CN206756421U - A kind of low-speed wind tunnel model - Google Patents

A kind of low-speed wind tunnel model Download PDF

Info

Publication number
CN206756421U
CN206756421U CN201720652095.4U CN201720652095U CN206756421U CN 206756421 U CN206756421 U CN 206756421U CN 201720652095 U CN201720652095 U CN 201720652095U CN 206756421 U CN206756421 U CN 206756421U
Authority
CN
China
Prior art keywords
section
fan
sensors
wind tunnel
low
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.)
Expired - Fee Related
Application number
CN201720652095.4U
Other languages
Chinese (zh)
Inventor
郑金辉
姬鹏宇
岳明洋
门正兴
付成龙
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.)
Chengdu Aeronautic Polytechnic
Original Assignee
Chengdu Aeronautic Polytechnic
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 Chengdu Aeronautic Polytechnic filed Critical Chengdu Aeronautic Polytechnic
Priority to CN201720652095.4U priority Critical patent/CN206756421U/en
Application granted granted Critical
Publication of CN206756421U publication Critical patent/CN206756421U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

It the utility model is related to a kind of low-speed wind tunnel model, including fan section, rectification section, test section and expansion segment, supply air system is provided with fan section, honeycomb is provided with rectification section, test section material is transparent material, the detection means that the support of installation object under test is provided with test section and is connected with object under test, detection means includes pressure plectrum, a sensors and a single-chip microcomputers, pressure plectrum is attached to the lower section of object under test, pressure plectrum is connected with a sensors, a sensors are connected with a single-chip microcomputers, supply air system includes fan fixed mount and blower fan, blower fan is connected with c sensors, c sensors are connected with controller.Wind tunnel model of the present utility model is integrally designed using segmentation structure, various pieces play different effects and mutual cooperation, the mobility status of entity ambient gas can be simulated, and the utility model cost is low, conveniently moving, observation are directly perceived, disclosure satisfy that middle school or regular higher educational institutions are used for the requirement of classroom instruction.

Description

A kind of low-speed wind tunnel model
Technical field
Teaching equipment technical field is the utility model is related to, specifically, refers to a kind of low-speed wind tunnel model.
Background technology
Wind-tunnel is to produce and control in a manual manner air-flow, for the flowing of simulated flight device or entity ambient gas Situation, and mensurable air-flow to the action effect of entity and observes a kind of pipe-like experimental facilities of physical phenomenon, it be into Row aerodynamic experiment is the most frequently used, one of maximally effective instrument.The China Higher Educate Train talent, many courses are directed to air The related content of power, therefore have very big demand to teaching wind-tunnel.
But all the time, because existing wing tunnel test apparatus is complicated, requires high, manufacturing cost to actuating unit It is high so that China university wind tunnel laboratory is studied mainly as longitudinal science fund national and at the provincial and ministerial level and large project Experimental place, and use groups are mainly College Teachers, master, doctoral candidate and other related scientific research personnel, for just high In, the efficiency of Undergraduate Experimental Teaching do not played substantially.Therefore, the physics opened up at present in middle school and regular higher educational institutions On classroom, wind tunnel experiment demonstration is general can only all to use the multimedia video about wind-tunnel on network to carry out aided education, unfavorable Visual understanding in student to content, has had a strong impact on quality of instruction.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of low-speed wind tunnel model, to meet middle school or common high It is used for the requirement of classroom instruction Deng universities and colleges.
The technical scheme that the utility model solves above-mentioned technical problem is as follows:A kind of low-speed wind tunnel model, including fan section, Rectification section, test section and expansion segment, the fan section is interior to be provided with supply air system, and honeycomb, test section material are provided with rectification section Matter is transparent material, the detection means that the support of installation object under test is provided with test section and is connected with object under test.
Operation principle of the present utility model is:Air-flow is led into rectification section by supply air system, airflow passes rectification section It is changed into steady air flow after honeycomb, air-flow enters test section and acted on object under test, passes through the test section energy of transparent material The physical phenomenon of object under test is enough observed, the size of active force suffered by object under test, expansion segment can be measured by detection means Airflow reflux can be avoided and influence experimental data.
The beneficial effects of the utility model are:Wind tunnel model is integrally designed using segmentation structure, and various pieces play not Same effect and mutual cooperation, the mobility status of entity ambient gas can be simulated, and the utility model cost is low, movement side Just, observation is directly perceived, disclosure satisfy that middle school or regular higher educational institutions are used for the requirement of classroom instruction.
On the basis of above-mentioned technical proposal, the utility model can also do following improvement.
Further, the detection means includes pressure plectrum, a sensors and a single-chip microcomputers, and pressure plectrum is attached to determinand The lower section of body, pressure plectrum are connected with a sensors, and a sensors are connected with a single-chip microcomputers.
It is using the above-mentioned further beneficial effect of scheme:When airflow function is on pressure plectrum, pressure plectrum is to be measured The bottom of object produces pressure, and the pressure conversion that a sensors will act on pressure plectrum is electric signal and sent to a monolithics Machine, a single-chip microcomputers can calculate pressure value of the airflow function on object under test according to resulting magnitude of voltage, and this pressure value is For value of lift of the airflow function in object under test bottom.
Further, the detection means includes spring, and spring one end is connected with support bottom, the spring other end with it is to be measured Object is connected, and graduation mark is identified with the side wall of test section.
It is using the above-mentioned further beneficial effect of scheme:When airflow function is on object under test, air-flow measuring targets Caused lift rises object under test, and then extends spring, experimenter by the graduation mark that is identified in test section side wall, The elongation of spring can be drawn, can also obtain acting on object under test further according to the elongation and coefficient of elasticity of spring Value of lift.
Further, the supply air system includes the fan fixed mount being arranged in fan section and installed in fan fixed mount On blower fan, blower fan is connected with c sensors, and c sensors are connected with controller.
It is using the above-mentioned further beneficial effect of scheme:Controller and c sensors can change the rotating speed of blower fan to obtain Air-flow different in flow rate is obtained, so as to meet the experiment needs of experimenter.
Further, the honeycomb is provided with rope or smog syringe.
It is using the above-mentioned further beneficial effect of scheme:It is fixed on light and fine and soft rope on honeycomb, can basis Whether the amplitude observation air-flow of rope shake is stablized;Flowing by smog caused by smog syringe with air-flow, can also see Examine whether air-flow is stablized.
Further, the support is carbon-point.
It is using the above-mentioned further beneficial effect of scheme:Carbon-point is simple in construction, small volume, the branch as object under test Frame, be advantageous to reduce support interferences caused by stream field, so as to improve the accuracy of experimental data.In addition, carbon-point good toughness, It is not easy to break, object under test is kept relative stabilization in experimentation, and carbon-point is also convenient for the peace of object under test Dress.
Further, the expansion segment trailer is provided with speed detection instrument, and it is mono- that speed detection instrument includes fan, b sensors and b Piece machine, fan are arranged on the afterbody of expansion segment, and fan is connected with b sensors, and b sensors are connected with b single-chip microcomputers.
It is using the above-mentioned further beneficial effect of scheme:When expansion segment blowout airflow function on fan, can cause The rotation of electric fan, b sensors measure the rotating speed of flabellum, and velocity amplitude is sent to b single-chip microcomputers, and b single-chip microcomputers are according to wind The velocity amplitude of fan flabellum rotating speed can obtain the wind pressure value of blower fan blowout air-flow.
Further, the fan section, rectification section, test section and expansion segment material are PVC board.
It is using the above-mentioned further beneficial effect of scheme:PVC board cost is low, hardness is big, intensity is high, any surface finish is put down It is whole, it on the one hand can make weight saving of the present utility model, consequently facilitating it is mobile, on the other hand, because PVC board any surface finish is put down It is whole, additionally it is possible to reduce the hole wall of wind tunnel model to drag effects caused by air-flow.
Further, the free end of the fan section is provided with protective cover.
It is using the above-mentioned further beneficial effect of scheme:Protective cover can avoid experimenter that hand is stretched into blower fan and caused Security incident.
Brief description of the drawings
Fig. 1 is sectional view of the present utility model;
Fig. 2 is stereogram of the present utility model.
In accompanying drawing, the part representated by each label is as follows:
1st, fan section, 2, rectification section, 3, test section, 4, expansion segment, 5, blower fan, 6, honeycomb, 7, support, 8, determinand Body, 9, fan fixed mount, 10, protective cover.
Embodiment
Principle of the present utility model and feature are described below in conjunction with accompanying drawing, example is served only for explaining this practicality It is new, it is not intended to limit the scope of the utility model.
A kind of low-speed wind tunnel model, as shown in Figure 1 and Figure 2, including fan section 1, rectification section 2, test section 3 and expansion segment 4, fan section 1 is interior to be provided with fan fixed mount 9, and blower fan 5 is provided with fan fixed mount 9, and protection is provided with the free end of fan section 1 Cover 10, causes security incident to avoid experimenter that hand is stretched into blower fan 5.Blower fan 5 is connected with c sensors, and c sensors are connected with Controller, experimenter can change the rotating speed of blower fan 5 by c sensors and controller, to obtain air-flow different in flow rate.
As shown in Figure 1 and Figure 2, honeycomb 6 is provided with rectification section 2, is changed into stable air-flow after airflow passes honeycomb 6, Light and fine and soft rope is fixed with honeycomb 6, when air current flow, restricts and is shaken with air-flow, experimenter can be according to rope shake Whether amplitude observation air-flow is stablized.Or smog syringe is installed on honeycomb 6, experimenter passes through produced by smog syringe Smog with the flowing of air-flow, can also observe whether air-flow is stablized.
As shown in Figure 1 and Figure 2, test section 3 is made using the glass of the high grade of transparency, or test section 3 is provided with and is easy to The window being made using the glass of the high grade of transparency of observation, carbon-point is provided with test section 3, is provided with carbon-point to be measured Pressure plectrum is posted in object 8, the lower section of object under test 8, and pressure plectrum is connected with a sensors, and a sensors are connected with a single-chip microcomputers. When airflow function is on pressure plectrum, the bottom of pressure plectrum measuring targets 8 produces pressure, and a sensors will act at pressure Pressure conversion on plectrum can calculate outlet for electric signal and transmission to a single-chip microcomputers, a single-chip microcomputers according to resulting magnitude of voltage The pressure value that stream is acted on object under test 8, this pressure value are value of lift of the airflow function in object under test bottom.
As another embodiment, spring is installed in the bottom of carbon-point, the other end of spring is connected with object under test 8 Connect, graduation mark is identified in the side wall of test section 3.When airflow function is on object under test 8, produced by air-flow measuring targets 8 Lift object under test 8 is increased, and then extend spring, experimenter, can be with by the graduation mark that is identified in the side wall of test section 3 The elongation of spring is drawn, the liter acted on object under test 8 can also be obtained further according to elongation and the coefficient of elasticity of spring Force value.
As shown in Figure 1 and Figure 2, the afterbody of expansion segment 4 is provided with speed detection instrument, speed detection instrument include fan, b sensors with And b single-chip microcomputers, fan are arranged on the afterbody of expansion segment 4, fan is connected with b sensors, and b sensors are connected with b single-chip microcomputers. When expansion segment blowout airflow function on fan, the rotation of electric fan can be caused, b sensors measure the rotating speed of flabellum, And send velocity amplitude to b single-chip microcomputers, b single-chip microcomputers can obtain blower fan blowout air-flow according to the velocity amplitude of electric fan rotating speed Wind pressure value.
Above-mentioned fan section 1, rectification section 2, test section 3 and the material of expansion segment 4 are PVC board, and PVC board cost is low, hardness Greatly, intensity is high, any surface finish is smooth, on the one hand can make weight saving of the present utility model, consequently facilitating mobile, the opposing party Face, because PVC board any surface finish is smooth, additionally it is possible to reduce the hole wall of wind tunnel model to drag effects caused by air-flow.
Preferred embodiment of the present utility model is the foregoing is only, it is all in this practicality not to limit the utility model Within new spirit and principle, any modification, equivalent substitution and improvements made etc., guarantor of the present utility model should be included in Within the scope of shield.

Claims (9)

  1. A kind of 1. low-speed wind tunnel model, it is characterised in that:Including fan section(1), rectification section(2), test section(3)And expansion segment (4), the fan section(1)It is interior to be provided with supply air system, rectification section(2)It is interior to be provided with honeycomb(6), test section(3)Material is transparent Material, in test section(3)It is interior to be provided with installation object under test(8)Support(7)And and object under test(8)The detection means of connection.
  2. 2. low-speed wind tunnel model according to claim 1, it is characterised in that:The detection means includes pressure plectrum, a is passed Sensor and a single-chip microcomputers, pressure plectrum are attached to object under test(8)Lower section, pressure plectrum is connected with a sensors, a sensors It is connected with a single-chip microcomputers.
  3. 3. low-speed wind tunnel model according to claim 1, it is characterised in that:The detection means includes spring, spring one End is connected with support bottom, the spring other end and object under test(8)It is connected, scale is identified with the side wall of test section Line.
  4. 4. low-speed wind tunnel model according to claim 1, it is characterised in that:The supply air system includes being arranged on fan section (1)Interior fan fixed mount(9)And installed in fan fixed mount(9)On blower fan(5), blower fan(5)It is connected with c sensors, c Sensor is connected with controller.
  5. 5. low-speed wind tunnel model according to claim 1, it is characterised in that:The honeycomb(6)It is provided with rope or smog Syringe.
  6. 6. low-speed wind tunnel model according to claim 1, it is characterised in that:The support is carbon-point.
  7. 7. the low-speed wind tunnel model according to any one of claim 1 to 6, it is characterised in that:The expansion segment(4)Afterbody is set There is speed detection instrument, speed detection instrument includes fan, b sensors and b single-chip microcomputers, and fan is arranged on expansion segment(4)Afterbody, Fan is connected with b sensors, and b sensors are connected with b single-chip microcomputers.
  8. 8. the low-speed wind tunnel model according to any one of claim 1 to 6, it is characterised in that:The fan section(1), rectification Section(2), test section(3)And expansion segment(4)Material is PVC board.
  9. 9. the low-speed wind tunnel model according to any one of claim 1 to 6, it is characterised in that:The fan section(1)Freedom End is provided with protective cover(10).
CN201720652095.4U 2017-06-07 2017-06-07 A kind of low-speed wind tunnel model Expired - Fee Related CN206756421U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720652095.4U CN206756421U (en) 2017-06-07 2017-06-07 A kind of low-speed wind tunnel model

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720652095.4U CN206756421U (en) 2017-06-07 2017-06-07 A kind of low-speed wind tunnel model

Publications (1)

Publication Number Publication Date
CN206756421U true CN206756421U (en) 2017-12-15

Family

ID=60622310

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720652095.4U Expired - Fee Related CN206756421U (en) 2017-06-07 2017-06-07 A kind of low-speed wind tunnel model

Country Status (1)

Country Link
CN (1) CN206756421U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108318212A (en) * 2018-04-17 2018-07-24 成都工匠之星科技有限公司 A kind of experimental section of teaching demonstration wind-tunnel
CN109243263A (en) * 2018-08-30 2019-01-18 北京航空航天大学 A kind of Table top type DC low-speed wind-tunnel of teaching demonstration and experiment
CN109469634A (en) * 2018-10-12 2019-03-15 中国航发成都发动机有限公司 A kind of large size air source apparatus
CN110412315A (en) * 2019-08-07 2019-11-05 中国气象局气象探测中心 Integral-type wind element calibrating installation
CN114279672A (en) * 2021-12-09 2022-04-05 中国科学院新疆生态与地理研究所 Intensive wind tunnel structure capable of changing wind speed in layering manner

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108318212A (en) * 2018-04-17 2018-07-24 成都工匠之星科技有限公司 A kind of experimental section of teaching demonstration wind-tunnel
CN109243263A (en) * 2018-08-30 2019-01-18 北京航空航天大学 A kind of Table top type DC low-speed wind-tunnel of teaching demonstration and experiment
CN109469634A (en) * 2018-10-12 2019-03-15 中国航发成都发动机有限公司 A kind of large size air source apparatus
CN110412315A (en) * 2019-08-07 2019-11-05 中国气象局气象探测中心 Integral-type wind element calibrating installation
CN114279672A (en) * 2021-12-09 2022-04-05 中国科学院新疆生态与地理研究所 Intensive wind tunnel structure capable of changing wind speed in layering manner

Similar Documents

Publication Publication Date Title
CN206756421U (en) A kind of low-speed wind tunnel model
CN109243263A (en) A kind of Table top type DC low-speed wind-tunnel of teaching demonstration and experiment
CN202700511U (en) Simulation environment test chamber
CN206223233U (en) A kind of experimental system for simulating for large-scale cabin environment Comfort Evaluation
CN205264188U (en) Teaching is with test section of small -size low -speed smoke wind tunnel
CN104835389A (en) Multifunctional physical exploration experiment demonstration instrument
CN203386396U (en) Wind tunnel demonstration experiment device
CN203013072U (en) Air buoyancy demonstrator
CN102024358A (en) Airplane lift demonstration instrument for physics teaching
CN106910400A (en) Gas flow rate and pressure relation demonstration instrument
CN212365290U (en) Teaching device for demonstrating lifting force and stall phenomenon of wing
CN203163959U (en) Simulation device for wind resistance of speed regulation air laminar flow test model
CN111696412A (en) Experiment and simulation demonstration device for wing lift force and surface flow
CN204514358U (en) Air detection terminal
CN203837898U (en) Dust devil simulation platform
CN206573151U (en) A kind of measuring technology comprehensive experimental device
CN208060748U (en) A kind of ship meteorological to survey instrument with infrared sensor of the human body
CN208938480U (en) A kind of wind tunnel experiment equipment for teaching
CN207408068U (en) A kind of cloud layer simulation device
CN206441421U (en) Airfoil lift tests mechanism and the airplane ascensional force demonstrator with the mechanism
CN113138062A (en) Multifunctional aerodynamic experiment device and teaching method
CN204667723U (en) A kind of acceleration of gravity measurement mechanism
CN204463755U (en) A kind of educational propaganda plate with air detecting device
CN204440756U (en) A kind of speed measuring device for Physical Experiment
CN206584055U (en) A kind of miniature weather monitoring system

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: 20171215

Termination date: 20190607