CN106896236A - A kind of wind speed probe support for testing impact type quick freezing machine flow field - Google Patents
A kind of wind speed probe support for testing impact type quick freezing machine flow field Download PDFInfo
- Publication number
- CN106896236A CN106896236A CN201710221200.3A CN201710221200A CN106896236A CN 106896236 A CN106896236 A CN 106896236A CN 201710221200 A CN201710221200 A CN 201710221200A CN 106896236 A CN106896236 A CN 106896236A
- Authority
- CN
- China
- Prior art keywords
- wind speed
- speed probe
- interface end
- impact type
- flow field
- 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.)
- Pending
Links
- 239000000523 sample Substances 0.000 title claims abstract description 61
- 238000012360 testing method Methods 0.000 title claims abstract description 58
- 230000008014 freezing Effects 0.000 title claims abstract description 32
- 238000007710 freezing Methods 0.000 title claims abstract description 32
- 239000002184 metal Substances 0.000 claims abstract description 23
- 229910052751 metal Inorganic materials 0.000 claims abstract description 23
- 239000000956 alloy Substances 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 3
- 230000002146 bilateral effect Effects 0.000 claims 2
- 239000010931 gold Substances 0.000 claims 1
- 229910052737 gold Inorganic materials 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 3
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P1/00—Details of instruments
Abstract
A kind of wind speed probe support for testing impact type quick freezing machine flow field, including wind speed probe, duplex fitting, four-way connection, five-way joint, six-way joint, metal tube, enter embedding interface end, overcoat interface end, wind speed probe draw-in groove;The wind speed probe rack characteristic in test impact type quick freezing machine flow field is:Metal tube by joint be connected with each other turn into can fixed placement wind speed probe support.A kind of wind speed probe support for testing impact type quick freezing machine flow field of the present invention;Can flexibly be assembled by joint and metal tube, solve the problems, such as accurate fixed test position in the quick-frozen field flow-field test of impact type, increase the flexibility of testing tool, finally improve the accuracy of test result.
Description
Technical field
The invention belongs to quick-frozen food technical field, it is related to a kind of wind speed probe branch for testing impact type quick freezing machine flow field
Frame, more particularly to a kind of easy to use, effective anemobiagraph probe fixing device.
Background technology
Air flow impact type instant freezer has obtained widely should in recent years as a kind of efficient freezing plant in food service industry
With, but frozen region between quick-frozen machine nozzle and conveyer belt is extremely narrow, therefore, it is accurate during flow-field test fixed to survey
There is certain difficulty in examination position;And in test process effectively fix wind speed probe position, to the correct of test result
Property is most important.At present, due to changeable, the complexity of instant freezer nozzle arrangements so that there is presently no a kind of more flexible, side
Just testing tool is applied in instant freezer testing field.Therefore, related exploration also needs to the unremitting of various countries' researcher and exerts
Power.
The content of the invention
The present invention is for accurate fixed test position difficulty is larger in existing impact type quick freezing machine flow-field test and tests work
The poor present situation of the flexibility of tool, proposes a kind of wind speed probe support for testing impact type quick freezing machine flow field.
Technical scheme includes the wind speed probe support of the new impact type quick freezing machine flow-field test of design, improves wind
The measures such as flexibility, the test result accuracy of fast test process.Specifically technical scheme is:
The wind speed probe support in test impact type quick freezing machine flow field includes that wind speed probe, duplex fitting, four-way connection, five connect
Head, six-way joint, metal tube, enter embedding interface end, overcoat interface end, wind speed probe draw-in groove;Wind speed probe rack characteristic is:It is double
Pass joint, four-way connection, five-way joint, six-way joint are connected by metal tube;Duplex fitting, four-way connection, five-way joint, six
Pass joint enters that embedding interface end size is identical, and overcoat interface end size is identical;Four-way connection, five-way joint, six-way joint it is same
It is mutually perpendicular between the interface of one joint, the embedding interface end that enters of duplex fitting is located along the same line with overcoat interface end;Enter embedding
Interface end is 5-20mm high, and the cylinder of diameter 4-6mm, overcoat interface end is 5-20mm high, and internal diameter 4-6mm, external diameter 6-8mm is hollow
Cylinder;The section of wind speed probe draw-in groove is 1/4 circular arc of radius 3-5mm;The length of metal tube is 60-120mm, its diameter dimension
It is identical with overcoat interface end internal diameter size.
Enter embedding interface end for 6-16mm high, the cylinder of diameter 4.5-5.5mm, overcoat interface end is 6-16mm high, internal diameter
4.5-5.5mm, external diameter 6.5-7.5mm hollow cylinders.
Enter embedding interface end for 8-12mm high, the cylinder of diameter 4.5-5.5mm, overcoat interface end is 8-12mm high, internal diameter
4.5-5.5mm, external diameter 6.5-7.5mm hollow cylinders.
Enter embedding interface end for 10mm high, the cylinder of diameter 5mm, overcoat interface end is 10mm high, internal diameter 5mm, external diameter 7mm are empty
Heart cylinder.
The section of wind speed probe draw-in groove is 1/4 circular arc of radius 3.5-4.5mm.
The section of wind speed probe draw-in groove is 1/4 circular arc of radius 4mm.
The length of metal tube is 80-100mm.
The length of metal tube is 90mm.
Duplex fitting, four-way connection, five-way joint, six-way joint are made up of PVC material.
Metal tube is made up of alloy material;The overall weight of support can be improved using alloy material, the steady of support is improved
It is qualitative.
To adapt to the wind speed testing requirement of diverse location, can be every to adjust support by changing the connection number of duplex fitting
Height between layer;Using rubber band, the wind speed probe that will be placed on wind speed probe draw-in groove carries out bondage with metal tube, makes wind speed
Probe is fixed, it is ensured that the stability of wind speed probe during flow-field test, is conducive to improving the accuracy of test result.
A kind of wind speed probe support for testing impact type quick freezing machine flow field of the present invention, can be by joint and metal
The flexible assembling of pipe, solves the problems, such as accurate fixed test position in the quick-frozen field flow-field test of impact type, increases test
The flexibility of instrument, finally improves the accuracy of test result, and data supporting is provided to follow-up experimental study.
Brief description of the drawings
Fig. 1 is a kind of schematic three dimensional views of the wind speed probe support for testing impact type quick freezing machine flow field of the present invention;
In Fig. 1,1, wind speed probe;2nd, duplex fitting;3rd, four-way connection;4th, five-way joint;5th, six-way joint;6th, metal tube;
Fig. 2 is a kind of six-way joint schematic diagram of the wind speed probe support for testing impact type quick freezing machine flow field of the present invention;
In Fig. 2,7, enter embedding interface end;8th, overcoat interface end;
Fig. 3 is a kind of draw-in groove front view of the wind speed probe support for testing impact type quick freezing machine flow field of the present invention;
In Fig. 3,9, wind speed probe draw-in groove;
Fig. 4 is a kind of front view of the wind speed probe support for testing impact type quick freezing machine flow field of the present invention;
Fig. 5 is a kind of five-way joint schematic diagram of the wind speed probe support for testing impact type quick freezing machine flow field of the present invention;
Fig. 6 is a kind of four-way connection schematic diagram of the wind speed probe support for testing impact type quick freezing machine flow field of the present invention;
Fig. 7 is a kind of duplex fitting schematic diagram of the wind speed probe support for testing impact type quick freezing machine flow field of the present invention.
Specific embodiment
For the operating process for making present invention realization is easy to understand with creation characteristic, with reference to specific embodiment,
The present invention is expanded on further.
The wind speed probe support in test impact type quick freezing machine flow field include wind speed probe 1, duplex fitting 2, four-way connection 3,
Five-way joint 4, six-way joint 5, metal tube 6, enter embedding interface end 7, overcoat interface end 8, wind speed probe draw-in groove 9;Wind speed probe branch
Frame is characterised by:Duplex fitting 2, four-way connection 3, five-way joint 4, six-way joint 5 are connected by metal tube 6;Duplex fitting 2,
Four-way connection 3, five-way joint 4, six-way joint 5 enter that the size of embedding interface end 7 is identical, and the size of overcoat interface end 8 is identical;Four connect
First 3, be mutually perpendicular between five-way joint 4, the interface of the same joint of six-way joint 5, duplex fitting 2 enter embedding interface end 7 with
Overcoat interface end 8 is located along the same line;Enter embedding interface end 7 for 10mm high, the cylinder of diameter 5mm, overcoat interface end 8 is height
10mm, internal diameter 5mm, external diameter 7mm hollow cylinders;The section of wind speed probe draw-in groove 9 is 1/4 circular arc of radius 4mm;Metal tube 6
Length is 9mm, and its diameter dimension is identical with overcoat interface end 8 sizes of internal diameter.
Duplex fitting 2, four-way connection 3, five-way joint 4, six-way joint 5 are made up of PVC material.
Metal tube 6 is made up of alloy material;The overall weight of support can be improved using alloy material, the steady of support is improved
It is qualitative.
To adapt to the wind speed testing requirement of diverse location, support can be adjusted by changing the connection number of duplex fitting 2
Height between every layer;Using rubber band, the wind speed probe 1 that will be placed on wind speed probe draw-in groove 9 carries out bondage with metal tube 6,
Fix wind speed probe 1, it is ensured that the stability of wind speed probe 1 during flow-field test, be conducive to improving the accurate of test result
Property.
A kind of wind speed probe support for testing impact type quick freezing machine flow field of the present invention, can be by joint and metal
The flexible assembling of pipe, solves the problems, such as accurate fixed test position in the quick-frozen field flow-field test of impact type, increases test
The flexibility of instrument, finally improves the accuracy of test result, and data supporting is provided to follow-up experimental study.
Claims (10)
1. a kind of wind speed probe support for testing impact type quick freezing machine flow field, it is characterised in that:Test impact type quick freezing machine flow field
Wind speed probe support include wind speed probe(1), duplex fitting(2), four-way connection(3), five-way joint(4), six-way joint
(5), metal tube(6), enter embedding interface end(7), overcoat interface end(8), wind speed probe draw-in groove(9);Wind speed probe rack characteristic exists
In:Duplex fitting(2), four-way connection(3), five-way joint(4), six-way joint(5)By metal tube(6)Connection;Duplex fitting
(2), four-way connection(3), five-way joint(4), six-way joint(5)Enter embedding interface end(7)Size is identical, overcoat interface end(8)
Size is identical;Four-way connection(3), five-way joint(4), six-way joint(5)Same joint interface between be mutually perpendicular to, bilateral
Joint(2)Enter embedding interface end(7)With overcoat interface end(8)It is located along the same line;Enter embedding interface end(7)It is 5-20mm high,
The cylinder of diameter 4-6mm, overcoat interface end(8)It is 5-20mm high, internal diameter 4-6mm, external diameter 6-8mm hollow cylinders;Wind speed probe
Draw-in groove(9)Section for radius 3-5mm 1/4 circular arc;Metal tube(6)Length be 60-120mm, its diameter dimension and overcoat
Interface end(8)Internal diameter size is identical.
2. a kind of wind speed probe support for testing impact type quick freezing machine flow field as claimed in claim 1, it is characterised in that:Enter embedding
Interface end(7)It is 6-16mm high, the cylinder of diameter 4.5-5.5mm, overcoat interface end(8)It is 6-16mm high, internal diameter 4.5-
5.5mm, external diameter 6.5-7.5mm hollow cylinders.
3. a kind of wind speed probe support for testing impact type quick freezing machine flow field as claimed in claim 1, it is characterised in that:Enter embedding
Interface end(7)It is 8-12mm high, the cylinder of diameter 4.5-5.5mm, overcoat interface end(8)It is 8-12mm high, internal diameter 4.5-
5.5mm, external diameter 6.5-7.5mm hollow cylinders.
4. a kind of wind speed probe support for testing impact type quick freezing machine flow field as claimed in claim 1, it is characterised in that:Enter embedding
Interface end(7)It is 10mm high, the cylinder of diameter 5mm, overcoat interface end(8)It is 10mm high, internal diameter 5mm, external diameter 7mm open circles
Post.
5. a kind of wind speed probe support for testing impact type quick freezing machine flow field as claimed in claim 1, it is characterised in that:Wind speed
Probe draw-in groove(9)Section for radius 3.5-4.5mm 1/4 circular arc.
6. a kind of wind speed probe support for testing impact type quick freezing machine flow field as claimed in claim 1, it is characterised in that:Wind speed
Probe draw-in groove(9)Section for radius 4mm 1/4 circular arc.
7. a kind of wind speed probe support for testing impact type quick freezing machine flow field as claimed in claim 1, it is characterised in that:Metal
Pipe(6)Length be 80-100mm.
8. a kind of wind speed probe support for testing impact type quick freezing machine flow field as claimed in claim 1, it is characterised in that:Metal
Pipe(6)Length be 90mm.
9. a kind of wind speed probe support for testing impact type quick freezing machine flow field as claimed in claim 1, it is characterised in that:Bilateral
Joint(2), four-way connection(3), five-way joint(4), six-way joint(5)It is made up of PVC material.
10. a kind of wind speed probe support for testing impact type quick freezing machine flow field as claimed in claim 1, it is characterised in that:Gold
Category pipe(6)It is made up of alloy material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710221200.3A CN106896236A (en) | 2017-04-06 | 2017-04-06 | A kind of wind speed probe support for testing impact type quick freezing machine flow field |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710221200.3A CN106896236A (en) | 2017-04-06 | 2017-04-06 | A kind of wind speed probe support for testing impact type quick freezing machine flow field |
Publications (1)
Publication Number | Publication Date |
---|---|
CN106896236A true CN106896236A (en) | 2017-06-27 |
Family
ID=59194346
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710221200.3A Pending CN106896236A (en) | 2017-04-06 | 2017-04-06 | A kind of wind speed probe support for testing impact type quick freezing machine flow field |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN106896236A (en) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2768520A1 (en) * | 1997-09-12 | 1999-03-19 | Jacques Salles | Wind speed visual display |
CN201229353Y (en) * | 2008-07-09 | 2009-04-29 | 上海理工大学 | Wind speed and air quantity tester of combination high-effect filter |
RU2009139880A (en) * | 2009-10-28 | 2011-05-10 | Государственное образовательное учреждение высшего профессионального образования "Башкирский государственный университет" БашГУ (RU) | DEVICE FOR CALIBRATING THERMAL ANEMOMETRIC FLOW FLOW SENSORS |
CN204157977U (en) * | 2014-10-30 | 2015-02-18 | 吴佛金 | A kind of assembling plastic layer shelf structure |
CN204536353U (en) * | 2015-04-16 | 2015-08-05 | 中国建筑科学研究院 | Air velocity transducer array and wind speed measuring apparatus |
CN204832228U (en) * | 2015-07-09 | 2015-12-02 | 公安部天津消防研究所 | A multiple spot air speed measuring device that is used for tunnel detection of preventing discharging fume |
CN206710450U (en) * | 2017-04-06 | 2017-12-05 | 上海海洋大学 | A kind of wind speed probe supporting structure |
-
2017
- 2017-04-06 CN CN201710221200.3A patent/CN106896236A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2768520A1 (en) * | 1997-09-12 | 1999-03-19 | Jacques Salles | Wind speed visual display |
CN201229353Y (en) * | 2008-07-09 | 2009-04-29 | 上海理工大学 | Wind speed and air quantity tester of combination high-effect filter |
RU2009139880A (en) * | 2009-10-28 | 2011-05-10 | Государственное образовательное учреждение высшего профессионального образования "Башкирский государственный университет" БашГУ (RU) | DEVICE FOR CALIBRATING THERMAL ANEMOMETRIC FLOW FLOW SENSORS |
CN204157977U (en) * | 2014-10-30 | 2015-02-18 | 吴佛金 | A kind of assembling plastic layer shelf structure |
CN204536353U (en) * | 2015-04-16 | 2015-08-05 | 中国建筑科学研究院 | Air velocity transducer array and wind speed measuring apparatus |
CN204832228U (en) * | 2015-07-09 | 2015-12-02 | 公安部天津消防研究所 | A multiple spot air speed measuring device that is used for tunnel detection of preventing discharging fume |
CN206710450U (en) * | 2017-04-06 | 2017-12-05 | 上海海洋大学 | A kind of wind speed probe supporting structure |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR101820545B1 (en) | Device for multipoint acquisition/distribution of fluid, in particular probe for tapping pressure in a turbomachine air inlet | |
CN206710450U (en) | A kind of wind speed probe supporting structure | |
CN102269690B (en) | Method and device for testing frictional drag coefficient of inner wall of pipeline | |
CN106768824B (en) | Three-hole pressure probe comb | |
CN110044570B (en) | Pneumatic tremor error correction method for pressure measurement experiment of rotating body | |
CN202049174U (en) | Seven-hole pressure probe manufactured through adopting photocuring quick-forming method | |
CN209706971U (en) | It is a kind of to flow down the device of internal multi-point temperature measurement for high temperature pressure corrosion environment | |
CN106896236A (en) | A kind of wind speed probe support for testing impact type quick freezing machine flow field | |
CN209043611U (en) | A kind of stagnation pressure and static pressure test detector probe | |
CN106949989A (en) | A kind of hemispherical head steady temperature force combination probe for measuring low speed three-dimensional flow field | |
CN208399151U (en) | A kind of circle static probe component and static probe component | |
CN204694444U (en) | A kind of probe assembly and there is its device | |
CN206020340U (en) | Impedance tube sound insulation measurement exemplar fixing device | |
CN203848890U (en) | Card type ultrasonic fluid flow measuring device | |
CN109828036B (en) | Guide sleeve with small blind area | |
CN107014434A (en) | A kind of conehead steady temperature force combination probe for measuring high subsonics three-dimensional flow field | |
CN104359646A (en) | Hypersonic-speed effuser employing pumping method to control boundary layer thickness | |
CN205280368U (en) | Measuring device is always pressed to experimental radial multiple spot of high thrust engine distortion | |
CN203385700U (en) | Portable type ultrasonic guided-wave detection test block for axial defects | |
CN106918437A (en) | A kind of four hole probes for measuring subsonic speed two-dimensional flow field | |
CN204613241U (en) | A kind of Multi-tube composite wind speed measuring device | |
CN106768827A (en) | A kind of steady temperature force combination probe for measuring transonic speed two-dimensional flow field | |
CN206905824U (en) | A kind of Ultrasonic water meter, calorimeter, flowmeter center sleeve line structure | |
CN204388981U (en) | The high-performance fairing of critical flow sonic nozzle | |
CN207556630U (en) | Flow measurement test-run a machine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170627 |