CN204347183U - The online switching test device of General Aviation plug - Google Patents
The online switching test device of General Aviation plug Download PDFInfo
- Publication number
- CN204347183U CN204347183U CN201420803869.5U CN201420803869U CN204347183U CN 204347183 U CN204347183 U CN 204347183U CN 201420803869 U CN201420803869 U CN 201420803869U CN 204347183 U CN204347183 U CN 204347183U
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- test
- aviation plug
- torus
- test chamber
- casing
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Abstract
The utility model discloses the online switching test device of a kind of General Aviation plug, comprise test casing, described test casing is provided with control device, there is in described test casing a test chamber and a torus, the both sides of described test chamber are all connected with described torus, and be provided with a circulating fan between described test chamber and described torus, a humidifier is provided with in described torus, the left and right sides of described test chamber is provided with multipair Aviation Connector, described Aviation Connector is for connecting aviation plug to be tested, and described Aviation Connector is connected with control device.The utility model by arranging test chamber for testing aviation plug in test casing, in use, humidifier is by the air wetting in test casing, blower fan drives humid air to circulate between torus and test chamber, simulation wet environment, under control device test wet environment, the working condition of aviation plug, facilitates designer to the inspection of aviation plug moisture resistant environment.
Description
Technical field
The utility model relates to aviation plug technical field of measurement and test, more particularly, and the particularly online switching test device of General Aviation plug.
Background technology
In prior art; aircraft often needs through cumulonimbus layer when flying; the aviation plug that steam electrical equipment more greatly and wherein uses often can contact the larger air of humidity, and in the production and R&D process of aviation plug, just need a kind of working condition of the aviation plug can simulated in the larger situation of humidity.
Utility model content
The purpose of this utility model is to provide a kind of online switching test device of General Aviation plug can simulated in the larger situation of humidity.
In order to achieve the above object, the technical solution adopted in the utility model is as follows:
The online switching test device of a kind of General Aviation plug, comprise test casing, described test casing is provided with control device, there is in described test casing a test chamber and a torus, the both sides of described test chamber are all connected with described torus, and be provided with a circulating fan between described test chamber and described torus, a humidifier is provided with in described torus, the left and right sides of described test chamber is provided with multipair Aviation Connector, described Aviation Connector is for connecting aviation plug to be tested, and described Aviation Connector is connected with control device.
Further, also heating arrangement is provided with bottom described test chamber.
Further, each described Aviation Connector is all located at one independently in annular seal space, and all by a gas-tight silo door sealing between each described annular seal space and described test chamber.
Further, described humidifier is installed on test box body sidewall, and described test box body sidewall is also provided with a water tank, and described water tank is connected with described humidifier.
Further, the test casing being positioned at test chamber place is provided with a test door.
Compared with prior art, the utility model has the advantage of: by arranging test chamber for testing aviation plug in test casing, in use, humidifier is by the air wetting in test casing, blower fan drives humid air to circulate between torus and test chamber, simulation wet environment, under control device test wet environment, the working condition of aviation plug, facilitates designer to the inspection of aviation plug moisture resistant environment.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation of the online switching test device of General Aviation plug described in the utility model;
Fig. 2 is the inner structure schematic diagram of the online switching test device of General Aviation plug described in the utility model;
Fig. 3 is the inner structure schematic diagram of General Aviation plug described in the utility model online switching test device when using.
Embodiment
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described in detail, to make advantage of the present utility model and feature can be easier to be readily appreciated by one skilled in the art, thus more explicit defining is made to protection domain of the present utility model.
Consult shown in Fig. 1 to Fig. 3, the utility model provides a kind of General Aviation plug online switching test device, it is characterized in that: comprise test casing 1, test casing 1 is provided with control device 2, in test casing 1, there is test chamber 11 and a torus 12, the both sides of test chamber 11 are all connected with torus 12 and jointly form a passage circulated, and between test chamber 11 and torus 12, be provided with a circulating fan 3, a humidifier 4 is provided with for humidifying air in torus 12, the left and right sides of test chamber 11 is provided with the Aviation Connector 5 of multipair different model, Aviation Connector 5 is for connecting aviation plug 6 to be tested, Aviation Connector 5 is connected with control device 2.By arranging test chamber 11 for testing aviation plug 6 in test casing 1, in use, humidifier 4 is by the air wetting in test casing 1, circulating fan 3 drives humid air to circulate between torus 12 and test chamber 11, simulation wet environment, the working condition of aviation plug 6 under wet environment tested by control device 2, facilitates designer to the inspection of aviation plug 6 moisture resistant environment.
In the present embodiment, heating arrangement 7 is also provided with bottom test chamber 11.Need to dry in test casing 1 after having tested at proving installation, prevent the electronic component tested in casing 1 to be in steam for a long time and lost efficacy.
Each Aviation Connector 5 is all located at one independently in annular seal space 13, and all seals door 8 by one between each annular seal space 13 and test chamber 11 and seal.When needing the aviation plug 6 testing certain model, only need open the sealing door 8 of corresponding Aviation Connector 5, the Aviation Connector 5 of other models can not touch aqueous vapor, Aviation Connector 5 long service life of each model.
Humidifier 4 is installed on test casing 1 sidewall in torus 12, and test casing 1 sidewall is also provided with a water tank 9, and water tank 9 is connected with humidifier 4.Water tank 9 can be humidifier 4 moisturizing at any time, and on test casing 1 sidewall, also offers a filler be connected with water tank 9 conveniently add water.The test casing 1 being positioned at test chamber 11 place is provided with a test door 10.Permitted test chamber 11 due to test door 10 to be connected, conveniently aviation plug 6 to be tested be installed into test chamber 11 or take out from test chamber 11.
Although describe embodiment of the present utility model by reference to the accompanying drawings; but patent owner can make various distortion or amendment within the scope of the appended claims; as long as be no more than the protection domain described by claim of the present utility model, all should within protection domain of the present utility model.
Claims (5)
1. the online switching test device of General Aviation plug, it is characterized in that: comprise test casing (1), described test casing (1) is provided with control device (2), there is in described test casing (1) test chamber (11) and a torus (12), the both sides of described test chamber (11) are all connected with described torus (12), and be provided with a circulating fan (3) between described test chamber (11) and described torus (12), a humidifier (4) is provided with in described torus (12), the left and right sides of described test chamber (11) is provided with multipair Aviation Connector (5), described Aviation Connector (5) is for connecting aviation plug to be tested (6), described Aviation Connector (5) is connected with control device (2).
2. the online switching test device of General Aviation plug according to claim 1, is characterized in that: described test chamber (11) bottom is also provided with heating arrangement (7).
3. the online switching test device of General Aviation plug according to claim 2, it is characterized in that: each described Aviation Connector (5) is all located at one independently in annular seal space (13), and all seal door (8) by one between each described annular seal space (13) and described test chamber (11) and seal.
4. the online switching test device of General Aviation plug according to claim 3, it is characterized in that: described humidifier (4) is installed on test casing (1) sidewall, and described test casing (1) sidewall is also provided with a water tank (9), described water tank (9) is connected with described humidifier (4).
5. the online switching test device of General Aviation plug according to claim 4, is characterized in that: the test casing (1) being positioned at test chamber (11) place is provided with a test door (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420803869.5U CN204347183U (en) | 2014-12-17 | 2014-12-17 | The online switching test device of General Aviation plug |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420803869.5U CN204347183U (en) | 2014-12-17 | 2014-12-17 | The online switching test device of General Aviation plug |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204347183U true CN204347183U (en) | 2015-05-20 |
Family
ID=53230444
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420803869.5U Expired - Fee Related CN204347183U (en) | 2014-12-17 | 2014-12-17 | The online switching test device of General Aviation plug |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204347183U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106019146A (en) * | 2016-08-12 | 2016-10-12 | 国网山东省电力公司日照供电公司 | Circuit breaker action characteristic experiment device and method |
| CN107860586A (en) * | 2017-10-17 | 2018-03-30 | 柳州裕信方盛汽车饰件有限公司 | Passenger car instrument desk module electric-examination adapting fixture |
| CN111866496A (en) * | 2020-07-17 | 2020-10-30 | 浙江鸿泉电子科技有限公司 | Aviation head test system |
-
2014
- 2014-12-17 CN CN201420803869.5U patent/CN204347183U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106019146A (en) * | 2016-08-12 | 2016-10-12 | 国网山东省电力公司日照供电公司 | Circuit breaker action characteristic experiment device and method |
| CN107860586A (en) * | 2017-10-17 | 2018-03-30 | 柳州裕信方盛汽车饰件有限公司 | Passenger car instrument desk module electric-examination adapting fixture |
| CN111866496A (en) * | 2020-07-17 | 2020-10-30 | 浙江鸿泉电子科技有限公司 | Aviation head test system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150520 Termination date: 20151217 |
|
| EXPY | Termination of patent right or utility model |