CN205079789U - Aviation test platform equipment - Google Patents
Aviation test platform equipment Download PDFInfo
- Publication number
- CN205079789U CN205079789U CN201520871888.6U CN201520871888U CN205079789U CN 205079789 U CN205079789 U CN 205079789U CN 201520871888 U CN201520871888 U CN 201520871888U CN 205079789 U CN205079789 U CN 205079789U
- Authority
- CN
- China
- Prior art keywords
- board
- circuit board
- integrated circuit
- signal
- excitation
- 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.)
- Active
Links
Abstract
The utility model provides an aviation test platform equipment, includes: the excitation computer is installed the excitation and is sent DAIO integrated circuit board, switching value integrated circuit board, electric current integrated circuit board and become the signal integrated circuit board soon, signal after carrying out signal simulation and providing the simulation in it, detect the computer, install universal meter integrated circuit board, oscillograph integrated circuit board and AD integrated circuit board in it, carry out signal verification and measured piece output signal and detect, still can include: the host computer passes through bus communication with the measured piece and realizes direct data interchange, with excitation computer and detection computer link are to its send instruction, the beneficial effects of the utility model are that: system's framework is clear and definite, detects, encourages separately control, host computer unified management allotment. Detecting and encouraging the function to change according to the demand, the test resource can be accomplished according to change adaptation case, and the platform still can be used as non standard equipment's development simultaneously.
Description
Technical field
The utility model belongs to the exploitation of aeronautic measurement equipment, design and operation technique field, particularly a kind of aeronautic measurement platform device.
Background technology
Present mainstream technology is the automation equipment of the non-standard class according to customer demand customization, and different equipment needs to redesign, and the construction cycle is long, stability is not high enough, test covering scope is inadequate.It is comparatively large that test equipment designs completes post debugging workload to production, and the function of design needs checking for a long time.A set of aeronautic measurement equipment only can test the fixing measured piece of a measured piece or a certain class, and new measured piece need do new testing apparatus have been come.
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 aeronautic measurement platform device, can develop different nonstandard testing apparatuss in identical platform.Board on excitation computing machine and detection computations machine can unrestricted choice or replacing, ensures the diversification of test resource.
To achieve these goals, the technical solution adopted in the utility model is:
A kind of aeronautic measurement platform device, comprising:
Excitation computing machine, is provided with excitation and sends D/AIO board, switching value board, electric current board and revolve varying signal board in it, carry out signal imitation and signal after providing simulation;
Detection computations machine, is provided with multimeter board, oscillograph board and A/D board in it, carry out signal authentication and the detection of measured piece output signal.
The utility model also comprises:
Host computer, realizes direct exchanges data with measured piece by bus communication, is connected sends instruction to it with described excitation computing machine and detection computations machine.
Described each board is directly connected with conditioning cabinet and adaptive cabinet, completes the conditioning to pumping signal and display, or connects measured piece through adaptive cabinet.
Compared with prior art, the beneficial effects of the utility model are: system architecture is clear and definite, and detect, encourage separately control, host computer unified management is allocated.Detection and incentive functions can be changed according to demand, and test resource can come according to change adaptive box, and platform also can be used as the exploitation of non-standard equipment simultaneously.
Accompanying drawing explanation
Fig. 1 is the utility model system chart.
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 aeronautic measurement platform device, comprising:
Excitation computing machine, is provided with excitation and sends D/AIO board, switching value board, electric current board and revolve varying signal board in it, carry out signal imitation and signal after providing simulation;
Detection computations machine, is provided with multimeter board, oscillograph board and A/D board in it, carry out signal authentication and the detection of measured piece output signal.
Excitation computing machine provides simulating signal, and detection computations machine realizes detecting according to simulating signal afterwards.
The utility model also can comprise host computer, host computer directly carries out exchanges data as system master equipment and measured piece bus communication, and unify to control, dispatch also and management testing platform task to detection, excitation slave computer, host computer is responsible for the foreground such as man-machine interaction, the issue of slave computer assignment instructions, test data collection, data computing, test data storage simultaneously; Detect, encourage slave computer to be responsible for pressing background work such as the execution of main control computer assignment instructions TT&C task, return data etc., wherein, the measured piece excitation tasks such as signal imitation are responsible for by excitation computing machine, and signal authentication is responsible for by detection computations machine, measured piece output signal detects.The integration test that upper and lower computer coordinates realization relevant with measured piece, measurement and artificial tasks.
Particularly, the utility model test board observing and controlling hardware system is divided into host computer, two slave computer operational modes, and host computer is main control computer, and two slave computers are that PXI encourages computing machine and PXI detection computations machine respectively, are cross-linked between upper and lower computer by network communication.
Epigynous computer section
Host computer directly carries out exchanges data as system master equipment and measured piece bus communication, and unify to control, dispatch also and management testing platform task to detection, excitation slave computer, host computer is responsible for the foreground such as man-machine interaction, the issue of slave computer assignment instructions, test data collection, data computing, test data storage simultaneously
Slave computer part
In detection computations machine, excitation computing machine, excitation is installed to send D/A, IO, switching value, electric current, revolve the boards such as varying signal, in detection computations machine, multimeter board, oscillograph board, A/D board etc. is installed.Slave computer resolves the instruction of host computer transmission according to the procotol of regulation, completes excitation transmission or the signal testing function of command request.Excitation computing machine and detection computations machine board directly with nurse one's health cabinet and adaptive cabinet is connected, complete to the conditioning of pumping signal and display or through adaptive cabinet connection measured piece.
Conditioning cabinet part
The parts nursed one's health are carried out in excitation, detection signal according to different designing requirements, the conditioning of pumping signal and the conditioning of detection signal enter into standard-sized board and nurse one's health, if parameter needs to change, directly the design board of standard of replacement size realizes.
Adaptive cabinet
Adaptive cabinet designs different adaptive cabinets according to different measured pieces, and adaptive cabinet connects different test resources according to different designing requirements from conditioning cabinet or slave computer again.
Above various piece inside all can change replacing, ensures that this platform is used as the exploitation of aeronautic measurement equipment, design and use.
Claims (3)
1. an aeronautic measurement platform device, is characterized in that, comprising:
Excitation computing machine, is provided with excitation and sends D/AIO board, switching value board, electric current board and revolve varying signal board in it, carry out signal imitation and signal after providing simulation;
Detection computations machine, is provided with multimeter board, oscillograph board and A/D board in it, carry out signal authentication and the detection of measured piece output signal.
2. aeronautic measurement platform device according to claim 1, is characterized in that, also comprise:
Host computer, realizes direct exchanges data with measured piece by bus communication, is connected sends instruction to it with described excitation computing machine and detection computations machine.
3. aeronautic measurement platform device according to claim 1, is characterized in that, described each board is directly connected with conditioning cabinet and adaptive cabinet, completes the conditioning to pumping signal and display, or through adaptive cabinet connection measured piece.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520871888.6U CN205079789U (en) | 2015-11-04 | 2015-11-04 | Aviation test platform equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520871888.6U CN205079789U (en) | 2015-11-04 | 2015-11-04 | Aviation test platform equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205079789U true CN205079789U (en) | 2016-03-09 |
Family
ID=55432191
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520871888.6U Active CN205079789U (en) | 2015-11-04 | 2015-11-04 | Aviation test platform equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205079789U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107894760A (en) * | 2017-11-01 | 2018-04-10 | 中国空间技术研究院 | A kind of aerospace component application verification platform based on equivalent excitation test module |
| CN110901950A (en) * | 2019-11-14 | 2020-03-24 | 哈尔滨飞机工业集团有限责任公司 | Automatic detection test platform for helicopter electrical system |
| CN114113820A (en) * | 2021-09-15 | 2022-03-01 | 中国航空工业集团公司西安飞机设计研究所 | Portable detection equipment for outfield of aviation power supply product |
-
2015
- 2015-11-04 CN CN201520871888.6U patent/CN205079789U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107894760A (en) * | 2017-11-01 | 2018-04-10 | 中国空间技术研究院 | A kind of aerospace component application verification platform based on equivalent excitation test module |
| CN107894760B (en) * | 2017-11-01 | 2021-02-09 | 中国空间技术研究院 | Aerospace component application verification platform based on equivalent excitation test module |
| CN110901950A (en) * | 2019-11-14 | 2020-03-24 | 哈尔滨飞机工业集团有限责任公司 | Automatic detection test platform for helicopter electrical system |
| CN114113820A (en) * | 2021-09-15 | 2022-03-01 | 中国航空工业集团公司西安飞机设计研究所 | Portable detection equipment for outfield of aviation power supply product |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103176161B (en) | Automatic electric quantity calibrating system and automatic electric quantity calibrating method | |
| CN103454522B (en) | Based on electronics spare part state of the art automatic checkout system and the method for PXI bus | |
| CN201757767U (en) | General comprehensive automatic test system of airplane electronic part | |
| CN102184749A (en) | Method for automatically testing DCS (Digital Control System) control cabinet | |
| CN201780506U (en) | Test equipment for testing electronic controller | |
| CN202904367U (en) | A testing system based on a PXI bus | |
| CN110045266A (en) | A kind of chip universal testing method and device | |
| CN205079789U (en) | Aviation test platform equipment | |
| CN203688055U (en) | Weighing instrument of dynamic rail weighter | |
| CN103336194A (en) | Integrated automatic test system of on-board computer of civilian airliner | |
| CN103616560A (en) | Automatic power consumption parameter testing device and method applied to avionics device | |
| CN103048984A (en) | Multi-channel ARINC(aeronautical radio incorporated) 700 bus monitoring device and realizing method thereof | |
| CN109189046A (en) | A kind of large aircraft Mechatronic Systems all-around test stand | |
| CN106168993A (en) | Electrical network real-time simulation analysis platform | |
| CN108873867A (en) | A kind of automation load and direct fault location test macro and control method | |
| CN104009882A (en) | Equivalent satellite power supply system testing method and system based on distributed architecture | |
| CN106768074A (en) | A kind of end product automatic test device, system and method | |
| CN203422426U (en) | Universal comprehensive automatic test system of airborne computer of civilian airliner | |
| CN105242134A (en) | Distributed test method suitable for system-grade test of intelligent high-voltage equipment | |
| CN206431614U (en) | A kind of USB interface-based general-purpose built-in type system test platform | |
| CN107861052B (en) | Circuit board test box | |
| CN105548717A (en) | Electrical parameter testing device based on virtual instrument technology | |
| CN108196527B (en) | Test verification system of FPGA and DSP tightly coupled architecture capable of being reconfigured | |
| Krishnanand et al. | Electrical submetering with repurposable applications for the built environment | |
| CN101650655A (en) | Method for analyzing test data of chip |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |