CN204514534U - Demarcate the device of multiple stage pressure test instrument simultaneously - Google Patents

Demarcate the device of multiple stage pressure test instrument simultaneously Download PDF

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Publication number
CN204514534U
CN204514534U CN201520177373.6U CN201520177373U CN204514534U CN 204514534 U CN204514534 U CN 204514534U CN 201520177373 U CN201520177373 U CN 201520177373U CN 204514534 U CN204514534 U CN 204514534U
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China
Prior art keywords
pressure
surge flask
regulating valve
meter
multiple stage
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Expired - Fee Related
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CN201520177373.6U
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Chinese (zh)
Inventor
冯昕
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China Academy of Building Research CABR
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China Academy of Building Research CABR
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Abstract

The utility model provides a kind of device simultaneously demarcating multiple stage pressure test instrument, and it comprises: clean compressed air source, the first surge flask, the first pressure-regulating valve, the second pressure-regulating valve, reference pressure meter and n platform pressure calibration meter; Described clean compressed air source is connected with the air intake opening of the first surge flask by first pressure-regulating valve, the gas outlet of described first surge flask is provided with second pressure-regulating valve; Described reference pressure meter and n platform pressure calibration meter are connected on the first surge flask all in a gastight manner, wherein, and n >=1.The utility model can meet to multiple stage pressure gauge carry out simultaneously demarcation calibration, and structure simple, with low cost, be easy to safeguard.

Description

Demarcate the device of multiple stage pressure test instrument simultaneously
Technical field
The utility model relates to a kind of device of nominal pressure test instrumentation, particularly a kind of device simultaneously demarcating multiple stage pressure test instrument.
Background technology
More current large-scale industrial occasions (as pharmaceutical factory, food processing factory, various laboratories etc.), comparatively complicated pressure gradient requirement often can be presented in the plane figure in room, and in order to ensure that all rooms all can realize required pressure gradient under robot control system(RCS) effect, then need that the real-time force value measured in institute's control room of a large amount of pressure test instrument (pressure gauge) is installed whether to meet design requirement, and the real-time Adjustment effect reflecting robot control system(RCS).
But in the engineering project that some are larger, the pressure gauge quantity of installing is often in tens of even hundreds of pieces.One by one regular demarcation calibration is carried out to each pressure gauge, bring heavy time and expense cost to user.
In view of this, for solving the problems of the technologies described above, the present inventor based on the research and development of association area, and tests and improvement through continuous, and then has generation of the present invention.
Utility model content
The purpose of this utility model be to propose a kind of structure simple, with low cost, be easy to safeguard and meet the device simultaneously carrying out demarcating calibration to multiple stage pressure gauge.
For reaching above-mentioned purpose, the utility model provides a kind of device simultaneously demarcating multiple stage pressure test instrument, and it comprises: clean compressed air source, the first surge flask, the first pressure-regulating valve, the second pressure-regulating valve, reference pressure meter and n platform pressure calibration meter;
Described clean compressed air source is connected with the air intake opening of the first surge flask by first pressure-regulating valve, the gas outlet of described first surge flask is provided with second pressure-regulating valve;
Described reference pressure meter and n platform pressure calibration meter are connected on the first surge flask all in a gastight manner, wherein, and n >=1.
The utility model also provides a kind of device simultaneously demarcating multiple stage pressure test instrument, and it comprises: clean compressed air source, the first surge flask, the second surge flask, the first pressure-regulating valve, the second pressure-regulating valve, the 3rd pressure-regulating valve, reference pressure meter and n platform pressure calibration meter;
Described clean compressed air source is connected with the air intake opening of the first surge flask by first pressure-regulating valve, the gas outlet of described first surge flask is provided with second pressure-regulating valve;
The air intake opening of the second described surge flask is communicated with the first surge flask, the gas outlet of the second surge flask is provided with the 3rd pressure-regulating valve;
Described reference pressure meter and n platform pressure calibration meter are connected on the second surge flask all in a gastight manner, wherein, and n >=1.
Demarcate the device of multiple stage pressure test instrument while described, wherein, replace clean compressed air source with vacuum pump.
The beneficial effects of the utility model are: can meet to multiple stage pressure gauge carry out simultaneously demarcation calibration, and structure simple, with low cost, be easy to safeguard.
Accompanying drawing explanation
Fig. 1 is device schematic diagram of the present utility model;
Fig. 2 is the device schematic diagram after the utility model increases surge flask.
Description of reference numerals: 1-first pressure-regulating valve; 2-second pressure-regulating valve; 3-clean compressed air source; 4-first surge flask; 5-second surge flask; 6-reference pressure meter; 7-first nominal pressure meter; 8-n-th pressure calibration meter; 9-the 3rd pressure-regulating valve.
Embodiment
Relevant the utility model is the technological means reaching above-mentioned application target and effect and adopt, and now enumerate better feasible embodiment, and coordinate shown in accompanying drawing, details are as follows:
First as shown in Figure 1, be device schematic diagram of the present utility model.The device simultaneously demarcating multiple stage pressure test instrument of the present utility model, mainly comprises: the first pressure-regulating valve 1, second pressure-regulating valve 2, clean compressed air source 3, first surge flask 4, reference pressure meter 6, first nominal pressure meter 7 etc.
Described clean compressed air source 3 is connected with the air intake opening of the first surge flask 4 by first pressure-regulating valve 1, the gas outlet of described first surge flask 4 is provided with second pressure-regulating valve 2.
In addition, described reference pressure meter 6, and n platform pressure calibration meter is connected on the first surge flask 4 all in a gastight manner.Wherein, n >=1.Depict the first nominal pressure meter 1 and the n-th pressure calibration meter 8 in the embodiment in figure 1.
In addition, improve the pressure stability in surge flask if wish, then can increase the quantity of surge flask, as shown in Figure 2, add the second surge flask 5, wherein the air intake opening of the second surge flask 5 is communicated with the first surge flask 4, the gas outlet of the second surge flask 5 is provided with the 3rd pressure-regulating valve 9.Described reference pressure meter 6, and n platform pressure calibration meter is then connected on the second surge flask 5 all in a gastight manner.
It should be noted that, the quantity of surge flask is not limited with two, can adjust quantity according to actual conditions.
If desired negative pressure pattern, its device composition is similar with Fig. 1 and Fig. 2, and difference is to replace clean compressed air source 3 with vacuum pump (not being shown in detail in figure).
Principle of work of the present utility model is:
1, clean compressed air source (being equipped with corresponding filtration, purification measure etc. as pneumatic accumulator or air compressor) provides stable, without oily clean test air.
2, test air enters gas in the first surge flask 4, first surge flask 4 through the first pressure-regulating valve 1 and is released into indoor through the second pressure-regulating valve 2.If add the second surge flask 5, be then that test air enters gas in the first surge flask 4 and the second surge flask 5, second surge flask 5 successively through the first pressure-regulating valve 1 and is released into indoor through the 3rd pressure-regulating valve 9.
3, by adjustment first pressure-regulating valve 1, second pressure-regulating valve 2 (and the 3rd variable valve 9), the pressure extremely required numerical value in the first surge flask 4 (and second surge flask 5) is regulated.
4, have again, true pressure numerical value in first surge flask 4 is illustrated by the reference pressure meter 6 demarcated in advance, n platform needs the pressure gauge demarcating calibration to be connected to the first surge flask 4 in a gastight manner, and adjust registration until consistent with reference pressure meter 6, thus complete the demarcation of n platform pressure calibration meter is calibrated.
In sum, the utility model can meet to multiple stage pressure gauge carry out simultaneously demarcation calibration, and structure simple, with low cost, be easy to safeguard.
Illustrative to description of the present utility model above; and it is nonrestrictive; those skilled in the art is understood, and can carry out many amendments, change or equivalence, but they all will fall in protection domain of the present utility model within the spirit and scope of claim restriction to it.

Claims (4)

1. demarcate a device for multiple stage pressure test instrument simultaneously, it is characterized in that, comprising: clean compressed air source, the first surge flask, the first pressure-regulating valve, the second pressure-regulating valve, reference pressure meter and n platform pressure calibration meter;
Described clean compressed air source is connected with the air intake opening of the first surge flask by first pressure-regulating valve, the gas outlet of described first surge flask is provided with second pressure-regulating valve;
Described reference pressure meter and n platform pressure calibration meter are connected on the first surge flask all in a gastight manner, wherein, and n >=1.
2. the device simultaneously demarcating multiple stage pressure test instrument according to claim 1, is characterized in that, replaces clean compressed air source with vacuum pump.
3. demarcate the device of multiple stage pressure test instrument for one kind simultaneously, it is characterized in that, comprising: clean compressed air source, the first surge flask, the second surge flask, the first pressure-regulating valve, the second pressure-regulating valve, the 3rd pressure-regulating valve, reference pressure meter and n platform pressure calibration meter;
Described clean compressed air source is connected with the air intake opening of the first surge flask by first pressure-regulating valve, the gas outlet of described first surge flask is provided with second pressure-regulating valve;
The air intake opening of the second described surge flask is communicated with the first surge flask, the gas outlet of the second surge flask is provided with the 3rd pressure-regulating valve;
Described reference pressure meter and n platform pressure calibration meter are connected on the second surge flask all in a gastight manner, wherein, and n >=1.
4. the device simultaneously demarcating multiple stage pressure test instrument according to claim 3, is characterized in that, replaces clean compressed air source with vacuum pump.
CN201520177373.6U 2015-03-26 2015-03-26 Demarcate the device of multiple stage pressure test instrument simultaneously Expired - Fee Related CN204514534U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520177373.6U CN204514534U (en) 2015-03-26 2015-03-26 Demarcate the device of multiple stage pressure test instrument simultaneously

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Application Number Priority Date Filing Date Title
CN201520177373.6U CN204514534U (en) 2015-03-26 2015-03-26 Demarcate the device of multiple stage pressure test instrument simultaneously

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CN204514534U true CN204514534U (en) 2015-07-29

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105547575A (en) * 2016-01-25 2016-05-04 广东菲柯特电子科技有限公司 Tire pressure instrument detection system
CN106895945A (en) * 2017-02-10 2017-06-27 中国航发沈阳发动机研究所 A kind of aircraft engine test stand pressure instrumentataion Zero calibration apparatus and the method for school zero
CN106908196A (en) * 2017-02-10 2017-06-30 中国航发沈阳发动机研究所 A kind of aircraft engine test stand pressure instrumentataion calibrating installation and calibration method
CN108102906A (en) * 2017-09-28 2018-06-01 上海国强生化工程装备有限公司 A kind of method of parallel reactor system and parallel control experiment

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105547575A (en) * 2016-01-25 2016-05-04 广东菲柯特电子科技有限公司 Tire pressure instrument detection system
CN106895945A (en) * 2017-02-10 2017-06-27 中国航发沈阳发动机研究所 A kind of aircraft engine test stand pressure instrumentataion Zero calibration apparatus and the method for school zero
CN106908196A (en) * 2017-02-10 2017-06-30 中国航发沈阳发动机研究所 A kind of aircraft engine test stand pressure instrumentataion calibrating installation and calibration method
CN106895945B (en) * 2017-02-10 2019-05-24 中国航发沈阳发动机研究所 A kind of aircraft engine test stand pressure instrumentataion Zero calibration apparatus and zero method of school
CN106908196B (en) * 2017-02-10 2019-09-06 中国航发沈阳发动机研究所 A kind of aircraft engine test stand pressure instrumentataion calibrating installation and calibration method
CN108102906A (en) * 2017-09-28 2018-06-01 上海国强生化工程装备有限公司 A kind of method of parallel reactor system and parallel control experiment
CN108102906B (en) * 2017-09-28 2023-12-15 上海国强生化工程装备有限公司 Parallel reactor system and parallel control experiment method

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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: 20150729

Termination date: 20170326