CN101482440A - Special inside static pressure field test device for main nozzle of jet loom - Google Patents

Special inside static pressure field test device for main nozzle of jet loom Download PDF

Info

Publication number
CN101482440A
CN101482440A CNA2009100461238A CN200910046123A CN101482440A CN 101482440 A CN101482440 A CN 101482440A CN A2009100461238 A CNA2009100461238 A CN A2009100461238A CN 200910046123 A CN200910046123 A CN 200910046123A CN 101482440 A CN101482440 A CN 101482440A
Authority
CN
China
Prior art keywords
pressure
jet loom
air
main nozzle
diameter
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.)
Granted
Application number
CNA2009100461238A
Other languages
Chinese (zh)
Other versions
CN101482440B (en
Inventor
薛文良
陈革
魏孟媛
程隆棣
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Bureau of Emigration &. Engression Examination &. Quarantine People's R
Donghua University
Original Assignee
Donghua University
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Donghua University filed Critical Donghua University
Priority to CN2009100461238A priority Critical patent/CN101482440B/en
Publication of CN101482440A publication Critical patent/CN101482440A/en
Application granted granted Critical
Publication of CN101482440B publication Critical patent/CN101482440B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Looms (AREA)

Abstract

The invention relates to a special inner static pressure field testing device for the main jet nozzle of jet loom, which consists of a jet loom main jet nozzle simulator, a pressure sensor (9), a multi-point input data acquisition card (10) and a computer (11); a row of pressure detection holes (12) are formed on the jet pipe (6) of the jet loom main jet nozzle simulator along the length direction; each pressure detection hole (12) is installed with a pressure sensor (9) vertically on outside; and the pressure sensor (9) is connected with the computer (11) through the multi-point input data acquisition card (10). The invention can obtain accurate static pressure testing curve by simulating the main jet nozzle of the jet loom and installing measuring equipment, is very helpful for improving the research of jet loom, and plays a major part in improving the performance of jet loom.

Description

Special inside static pressure field test device for main nozzle of jet loom
Technical field
The invention belongs to main nozzle of jet loom DATA REASONING field, particularly relate to a kind of proving installation of static-pressure field.
Background technology
Air-jet loom is a shuttleless loom with fastest developing speed, owing to adopted the mode of air-jet weft insertion, makes loom production efficiency improve greatly.Main burner is one of most important parts of air-jet loom, and the jet-stream wind that produces by main burner makes weft yarn obtain initial flying speed.And the jet-stream wind characteristic that main burner produces depends on the inner structure and the shape of nozzle consumingly.Therefore the relation of studying main burner inside, shape and jet-stream wind characteristic is to improve the main path of air-jet loom performance.But because the main burner structure is very complicated, precision is also very high, and correlative study at present mainly is by computational tool numerical analysis to be carried out in the nozzle interior flow field, lacks effective laboratory facilities and is verified.
Summary of the invention
Technical matters to be solved by this invention provides a kind of special inside static pressure field test device for main nozzle of jet loom, to solve the defective that lacks efficiency test means checking main nozzle of jet loom inside static pressure Flow Field Numerical in the prior art.
A kind of special inside static pressure field test device for main nozzle of jet loom, by the main nozzle of jet loom analogue means, pressure transducer (9), multiple spot input data collecting card (10) and computing machine (11) four parts are formed, have a row pressure power exploration hole (12) on the length direction of the playpipe of described main nozzle of jet loom analogue means (6), the outer pressure transducer (9) that all is vertically installed with of each pressure exploration hole (12), described pressure transducer (9) connects computing machine (11) by multiple spot input data collecting card (10).
Described pressure exploration hole (12) has 10~16.
Described pressure exploration hole (12) is equidistantly arranged, and pore size is 0.6~1.2mm.
Described main nozzle of jet loom analogue means comprises air intake opening (1), ring-shaped air chamber (2), rectification air flue (3), throat (4), annular air channel (5), playpipe (6), negative-pressure air-flow inlet (7), negative-pressure air-flow runner (8), wherein air intake opening (1) diameter D 1Be 2~4mm, negative-pressure air-flow runner (8) diameter D 2Be 2~3mm, negative-pressure air-flow runner (8) inner and outer diameter D 3Be 0.3~0.5mm, playpipe (6) diameter D 4Be 4~5mm, negative-pressure air-flow inlet diameter D 5Be 5~6mm, main burner analogue means diameter D 6Be 14~16mm, air intake opening (1) left side distance L 1Be 15~16mm, ring-shaped air chamber (2) outer length L 2Be 10~12mm, ring-shaped air chamber (2) inner length L 3Be 8~10mm, the streamlined design is all adopted in the outside in the rectification air flue (3), guarantees the interval L of throat (4) 5Be 0.2~8mm, horizontal length L 4Be 10~12mm, the transition section horizontal range L of annular air channel (5) 6Be 5~8mm, parallel-segment horizontal range L 7Be 6~9mm, playpipe (6) length L 8Be 200~250mm.
Beneficial effect
The present invention passes through the simulation main nozzle of jet loom, and installs and measures equipment, so that obtain static pressure test curve accurately, can well help improve the research work of air-jet loom, for important contribution has been made in the performance raising of air-jet loom.
Description of drawings
Fig. 1 is the structural representation of main nozzle of jet loom analogue means of the present invention;
Fig. 2 is the structural representation of special inside static pressure field test device for main nozzle of jet loom of the present invention
Wherein, 1-air intake opening, 2-ring-shaped air chamber, 3-rectification air flue, 4-throat, 5-annular air channel, 6-playpipe, 7-negative-pressure air-flow inlet, 8-negative-pressure air-flow runner, 9-pressure transducer, 10-data collecting card, 11-computing machine
Embodiment
Below in conjunction with specific embodiment, further set forth the present invention.Should be understood that these embodiment only to be used to the present invention is described and be not used in and limit the scope of the invention.Should be understood that in addition those skilled in the art can make various changes or modifications the present invention after the content of having read the present invention's instruction, these equivalent form of values fall within the application's appended claims institute restricted portion equally.
Embodiment 1
A kind of special inside static pressure field test device for main nozzle of jet loom, by the main nozzle of jet loom analogue means, pressure transducer 9, multiple spot input data collecting card 10 and computing machine 11 4 parts are formed, described main nozzle of jet loom analogue means comprises air intake opening 1, ring-shaped air chamber 2, rectification air flue 3, throat 4, annular air channel 5, playpipe 6, negative-pressure air-flow inlet 7, negative-pressure air-flow runner 8, wherein air intake opening 1 diameter D 1Be 2~4mm, negative-pressure air-flow runner 8 diameter D 2Be 2~3mm, negative-pressure air-flow runner 8 inner and outer diameter D 3Be 0.3~0.5mm, playpipe 6 diameter D 4Be 4~5mm, negative-pressure air-flow inlet diameter D 5Be 5~6mm, main burner analogue means diameter D 6Be 14~16mm, air intake opening 1 left side distance L 1Be 15~16mm, ring-shaped air chamber 2 outer length L 2Be 10~12mm, ring-shaped air chamber 2 inner length L 3Be 8~10mm, the streamlined design is all adopted in the outside in the rectification air flue 3, guarantees the interval L of throat 4 5Be 0.2~8mm, horizontal length L 4Be 10~12mm, the transition section horizontal range L of annular air channel 5 6Be 5~8mm, parallel-segment horizontal range L 7Be 6~9mm, playpipe 6 length L 8Be 200~250mm; Have a row totally 10~16 pressure exploration holes 12 on the length direction of the playpipe 6 of described main nozzle of jet loom analogue means, pore size is 0.6~1.2mm, all be vertically installed with a pressure transducer 9 outside each pressure exploration hole 12, described pressure transducer 9 connects computing machine 11 by multiple spot input data collecting card 10, pressure exploration hole 12 can equidistantly be arranged during detection, also can adjust arrangement pitch, so that obtain more along sliding static pressure test curve according to the pressure data that test obtains.

Claims (4)

1. special inside static pressure field test device for main nozzle of jet loom, it is characterized in that: by the main nozzle of jet loom analogue means, pressure transducer (9), multiple spot input data collecting card (10) and computing machine (11) four parts are formed, have a row pressure power exploration hole (12) on the length direction of the playpipe of described main nozzle of jet loom analogue means (6), the outer pressure transducer (9) that all is vertically installed with of each pressure exploration hole (12), described pressure transducer (9) connects computing machine (11) by multiple spot input data collecting card (10).
2. special inside static pressure field test device for main nozzle of jet loom as claimed in claim 1 is characterized in that: described pressure exploration hole (12) has 10~16.
3. special inside static pressure field test device for main nozzle of jet loom as claimed in claim 1 or 2 is characterized in that: described pressure exploration hole (12) is equidistantly arranged, and pore size is 0.6~1.2mm.
4. special inside static pressure field test device for main nozzle of jet loom as claimed in claim 3, it is characterized in that: described main nozzle of jet loom analogue means comprises air intake opening (1), ring-shaped air chamber (2), rectification air flue (3), throat (4), annular air channel (5), playpipe (6), negative-pressure air-flow inlet (7), negative-pressure air-flow runner (8), wherein air intake opening (1) diameter D 1Be 2~4mm, negative-pressure air-flow runner (8) diameter D 2Be 2~3mm, negative-pressure air-flow runner (8) inner and outer diameter D 3Be 0.3~0.5mm, playpipe (6) diameter D 4Be 4~5mm, negative-pressure air-flow inlet diameter D 5Be 5~6mm, main burner analogue means diameter D 6Be 14~16mm, air intake opening (1) left side distance L 1Be 15~16mm, ring-shaped air chamber (2) outer length L 2Be 10~12mm, ring-shaped air chamber (2) inner length L 3Be 8~10mm, the streamlined design is all adopted in the outside in the rectification air flue (3), guarantees the interval L of throat (4) 5Be 0.2~8mm, horizontal length L 4Be 10~12mm, the transition section horizontal range L of annular air channel (5) 6Be 5~8mm, parallel-segment horizontal range L 7Be 6~9mm, playpipe (6) length L 8Be 200~250mm.
CN2009100461238A 2009-02-12 2009-02-12 Special inside static pressure field test device for main nozzle of jet loom Expired - Fee Related CN101482440B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009100461238A CN101482440B (en) 2009-02-12 2009-02-12 Special inside static pressure field test device for main nozzle of jet loom

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009100461238A CN101482440B (en) 2009-02-12 2009-02-12 Special inside static pressure field test device for main nozzle of jet loom

Publications (2)

Publication Number Publication Date
CN101482440A true CN101482440A (en) 2009-07-15
CN101482440B CN101482440B (en) 2010-11-17

Family

ID=40879651

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009100461238A Expired - Fee Related CN101482440B (en) 2009-02-12 2009-02-12 Special inside static pressure field test device for main nozzle of jet loom

Country Status (1)

Country Link
CN (1) CN101482440B (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102495231A (en) * 2011-11-25 2012-06-13 江苏万工科技集团有限公司 Device and method for measuring flow velocity in main injection guide pipe
CN102517762A (en) * 2011-11-25 2012-06-27 江苏万工科技集团有限公司 System for measuring stability of weft yarn carried by main jet flow
CN102889957A (en) * 2011-07-18 2013-01-23 上海袋式除尘配件有限公司 Pressure testing device for pulse injection equipment of bag type dust collector
CN105403353A (en) * 2015-12-14 2016-03-16 广东溢达纺织有限公司 Air-jet loom air pressure detection apparatus and detection method
CN105908288A (en) * 2016-04-29 2016-08-31 东华大学 Device for measuring air flow parameters in main carding area of carding machine and measuring method of device
CN115901074A (en) * 2022-12-13 2023-04-04 重庆大学 Movable probe device for measuring pressure in flow channel of spray pipe

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102889957A (en) * 2011-07-18 2013-01-23 上海袋式除尘配件有限公司 Pressure testing device for pulse injection equipment of bag type dust collector
CN102495231A (en) * 2011-11-25 2012-06-13 江苏万工科技集团有限公司 Device and method for measuring flow velocity in main injection guide pipe
CN102517762A (en) * 2011-11-25 2012-06-27 江苏万工科技集团有限公司 System for measuring stability of weft yarn carried by main jet flow
CN105403353A (en) * 2015-12-14 2016-03-16 广东溢达纺织有限公司 Air-jet loom air pressure detection apparatus and detection method
CN105908288A (en) * 2016-04-29 2016-08-31 东华大学 Device for measuring air flow parameters in main carding area of carding machine and measuring method of device
CN115901074A (en) * 2022-12-13 2023-04-04 重庆大学 Movable probe device for measuring pressure in flow channel of spray pipe
CN115901074B (en) * 2022-12-13 2024-06-04 重庆大学 Movable probe device for measuring pressure in spray pipe flow channel

Also Published As

Publication number Publication date
CN101482440B (en) 2010-11-17

Similar Documents

Publication Publication Date Title
CN101482440B (en) Special inside static pressure field test device for main nozzle of jet loom
CN104391135A (en) Calibration device and calibration method for micro wind speed based on laser doppler
CN103471809A (en) Ultrahigh frequency response plasma flow measurement device
CN103335813A (en) Airflow anti-phase opposite thrust sand collector
CN203595596U (en) Boundary layer measuring rake for wind tunnel measurement
CN111175011B (en) Device and method for simulating working environment of fan and measuring air volume of fan during running of train
CN103048153A (en) Experiment system for cylindrical structure acoustic performance test
CN103940581B (en) A kind of experimental technique of monitoring trace gas concentration value measurement jet entrainment amount
CN112945500A (en) Simulation measurement device and method for influence of blocking degree of transonic wind tunnel
CN103175671A (en) Simulation device and method for wind resistance of speed-regulating laminar wind flow flowing test model
CN106989896A (en) A kind of dynamic temperature force combination probe for measuring subsonics three-dimensional non-steady flow field
CN200976007Y (en) Wind speed probe device for meteorological sensor
CN207717326U (en) A kind of dense form dummy vehicle airflow on surface boundary layer thickness measuring device
CN206020458U (en) A kind of Pitot-static tube
CN106525159A (en) Air flow measurement device
CN105699690A (en) A vortex street wind speed sensor based on fiber gratings and an assembly method thereof
CN203535067U (en) Measuring device for wind speed and wind volume
CN203479824U (en) Pitot tube apparatus for multiple-detection-point flue gas flow velocity measuring
CN211904600U (en) False tail branch for measuring internal resistance of ventilation model
CN215178954U (en) Particulate matter on-line measuring system
CN205643104U (en) Closed wire sand blown by wind corrodes analogue test device
CN101482437A (en) Special weft airflow acting force test device for main nozzle of jet loom
CN204085584U (en) A kind of wind quantity test device
CN202836651U (en) High-precision intelligent instrument counting and sampling device
CN202548144U (en) Device for measuring flow velocity in main injection guide pipe

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: SHANGHAI BUREAU OF EMIGRATION +. ENGRESSION EXAMIN

Effective date: 20130513

C41 Transfer of patent application or patent right or utility model
C53 Correction of patent for invention or patent application
CB03 Change of inventor or designer information

Inventor after: Xue Wenliang

Inventor after: Lu Weimin

Inventor after: Jiang Chun

Inventor after: Chen Ge

Inventor after: Wei Mengyuan

Inventor after: Cheng Longdai

Inventor before: Xue Wenliang

Inventor before: Chen Ge

Inventor before: Wei Mengyuan

Inventor before: Cheng Longdai

COR Change of bibliographic data

Free format text: CORRECT: INVENTOR; FROM: XUE WENLIANG CHEN GE WEI MENGYUAN CHENG LONGDI TO: XUE WENLIANG LU WEIMIN JIANG CHUN CHEN GE WEI MENGYUAN CHENG LONGDI

TR01 Transfer of patent right

Effective date of registration: 20130513

Address after: 201620 Shanghai, Songjiang new town, North Road, No. 2999 people

Patentee after: Donghua University

Patentee after: Shanghai Bureau of Emigration &. Engression Examination &. Quarantine People's R

Address before: 201620 Shanghai, Songjiang new town, North Road, No. 2999 people

Patentee before: Donghua University

C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20101117

Termination date: 20130212