CN206223884U - A kind of test equipment for carrier rocket measuring system with simulation source - Google Patents
A kind of test equipment for carrier rocket measuring system with simulation source Download PDFInfo
- Publication number
- CN206223884U CN206223884U CN201621176690.7U CN201621176690U CN206223884U CN 206223884 U CN206223884 U CN 206223884U CN 201621176690 U CN201621176690 U CN 201621176690U CN 206223884 U CN206223884 U CN 206223884U
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- China
- Prior art keywords
- module
- test
- channel selecting
- simulation source
- selecting module
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Abstract
The utility model is a kind of test equipment for carrier rocket measuring system with simulation source, is related to test equipment technical field.Including Devices to test connecting interface, simulation source setup module, channel selecting module, signal monitoring interface and power supply module；Devices to test connecting interface is connected with externally measured system equipment under test and channel selecting module respectively, the output of simulation source setup module is connected to channel selecting module, channel selecting module output is connected to signal monitoring interface, signal monitoring interface is connected with outside desk-top universal meter, power supply module is connected with externally fed power supply, and power supply module output is connected to simulation source setup module；Channel selecting module uses interlocking-type stacked switch, and interlocking is formed between two passages.The utility model can effectively reduce equipment under test caused by setting mistake because of operator and damage, and can realize the selection of different passages and disconnect, and can realize that single measurement only one of which passage is switched on, it is ensured that the security of equipment under test.
Description
Technical field
The utility model belongs to test equipment technical field, and in particular to a kind of to be surveyed for carrier rocket with simulation source
The test equipment of amount system.
Background technology
There are various measuring apparatus in carrier rocket measuring system【It is to be distinguished with test equipment of the present invention, please
Verification】For the direct current signal or AC signal in test system and convert the result to specific voltage and exported, measurement sets
It is standby after the completion of workshop is assembled, it is necessary to detect that all channel signals conversions are correct.Existing test mode one is directly to carry out hand
Work is tested, and is connected directly in equipment using wire, signal source and universal meter and is tested；This kind of mode shortcoming is operating process
Complexity, labor intensive and time, and easily cause operator's signal source that mistake or contact input are set because interface contact is excessive
Mistake, serious causes device damage.Mode two is that the manual interconnecting device being equipped with using equipment is measured, this manual turn
Connect equipment to be attached with equipment under test by the cable for matching, outer signal source accesses to equipment under test by switching, then
Read-record is carried out by external application table；This mode can be avoided in mode one because of device damage caused by contact wrong, but
It is complex equipment connection mode, while operator can not effectively be solved because of equipment damage caused by the mistake of setting signal source
It is bad.
The content of the invention
The utility model provides a kind of test equipment for carrier rocket measuring system with simulation source, can realize
Carrier rocket measuring apparatus are debugged and tested.
The technical solution of the utility model is：
A kind of test equipment for carrier rocket measuring system with simulation source, including Devices to test connecting interface,
Simulation source setup module, channel selecting module, signal monitoring interface and power supply module；
Devices to test connecting interface is connected with externally measured system equipment under test and channel selecting module respectively, and simulation source sets
Put module output and be connected to channel selecting module, channel selecting module output is connected to signal monitoring interface, signal monitoring interface
It is connected with outside desk-top universal meter, power supply module is connected with externally fed power supply, power supply module output is connected to simulation source setting
Module；
Channel selecting module uses interlocking-type stacked switch, forms interlocking between two passages, passage be signal from
Through channel selecting module and Devices to test connecting interface to externally measured system equipment under test, another leads to simulation source setup module
Road is signal from externally measured system equipment under test through Devices to test connecting interface and channel selecting module to signal monitoring interface.
The Devices to test connecting interface is connected using electric connector with externally measured system equipment under test.
The simulation source setup module is connected with external control panel.
The interlocking-type stacked switch that the channel selecting module is used interlocks uni-directional push-button switch for multi-gear combined type.
The beneficial effects of the utility model are：
A kind of test equipment for carrier rocket measuring system with simulation source described in the utility model can be real
The existing state of the art for testing carrier rocket measuring apparatus safe, fast, efficiently.By the design of simulation source setup module, energy
It is enough effectively to reduce because equipment under test is damaged caused by operator's setting mistake.By the design of channel selecting module, Neng Goushi
The selection of existing different passages and disconnection, and pass through the mutual exclusion formula design of passage gating module, can realize that single measurement only has
One passage is switched on, it is ensured that the security of equipment under test.
Brief description of the drawings
Fig. 1 is that a kind of test equipment for carrier rocket measuring system with simulation source described in the utility model is shown
It is intended to.
Wherein, 1- Devices to tests connecting interface, 2- simulation source setup modules, 3- channel selecting modules, 4- signal monitorings connect
Mouthful, 5- power supply modules.
Specific embodiment
The utility model is described further with reference to the accompanying drawings and examples.
As shown in figure 1, the utility model provides a kind of test for carrier rocket measuring system with simulation source setting
It is standby, including Devices to test connecting interface 1, simulation source setup module 2, channel selecting module 3, signal monitoring interface 4 and power supply mould
Block 5.
Wherein, Devices to test connecting interface 1 is connected with externally measured system equipment under test and channel selecting module 3 respectively,
The output of simulation source setup module 2 is connected to channel selecting module 3, and the output of channel selecting module 3 is connected to signal monitoring interface 4,
Signal monitoring interface 4 is connected with outside desk-top universal meter, and power supply module 5 is connected with externally fed power supply, and the output of power supply module 5 connects
It is connected to simulation source setup module 2.
Devices to test connecting interface 1 is attached according to the adaptable electric connector of equipment under test external interface selection, and
Period distribution is carried out according to its interface requirement.
Simulation source setup module 2 is according to the requirement of the electric signal of equipment under test, the corresponding direct current signal of preprogramming and friendship
Stream signal, and solidify in simulation source setup module 2, can be by the selection on the external control panel of simulation source setup module 2
Switch, realizes that different parameters direct current signal or the output of AC signal are set.Simulation source setup module 2 can realize analog signal
Setting, test equipment is exported pre-set different parameters direct current signal or friendship by the selecting switch on control panel
Stream signal.
Channel selecting module 3 realizes the path control of device interior input signal or output signal, by selecting interlocking-type
Stacked switch, realizes being interlocked between each autonomous channel, it is ensured that any time only one of which passage is connected, it is ensured that equipment under test
Safety；The interlocking-type stacked switch interlocks uni-directional push-button switch from multi-gear combined type.One passage is that channel selecting module 3 will
AC or DC signal from simulation source setup module 2 is exported to equipment under test by Devices to test connecting interface 1, for mould
Intend the AC or DC signal of input equipment under test in actual measuring system；Another passage is that channel selecting module 3 will come from
The conversion signal of the equipment under test input of Devices to test connecting interface 1 is exported to desk-top universal meter by signal monitoring interface 4, is led to
Whether the conversion signal for crossing the measurement result detection equipment under test of desk-top universal meter is correct.
Signal monitoring interface 4 is realized being reliably connected with desk-top universal meter, and positive and negative interface is indicated at connectivity port.
Power supply module 5 is using externally fed power supply for simulation source setup module 2 is powered.
To obtain accurate measurement result, from the desk-top universal meter of high accuracy.
Embodiment of the present utility model is explained in detail above, above-mentioned implementation method is only of the present utility model optimal
Embodiment, but the utility model is not limited to above-described embodiment, in the ken that those of ordinary skill in the art possess
It is interior, can also be made a variety of changes on the premise of the utility model objective is not departed from.
Claims (4)
1. a kind of test equipment for carrier rocket measuring system with simulation source, it is characterised in that：Including Devices to test
Connecting interface (1), simulation source setup module (2), channel selecting module (3), signal monitoring interface (4) and power supply module (5)；
Devices to test connecting interface (1) is connected with externally measured system equipment under test and channel selecting module (3) respectively, simulation source
Setup module (2) output is connected to channel selecting module (3), and channel selecting module (3) output is connected to signal monitoring interface
(4), signal monitoring interface (4) is connected with outside desk-top universal meter, and power supply module (5) is connected with externally fed power supply, mould of powering
Block (5) output is connected to simulation source setup module (2)；
Channel selecting module (3) uses interlocking-type stacked switch, and interlocking is formed between two passages, and a passage is signal from mould
Plan source setup module (2) through channel selecting module (3) and Devices to test connecting interface (1) to externally measured system equipment under test,
Another passage be signal from externally measured system equipment under test through Devices to test connecting interface (1) and channel selecting module (3)
To signal monitoring interface (4).
2. a kind of test equipment for carrier rocket measuring system with simulation source as claimed in claim 1, its feature
It is：The Devices to test connecting interface (1) is connected using electric connector with externally measured system equipment under test.
3. a kind of test equipment for carrier rocket measuring system with simulation source as claimed in claim 1, its feature
It is：The simulation source setup module (2) is connected with external control panel.
4. a kind of test equipment for carrier rocket measuring system with simulation source as claimed in claim 1, its feature
It is：The interlocking-type stacked switch that the channel selecting module (3) uses interlocks uni-directional push-button switch for multi-gear combined type.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621176690.7U CN206223884U (en) | 2016-11-02 | 2016-11-02 | A kind of test equipment for carrier rocket measuring system with simulation source |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621176690.7U CN206223884U (en) | 2016-11-02 | 2016-11-02 | A kind of test equipment for carrier rocket measuring system with simulation source |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206223884U true CN206223884U (en) | 2017-06-06 |
Family
ID=58788683
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621176690.7U Expired - Fee Related CN206223884U (en) | 2016-11-02 | 2016-11-02 | A kind of test equipment for carrier rocket measuring system with simulation source |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206223884U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107942166A (en) * | 2017-11-16 | 2018-04-20 | 北京宇航系统工程研究所 | A kind of fire-working article test system |
| CN110146750A (en) * | 2019-06-10 | 2019-08-20 | 西安现代控制技术研究所 | Play the static electrical detecting tool of arrow |
-
2016
- 2016-11-02 CN CN201621176690.7U patent/CN206223884U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107942166A (en) * | 2017-11-16 | 2018-04-20 | 北京宇航系统工程研究所 | A kind of fire-working article test system |
| CN110146750A (en) * | 2019-06-10 | 2019-08-20 | 西安现代控制技术研究所 | Play the static electrical detecting tool of arrow |
| CN110146750B (en) * | 2019-06-10 | 2021-07-02 | 西安现代控制技术研究所 | Static electric detection tool for rocket |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170606 Termination date: 20211102 |