe comprehensive detection device of position.
Technical scheme:
Technical scheme of the present invention is achieved in that by radio system line simulation designed lines on aircraftStube cable and detect control cabinet, cable two ends are provided with and are connected with wireless device and detect control cabinet connectionPlug. Detect the different connection cables of different wireless device board designs and plug according to need. DetectControl cabinet is provided with and detects different wireless device change-over switch, socket, display lamp, and is provided with to meet on machine and suppliesThe power supply that electricity requires. In the time that on aircraft, radio system has fault, by breakage of circuit on wireless device and aircraftOpen, use respective cable that tested wireless device is connected with display lamp with detection control cabinet change-over switch, lead toWorking power, display lamp just can represent that whether wireless device work is normal. Correctly judge is that radio is establishedOn standby or aircraft, circuit has fault.
Beneficial effect:
The present invention can judge the function of radio system trouble location quickly and accurately, is specially adapted to aircraftProduce and ground service maintenance, can shorten the cycle of aircraft troubleshooting, enhance productivity and the aircraft rate of attendance, haveStronger practicality. Overall structure is simple, cost is low; Easy for operation, safe and reliable.
Brief description of the drawings
Accompanying drawing drawing of the present invention is described as follows:
Fig. 1 is overall structure schematic diagram of the present invention.
1. sockets in figure, 2. cable, 3. plug, 4. radio station transceiver, 5. compass receiver,6. altimeter transceiver, 7. beacon receiver, 8. detects control cabinet, 9. display lamp, 10. change-over switch.
Detailed description of the invention
Below in conjunction with accompanying drawing and embodiment, the invention will be further described.
As shown in Figure 1, the present invention is mainly made up of stube cable and detection control cabinet. Cable 2 two ends are provided withPlug 3 is connected with wireless device and the socket 1 that detects control cabinet 8 connects. By radio station transceiver 4, compassThe different line simulations of receiver 5, altimeter transceiver 6 and beacon receiver 7 are designed with different connection electricityCable 2 and plug 3. Detect in control cabinet 8 and be provided with change-over switch 10 and display lamp 9,10 liang of change-over switchesEnd is connected with power supply and socket 1 respectively, display lamp 9 by cable and radio station transceiver 4, compass receiver 5,Altimeter transceiver 6 or beacon receiver 7 join. When the radio station transceiver 4 on aircraft, compass receiver 5,Altimeter transceiver 6 or beacon receiver 7 break down, and first circuit on aircraft are disconnected, with corresponding electricityCable 2 connects detection control cabinet 8 and radio station transceiver 4, compass receiver 5, altimeter transceiver 6 or beaconReceipts machine 7 with detect the socket 1 of control cabinet 8 and be connected, display lamp 9 and radio station transceiver 4, compass receiver 5,Altimeter transceiver 6 or beacon receiver 7 join, logical upper working power, tested radio station transceiver 4, compassReceiver 5, altimeter transceiver 6 or beacon receiver 7 are started working, and working condition feeds back to display lamp 9,Display lamp 9 is bright working properly with regard to indication equipment, and should be aircraft circuit has fault, if display lamp 9 does not work, and shouldFor equipment itself has fault.
Claims (2)
1. a radio system comprehensive detection device, is mainly made up of stube cable and detection control cabinet, itsBe characterised in that: cable (2) two ends are provided with the plug (3) that is connected with wireless device and detects control cabinet connection,Detect in control cabinet (8) and be provided with change-over switch (10) and display lamp (9), change-over switch (10) two ends are dividedBe not connected with power supply and socket (1); Described cable (2) and detection control cabinet (8) are according to nothing on aircraftLine electric system line simulation design, in the time that on aircraft, radio system has fault, by wireless device with flyOn machine, circuit disconnects, and with described cable (2) connection wireless device and described detection control cabinet (8), connectsWorking power, judges that by the instruction of described display lamp (9) on wireless device or aircraft, circuit has eventBarrier.
2. radio system comprehensive detection device according to claim 1, is characterized in that: receive by radio stationSend out machine (4), compass receiver (5), altimeter transceiver (6) and the different circuits of beacon receiver (7)Be designed with different stube cable (2) and plug (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200610120590.7A CN106342410B (en) | 2006-11-30 | 2006-11-30 | Radio system comprehensive detection device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN200610120590.7A CN106342410B (en) | 2006-11-30 | 2006-11-30 | Radio system comprehensive detection device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106342410B true CN106342410B (en) | 2010-11-10 |
Family
ID=57797768
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200610120590.7A Expired - Fee Related CN106342410B (en) | 2006-11-30 | 2006-11-30 | Radio system comprehensive detection device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106342410B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110187648A (en) * | 2019-06-03 | 2019-08-30 | 西安飞机工业（集团）有限责任公司 | A kind of Aircraft radio system integrated emulation simulated testing system |
| CN110906917A (en) * | 2019-12-19 | 2020-03-24 | 中航贵州飞机有限责任公司 | Test inspection method on multipurpose airplane radio compass |
-
2006
- 2006-11-30 CN CN200610120590.7A patent/CN106342410B/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110187648A (en) * | 2019-06-03 | 2019-08-30 | 西安飞机工业（集团）有限责任公司 | A kind of Aircraft radio system integrated emulation simulated testing system |
| CN110906917A (en) * | 2019-12-19 | 2020-03-24 | 中航贵州飞机有限责任公司 | Test inspection method on multipurpose airplane radio compass |
| CN110906917B (en) * | 2019-12-19 | 2022-09-16 | 中航贵州飞机有限责任公司 | Test inspection method on multipurpose airplane radio compass |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR03 | Grant of secret patent right | ||
| DC01 | Secret patent status has been lifted | ||
| DCSP | Declassification of secret patent | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101110 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |