CN202013207U - Integrated performance testboard for pneumatic accessories of aircraft - Google Patents
Integrated performance testboard for pneumatic accessories of aircraft Download PDFInfo
- Publication number
- CN202013207U CN202013207U CN2011200478320U CN201120047832U CN202013207U CN 202013207 U CN202013207 U CN 202013207U CN 2011200478320 U CN2011200478320 U CN 2011200478320U CN 201120047832 U CN201120047832 U CN 201120047832U CN 202013207 U CN202013207 U CN 202013207U
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- test
- experiment table
- pneumatic accessories
- aircraft
- utility
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Abstract
The utility model discloses an integrated performance testboard for pneumatic accessories of an aircraft. The testboard comprises an experiment table and a control console, wherein the experiment table is provided with an air supply interface and a power interface and is connected with test equipment by the air supply interface and the power interface; and the control console is provided with a digital display meter and an automatic control switch, so as to achieve the integrated test for the equipment performance. The testboard has strong integration of the equipment, integrates all pneumatic accessories detection equipment into one and has the advantages that the connection is simple, and the operation is easy.
Description
Technical field
The utility model relates to the aircraft system parts, particularly aircraft pneumatic accessories combination property test desk.
Background technology
Present most of performance test bed function ratio is limitation, generally can only carry out a certain performance test, if carry out other performance test, then need to change in addition a test board, very inconvenience is wasted time and energy, and it is more to make the test board repeatability parts of each different performance, the waste resource, the cost cost is also high.
The utility model content
In order to overcome the defective that above-mentioned prior art exists, the utility model provides a kind of aircraft pneumatic accessories combination property test desk, and multiple performance test can be provided, and has remedied the defective that the general test platform can only carry out a certain functional test.
To achieve these goals, the technical solution of the utility model is as follows:
Aircraft pneumatic accessories combination property test desk comprises experiment table and control desk, and gas source interface and power interface are set on the described experiment table, connects testing apparatus by described gas source interface and power interface; Digital display meter and automatic control switch are set on the described control desk, can realize full test equipment performance;
Further, hand control switch and pointer indicator gauge being set also on the described experiment table, also can realizing full test to equipment by described hand control switch and pointer indicator gauge, is the another kind of manual adjustments mode of above-mentioned automatic control.
Further, described experiment table also can connect the butterfly valve position indicator, makes people observe the residing state of test board more intuitively, reduces maloperation.
This test board is mainly with doing to provide test required source of the gas and power supply to measured piece, this equipment can provide pressure test, pressure reduction test, flow rate test, seepage test, vacuum pressure test, pressure rate test, air themperature test, angular displacement angle measurement, straight-line displacement test, low pressure/alarm for high voltage functional test, comparing its function of former test board increases greatly, more comprehensive, test more accurately and reliably.
The beneficial effects of the utility model are:
Equipment complex is strong, integrated all pneumatic accessories checkout equipments in one, had simple, the easy to operate advantage of connection, can carry out the manual adjustments test according to the measured piece actual needs and test flexible conversion with regulating automatically, greatly facilitate operational testing, increase work efficiency.
Description of drawings
Fig. 1 is a structured flowchart of the present utility model.
Embodiment
Be easy to understand understanding in order to make creation characteristic of the present utility model, technological means and to reach purpose, further set forth the utility model below in conjunction with specific embodiment.
Embodiment:
Referring to Fig. 1, aircraft pneumatic accessories combination property test desk comprises experiment table 1 and control desk 2, and gas source interface 11 and power interface 12 are set on the described experiment table 1, connects testing apparatus 3 by described gas source interface 11 and power interface 12;
Experiment table 1 also can connect butterfly valve position indicator 4, makes people observe the residing state of test board more intuitively, reduces maloperation.
Above-mentioned test board is mainly with doing to provide test required source of the gas and power supply to measured piece, and can provide pressure test, pressure reduction test, flow rate test, seepage test, vacuum pressure test, pressure rate test, air themperature test, angular displacement angle measurement, straight-line displacement test, low pressure/alarm for high voltage functional test, comparing its function of former test board increases greatly, more comprehensive, test more accurately and reliably.
More than show and described ultimate principle of the present utility model, principal character and advantage of the present utility model.The technician of the industry should understand; the utility model is not restricted to the described embodiments; that describes in the foregoing description and the instructions just illustrates principle of the present utility model; the utility model also has various changes and modifications under the prerequisite that does not break away from the utility model spirit and scope, and these changes and improvements all fall in claimed the utility model scope.The claimed scope of the utility model is defined by appending claims and equivalent thereof.
Claims (3)
1. aircraft pneumatic accessories combination property test desk is characterized in that, it comprises experiment table and control desk, and gas source interface and power interface are set on the described experiment table, connects testing apparatus by described gas source interface and power interface; Digital display meter and automatic control switch are set on the described control desk.
2. aircraft pneumatic accessories combination property test desk according to claim 1 is characterized in that, hand control switch and pointer indicator gauge also are set on the described experiment table.
3. aircraft pneumatic accessories combination property test desk according to claim 1 is characterized in that described experiment table also can connect the butterfly valve position indicator.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200478320U CN202013207U (en) | 2011-02-18 | 2011-02-18 | Integrated performance testboard for pneumatic accessories of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200478320U CN202013207U (en) | 2011-02-18 | 2011-02-18 | Integrated performance testboard for pneumatic accessories of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202013207U true CN202013207U (en) | 2011-10-19 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011200478320U Expired - Fee Related CN202013207U (en) | 2011-02-18 | 2011-02-18 | Integrated performance testboard for pneumatic accessories of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202013207U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105091834A (en) * | 2014-05-07 | 2015-11-25 | 哈尔滨飞机工业集团有限责任公司 | Position indicator tester |
| CN107575437A (en) * | 2017-11-01 | 2018-01-12 | 燕山大学 | A kind of aerospace hydraulic pump and fluid pressure line performance test experiment table |
| CN109099963A (en) * | 2018-07-04 | 2018-12-28 | 中国航天员科研训练中心 | A kind of multrirange multi output pneumatic control detection device |
-
2011
- 2011-02-18 CN CN2011200478320U patent/CN202013207U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105091834A (en) * | 2014-05-07 | 2015-11-25 | 哈尔滨飞机工业集团有限责任公司 | Position indicator tester |
| CN107575437A (en) * | 2017-11-01 | 2018-01-12 | 燕山大学 | A kind of aerospace hydraulic pump and fluid pressure line performance test experiment table |
| CN109099963A (en) * | 2018-07-04 | 2018-12-28 | 中国航天员科研训练中心 | A kind of multrirange multi output pneumatic control detection device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20111019 Termination date: 20140218 |