CN205228771U - Experimental minute -pressure measurement system in low speed wind tunnel flow field - Google Patents
Experimental minute -pressure measurement system in low speed wind tunnel flow field Download PDFInfo
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- CN205228771U CN205228771U CN201520904838.3U CN201520904838U CN205228771U CN 205228771 U CN205228771 U CN 205228771U CN 201520904838 U CN201520904838 U CN 201520904838U CN 205228771 U CN205228771 U CN 205228771U
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- measuring blood
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Abstract
The utility model discloses an experimental minute -pressure measurement system in low speed wind tunnel flow field, including a plurality of pressure measurement chip, be provided with two atmospheric pressure input ports on each pressure measurement chip, a pressure measurement needle is connected to hose of each atmospheric pressure input port connection, the other end of hose, the other end of pressure measurement needle towards gas field incoming flow direction, a plurality of pressure measurement chip set becomes one, provides the electric current behind the rectifying and wave -filtering by same power supply system in unison, and a plurality of signaling conversion circuit, every signaling conversion circuit's input are connected to the signal output part of a pressure measurement chip separately, and signaling conversion circuit's output is connected to the outer control system of wind -tunnel through the transmission line, the utility model has the characteristics of the precision is high, the real -time is good, sampling frequency is high, pressure difference between can directly obtaining at 2 has reduced a great deal of error and has introduced the link, and the precision can reach 0.1 percent. It satisfies the measurement requirement of wind -tunnel flow field completely to be applicable to multiple small ressure measurement environment.
Description
Technical field
The present invention relates to wind tunnel test field, specifically relate to a kind of low-speed wind tunnel flow field test micro-pressure measurement system.
Background technology
In wind tunnel test, in order to obtain reliable and stable test figure, many times needing to measure the air pressure in Flow Field in Wind Tunnel, in order to the air pressure of whole Flow Field in Wind Tunnel can be obtained more accurately, needing to carry out air pressure test to several points in wind-tunnel.
What traditional pressure measurement mode adopted is that electronic scanner directly measures each measuring point pressure, then the pressure reduction by calculating corresponding measuring point measures air-flow drift angle, its difference between two between pressure tap of good flow field is often very little, usually a few Pa is only had, and more independent force value is very large, because electronic scanner exists fixing error, the range of general sensor is all several atmospheric pressure (0.1Mpa is an atmospheric pressure), sensor oneself itself estimates there are tens pa to the Acquisition Error of each point, so again two points are subtracted each other (pressure differential in reality between these two points estimates to only have several pa), only the impact that brings of error all actual value to having masked, therefore adopt and directly measure the method that two elevated pressures measuring points calculate its relative micro-pressure-difference, larger measuring error certainly will be produced.
And adopt traditional electronic scanner, because the reason of itself structure, needing in wind-tunnel, lay pressure measurement pipeline and circuit, just needing to arrange many pipelines and circuit when needing the air pressure between multiple 2 of test.And in wind tunnel test, in order to obtain stable flow process, need other devices allowing the interior few laying as far as possible of wind-tunnel and tested model have nothing to do, in case affect in test Flow Field in Wind Tunnel, make test data out of true.
Therefore traditional pressure testing method is that precision problem or offering question all have influence on wind tunnel test, not in applicable current wind tunnel test demand.
Summary of the invention
The object of the invention is on prior art basis, provide a kind of low-speed wind tunnel flow field to test micro-pressure measurement system, solved the pressure reduction between the time 2 same in Flow Field in Wind Tunnel by new metering system.
For achieving the above object, the present invention adopts following technical scheme:
A kind of low-speed wind tunnel flow field test micro-pressure measurement system, comprising:
Several pressure measurement chips, each pressure measurement chip are provided with two air pressure input ports, and each air pressure input port connects a flexible pipe, and the other end of flexible pipe connects a needle for measuring blood pressue, and flow path direction is carried out to gas field in the other end of needle for measuring blood pressue;
Several pressure measurement integrated chips are integrated, and unification provides the electric current after rectifying and wave-filtering by same electric power system,
Several signaling conversion circuits, the input end of each signaling conversion circuit is connected to the signal output part of a pressure measurement chip separately, and the output terminal of signaling conversion circuit is connected to the control system outside wind-tunnel by transmission line.
In technique scheme, described needle for measuring blood pressue carrys out flow path direction one end towards gas field is provided with through hole to one end of connecting hose along axis.
In technique scheme, described needle for measuring blood pressue comes towards gas field the needle body wall of flow path direction one end is provided with several holes, and each hole is communicated with the through hole in needle for measuring blood pressue.
In technique scheme, the hole on described needle for measuring blood pressue body wall is arranged on circumferentially same, and quantity is no less than four.
In technique scheme, described needle for measuring blood pressue is that metal material is made, and the diameter of needle for measuring blood pressue is between 1mm ~ 2mm.
In technique scheme, described flexible pipe can replace with metal tube.
A method of testing for low-speed wind tunnel flow field test micro-pressure measurement system, detailed process is as follows:
Be arranged in wind-tunnel by the whole measurement mechanism become one, each two needle for measuring blood pressue be connected with pressure measurement chip is arranged on two points that needs test separately;
When wind tunnel test is opened, pressure measurement chip collects the atmospheric pressure value of two points at one time, and is carried out subtracting each other by the atmospheric pressure value of two points and obtain air pressure difference;
In pressure measurement chip, air pressure difference is carried out piezoelectricity conversion, be transferred to signaling conversion circuit after being converted to electric signal, signal carries out A/D conversion and is transferred to control system in signaling conversion circuit after amplification, filtering;
The formula surveyed by the school preset in control system is converted to pressure difference value to electric signal and shows.
In sum, owing to have employed technique scheme, the invention has the beneficial effects as follows:
The present invention has that precision is high, real-time good, sample frequency high, can directly obtain pressure difference value between 2, decreases all multiple errors and introduces link, and precision can reach ± and 0.1%; Be applicable to multiple slight pressure measurement environment and meet Flow Field in Wind Tunnel measurement requirement completely;
The present invention uses homemade circuit, and integrated level is high, perfect heat-dissipating, can carry out modularization installation.Individual module has the functions such as independently constant current source power supply, temperature gain compensation, output signal amplification, and mutual interference is zero substantially, achieves the target of through engineering approaches application;
The present invention is applied in low-speed wind tunnel test, military and remarkable in economical benefits: be applied to flow field detection experiment, achieves the direct measurement to differential pressure between 2 o'clock, for conventional means, not only increase the precision of test figure, and substantially increase its accuracy; Be applied to other types manometric test, the data precision obtained due to it is high, is therefore also applicable to other conventional little pressure survey occasions.
Accompanying drawing explanation
Examples of the present invention will be described by way of reference to the accompanying drawings, wherein:
Fig. 1 is structural representation of the present invention;
Fig. 2 is control system schematic diagram of the present invention;
Wherein: 1 is pressure measurement chip, and 2 is flexible pipes, and 3 is needle for measuring blood pressue, and 4 is through holes, and 5 is side openings.
Embodiment
As shown in Figure 1, the pressure measurement mode that the present invention adopts is different with traditional pressure measurement, by a needle for measuring blood pressue, needle for measuring blood pressue adopts metal to make, in order to control pressure measurement precision, the diameter of needle for measuring blood pressue is between 1mm ~ 2mm, needle for measuring blood pressue passes through along axis and is provided with through hole, then needle for measuring blood pressue is connected on pressure measurement chip by a pipe, pipe adopts metal tube to be best, but metal tube is because its physical characteristics, too much arranges can affect flow field at wind-tunnel, therefore take rubber hose better, not only there is good impermeability, also there is good radiating effect.
The other end of flexible pipe is fixedly attached to the porch on pressure measurement chip, and pressure measurement chip itself has pressure measuring function, and in chip, directly can complete the same time subtracted each other by the air pressure collected and obtain pressure difference, and pressure difference is converted to analog electrical signal.
Analog electrical signal is carried out rectification by outside signaling conversion circuit by electric signal.Carry out A/D conversion again after filtering and by storing in transmission line to control system, the formula then surveyed by school just can be completed and be converted to actual pressure difference to the digital signal obtained and show.
In the present invention, divide accurate activity pressure value, the air intake opening of needle for measuring blood pressue needs just to carry out flow path direction to gas field, air flow energy is made successfully to enter on pressure measurement chip, simultaneously in order to record more flow field state value, the sidewall of needle for measuring blood pressue is provided with several side openings, and side opening must be arranged on circumferentially same, side opening needs to be communicated with the through hole in needle for measuring blood pressue, can obtain stagnation pressure and the static pressure in flow field by arranging this circle side opening.
By above setting, two needle for measuring blood pressue are arranged on separately on two points of needs test, the pressure reduction of two points in a certain moment just can be obtained by test, in order to the pressure reduction of more point can be obtained, by arranging needle for measuring blood pressue on difference, by integrating control (as shown in Figure 2), the pressure reduction at a time between wind-tunnel each point interior can be known.
Whole device volume after the present invention is integrated is very little, for 8 drive test pressure chips, whole device only has 21cm × 10cm size, the space also not having traditional pressure transducer to occupy from whole volume is large, and the profile of this device is regular, affect Flow Field in Wind Tunnel by what reasonably setting can't be too many.
The present invention is not limited to aforesaid embodiment.The present invention expands to any new feature of disclosing in this manual or any combination newly, and the step of the arbitrary new method disclosed or process or any combination newly.
Claims (6)
1. a low-speed wind tunnel flow field test micro-pressure measurement system, is characterized in that comprising:
Several pressure measurement chips, each pressure measurement chip are provided with two air pressure input ports, and each air pressure input port connects a flexible pipe, and the other end of flexible pipe connects a needle for measuring blood pressue, and flow path direction is carried out to gas field in the other end of needle for measuring blood pressue;
Several pressure measurement integrated chips are integrated, and unification provides the electric current after rectifying and wave-filtering by same electric power system,
Several signaling conversion circuits, the input end of each signaling conversion circuit is connected to the signal output part of a pressure measurement chip separately, and the output terminal of signaling conversion circuit is connected to the control system outside wind-tunnel by transmission line.
2. test micro-pressure measurement system in a kind of low-speed wind tunnel flow field according to claim 1, is characterized in that described needle for measuring blood pressue carrys out flow path direction one end towards gas field is provided with through hole to one end of connecting hose along axis.
3. a kind of low-speed wind tunnel flow field test micro-pressure measurement system according to claim 2, it is characterized in that described needle for measuring blood pressue comes towards gas field the needle body wall of flow path direction one end is provided with several holes, each hole is communicated with the through hole in needle for measuring blood pressue.
4. a kind of low-speed wind tunnel flow field test micro-pressure measurement system according to claim 3, it is characterized in that the hole on described needle for measuring blood pressue body wall is arranged on circumferentially same, and quantity is no less than four.
5. test micro-pressure measurement system in any one low-speed wind tunnel flow field according to claims 1 to 4, it is characterized in that described needle for measuring blood pressue is that metal material is made, the diameter of needle for measuring blood pressue is between 1mm ~ 2mm.
6. a kind of low-speed wind tunnel flow field test micro-pressure measurement system according to claim 1, is characterized in that described flexible pipe can replace with metal tube.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520904838.3U CN205228771U (en) | 2015-11-13 | 2015-11-13 | Experimental minute -pressure measurement system in low speed wind tunnel flow field |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201520904838.3U CN205228771U (en) | 2015-11-13 | 2015-11-13 | Experimental minute -pressure measurement system in low speed wind tunnel flow field |
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| CN205228771U true CN205228771U (en) | 2016-05-11 |
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| CN201520904838.3U Expired - Fee Related CN205228771U (en) | 2015-11-13 | 2015-11-13 | Experimental minute -pressure measurement system in low speed wind tunnel flow field |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105258914A (en) * | 2015-11-13 | 2016-01-20 | 中国空气动力研究与发展中心低速空气动力研究所 | Low-speed wind tunnel flow field test micropressure measurement system |
| CN107105565A (en) * | 2017-05-02 | 2017-08-29 | 西北工业大学 | A kind of slight pressure traverse measuring device and measuring method for plasma flow control |
| CN110735672A (en) * | 2019-10-11 | 2020-01-31 | 中国航发沈阳发动机研究所 | shunt ring and intermediate casing sector section structure with same |
| CN117168758A (en) * | 2023-11-01 | 2023-12-05 | 中国空气动力研究与发展中心空天技术研究所 | Application method of hypersonic flight test parameter test system |
-
2015
- 2015-11-13 CN CN201520904838.3U patent/CN205228771U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105258914A (en) * | 2015-11-13 | 2016-01-20 | 中国空气动力研究与发展中心低速空气动力研究所 | Low-speed wind tunnel flow field test micropressure measurement system |
| CN105258914B (en) * | 2015-11-13 | 2019-01-08 | 中国空气动力研究与发展中心低速空气动力研究所 | A kind of low-speed wind tunnel flow field test micro-pressure measurement system |
| CN107105565A (en) * | 2017-05-02 | 2017-08-29 | 西北工业大学 | A kind of slight pressure traverse measuring device and measuring method for plasma flow control |
| CN110735672A (en) * | 2019-10-11 | 2020-01-31 | 中国航发沈阳发动机研究所 | shunt ring and intermediate casing sector section structure with same |
| CN110735672B (en) * | 2019-10-11 | 2021-10-22 | 中国航发沈阳发动机研究所 | Shunt ring and intermediate casing fan-shaped section structure with same |
| CN117168758A (en) * | 2023-11-01 | 2023-12-05 | 中国空气动力研究与发展中心空天技术研究所 | Application method of hypersonic flight test parameter test system |
| CN117168758B (en) * | 2023-11-01 | 2024-01-23 | 中国空气动力研究与发展中心空天技术研究所 | Application method of hypersonic flight test parameter test system |
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| C14 | Grant of patent or utility model | ||
| 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: 20160511 Termination date: 20181113 |