CN205080214U - Electric general test equipment of aviation - Google Patents
Electric general test equipment of aviation Download PDFInfo
- Publication number
- CN205080214U CN205080214U CN201520871887.1U CN201520871887U CN205080214U CN 205080214 U CN205080214 U CN 205080214U CN 201520871887 U CN201520871887 U CN 201520871887U CN 205080214 U CN205080214 U CN 205080214U
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- test equipment
- cabinet
- rear panel
- quick
- board
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Abstract
The utility model provides an electric general test equipment of aviation, includes quick -witted case, and the integrated circuit board is nursed one's health to the quick -witted incasement rear panel upper portion installation back of the body formula of inserting, and the department is provided with the business turn over cable plug under the rear panel, and the piece that awaits measuring passes through business turn over cable connector assembly to quick -witted incasement, and the case front panel is provided with monitoring hole relevant with test procedure or status indicator lamp, gasket -mounted separated time terminal row, the utility model discloses with same system architecture design, satisfy different kinds of test equipment's function. System architecture is the same, and framework diversification the design of non - standard device is united, and convenient and fast is built to the framework.
Description
Technical field
The utility model belongs to design and the operation technique field of aircraft electric general purpose test equipment, particularly a kind of aircraft electric general purpose test equipment.
Background technology
Present mainstream technology is all automation equipments of the non-standard class according to customer demand customization, and function measures the automated test device of body design, customization.The design of non-standard equipment is Theoretical Design, how does not attractive in appearancely require, only takes notice of simple content with funtion.So cause the project of different testing requirement need design its corresponding non-standard equipment, there is no unified structure, there is no unified system, there is no unified cabling mode.Different people designs different structures, and the different System level gray correlation opposite sex is larger
Summary of the invention
In order to overcome the shortcoming of above-mentioned prior art, the purpose of this utility model is to provide a kind of aircraft electric general purpose test equipment, system architecture is simple, applicable multiple aircraft electric testing apparatus project, emulation, conditioning, monitoring and cabling complete in a structure cabinet, solve the problem that framework is loaded down with trivial details, improve testing efficiency.
To achieve these goals, the technical solution adopted in the utility model is:
A kind of aircraft electric general purpose test equipment, comprise cabinet, in cabinet, rear panel top is installed the back of the body and is inserted formula conditioning board 1, rear panel lower gate is provided with turnover cable plug 2, be connected in cabinet by turnover cable plug 2 for be measured 5, case front panel is provided with the monitoring holes relevant with test process or status indicator lamp 4, and base plate installs line branch terminal row 3.
Described cabinet is standard 9U cabinet, and its front panel is 9U blind plate, and it is 6U or 3U board that the described back of the body inserts formula conditioning board 1.
Compared with prior art, the beneficial effects of the utility model are: design by same system architecture, meet the function of dissimilar testing apparatus.The identical framework versatile union non-standard equipment design of system architecture gets up, and framework is built convenient and swift.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation.
Embodiment
Embodiment of the present utility model is described in detail below in conjunction with drawings and Examples.
As shown in Figure 1, a kind of aircraft electric general purpose test equipment, comprise cabinet, in cabinet, rear panel top is installed the back of the body and is inserted formula conditioning board 1, rear panel lower gate is provided with turnover cable plug 2, be connected in cabinet by turnover cable plug 2 for be measured 5, case front panel is provided with the monitoring holes relevant with test process or status indicator lamp 4, and base plate installs line branch terminal row 3.Cabinet is standard 9U cabinet, and its front panel is 9U blind plate, and it is 6U or 3U board that the back of the body inserts formula conditioning board 1.
Major part of the present utility model is as follows respectively:
Part I, front panel
Front panel is 9U blind plate, and the perforate on blind plate and lettering can require different designs according to different nonstandard Project design.Monitoring, display, self-inspection region can be distinguished by piecemeal lettering, monitored area can be detected some signal in system in design test hole in real time, viewing area can show the quantity of state lamp in system, and self-inspection region can design self-inspection button or status indicator lamp 4 is system self-checking function.
Part II, the back of the body inserts formula conditioning board 1
It is 6U or 3U board that the back of the body inserts formula conditioning board 1, according to the designing requirement of the nonstandard project of difference, designs the boards such as different conditionings, control, emulation.Board be designed to backboard plug-in, mounting kit selection standard guide rail and standard drawing-aid device, can also perforate directly be connected with the board 6 of industrial computer 7 on drawing-aid device simultaneously, control the back of the body by industrial computer 7 and board 6 and insert formula conditioning board 1, board 6 below link can select European plugs connection signal, can be connected to the front panel of cabinet, rear panel plug, line branch terminal row 3 etc.
Part III, turnover cable plug 2
This part mainly completes and outside linkage function, the signal entered can be had also can to have the signal of going out, outside can be connected directly to measured piece, is connected internally to that front panel carries out monitoring, shows, self-inspection, or enters to carry out nursing one's health or emulating to standard 6U or 3U board.
Part IV, line branch terminal row 3
This part can be used as common ground or the point in common-battery source, can be standard 6U or 3U board and provides power supply and altogether.
Claims (2)
1. an aircraft electric general purpose test equipment, comprise cabinet, it is characterized in that, in cabinet, rear panel top is installed the back of the body and is inserted formula conditioning board (1), rear panel lower gate is provided with turnover cable plug (2), to be measured (5) are connected in cabinet by turnover cable plug (2), and case front panel is provided with the monitoring holes relevant with test process or status indicator lamp (4), and base plate installs line branch terminal row (3).
2. aircraft electric general purpose test equipment according to claim 1, it is characterized in that, described cabinet is standard 9U cabinet, and its front panel is 9U blind plate, and it is 6U or 3U board that the described back of the body inserts formula conditioning board (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520871887.1U CN205080214U (en) | 2015-11-04 | 2015-11-04 | Electric general test equipment of aviation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520871887.1U CN205080214U (en) | 2015-11-04 | 2015-11-04 | Electric general test equipment of aviation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205080214U true CN205080214U (en) | 2016-03-09 |
Family
ID=55432612
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520871887.1U Active CN205080214U (en) | 2015-11-04 | 2015-11-04 | Electric general test equipment of aviation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205080214U (en) |
-
2015
- 2015-11-04 CN CN201520871887.1U patent/CN205080214U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |