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CN208537061U - A wind speed, pressure and temperature calibration system based on jet wind tunnel - Google Patents

A wind speed, pressure and temperature calibration system based on jet wind tunnel Download PDF

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Publication number
CN208537061U
CN208537061U CN201821397667.XU CN201821397667U CN208537061U CN 208537061 U CN208537061 U CN 208537061U CN 201821397667 U CN201821397667 U CN 201821397667U CN 208537061 U CN208537061 U CN 208537061U
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pressure
jet
evaporator
wind speed
wind tunnel
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杨文�
白志鹏
耿春梅
殷宝辉
高凌云
韩斌
赵雪艳
王静
王歆华
赵若杰
张楠
王健
马银红
刘盈盈
孙峰
张霞
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Chinese Research Academy of Environmental Sciences
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Chinese Research Academy of Environmental Sciences
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Abstract

The utility model discloses a kind of wind speed based on jet stream wind-tunnel, pressure, temperature calibration system, the system comprises: controller, vacuum pump, refrigeration unit, evaporator, jet stream wind-tunnel, blower, seal cavity;The evaporator, the jet stream wind-tunnel and the blower are arranged inside the seal cavity;The outside of the seal cavity is arranged in the controller, the refrigeration unit and the vacuum pump;The blower is arranged in the jet stream wind-tunnel;The controller is used to change the intracorporal temperature of the seal chamber, wind speed and pressure by controlling the refrigeration unit, the jet stream wind-tunnel and the vacuum pump.Above system in the utility model can be realized the accurate simulation to wind speed, pressure and temperature to guarantee to demarcate all environment quasi-instruments.

Description

A kind of wind speed based on jet stream wind-tunnel, pressure, temperature calibration system
Technical field
The utility model relates to true environment simulation field, more particularly to a kind of wind speed based on jet stream wind-tunnel, pressure, Temperature calibration system.
Background technique
The calibration of wind speed, pressure and temperature, indeed through the ring for simulating different wind speed, temperature and pressure The calibration to the instrument of airspeedometer, particle sampler, gas apparatus and all environmental classes is realized in border.By changing environment In wind speed, anticipated that the influence of cutting efficiency of the different particle samplers under different wind speed.Alternatively, by changing The variation of temperature and pressure precognition gas apparatus under different pressures and different temperatures in changing environment.Currently, due to adopting The non-intellectual of sample environment, it is existing that sampling instrument often will appear that data are not allowed, outrange, exceptional value, instrument operating parameter are abnormal etc. As therefore, in order to improve sampling instrument sampling precision and avoid the waste of unnecessary manpower financial capacity, it is necessary to provide one kind Wind speed, pressure, temperature calibration system.
Currently, in the prior art, typically by one seal cavity of setting, evaporator and wind are arranged in the cavity Machine etc. realizes the simulation to wind speed.But its simulation precision is lower, cannot achieve the control to wind speed, and cannot achieve pressure It is simulated while power, temperature, wind speed.
Summary of the invention
The purpose of the utility model is to provide a kind of wind speed based on jet stream wind-tunnel, pressure, temperature calibration system, realizations pair The accurate simulation of wind speed, pressure and temperature is to guarantee to demarcate all environment quasi-instruments.
To achieve the above object, the utility model provides following scheme:
A kind of wind speed based on jet stream wind-tunnel, pressure, temperature calibration system, the system comprises:
Controller, vacuum pump, refrigeration unit, evaporator, jet stream wind-tunnel, blower, seal cavity;
The evaporator, the jet stream wind-tunnel and the blower are arranged inside the seal cavity;
The outside of the seal cavity is arranged in the controller, the refrigeration unit and the vacuum pump;
The blower is arranged in the jet stream wind-tunnel;
The controller is used for by controlling the refrigeration unit, the jet stream wind-tunnel and the vacuum pump to change State the intracorporal temperature of seal chamber, wind speed and pressure.
Optionally, the seal cavity is also provided with door body, and the size of the door body is 1 × 1.5m.
Optionally, the seal cavity is made of insulation board, and the outer surface of the insulation board is coated with waterproof cement, described close The size for sealing cavity is 2 × 2.8 × 2.2m.
Optionally, it is additionally provided with hanging plate at the top of the seal cavity, multiple holes are offered on the hanging plate, for hanging Instrument to be calibrated.
Optionally, the evaporator specifically includes: the first evaporator, the second evaporator, third evaporator.
Optionally, the power of the blower is 15KW.
Optionally, the diameter of the efflux nozzle of the jet stream wind-tunnel is 300mm.
Optionally, the size of the evaporator is 2.7 × 0.55 × 0.6m, and the evaporator is located at the jet stream wind-tunnel Efflux nozzle the other side.
According to specific embodiment provided by the utility model, the utility model discloses following technical effects:
By the way that jet stream wind-tunnel is arranged in sealed chamber in the utility model, blower is set in jet stream wind-tunnel, is being sealed Vacuum pump and refrigeration unit is arranged in exterior thereto, controls unit, vacuum pump and rotation speed of fan by controller, can be realized In the accurate simulation of the indoor temperature of seal chamber, pressure and wind speed, and then realizes and all appts of environmental classes are demarcated.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment Needed in attached drawing be briefly described, it should be apparent that, the accompanying drawings in the following description is only the utility model Some embodiments for those of ordinary skill in the art without any creative labor, can also basis These attached drawings obtain other attached drawings.
Fig. 1 is wind speed, pressure, temperature calibration system construction drawing of the utility model embodiment based on jet stream wind-tunnel.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work Every other embodiment obtained, fall within the protection scope of the utility model.
The purpose of the utility model is to provide a kind of wind speed based on jet stream wind-tunnel, pressure, temperature calibration system, realizations pair The accurate simulation of wind speed, pressure and temperature is to guarantee to demarcate all environment quasi-instruments.
To keep the above objects, features, and advantages of the utility model more obvious and easy to understand, with reference to the accompanying drawing and have Body embodiment is described in further detail the utility model.
Fig. 1 is wind speed, pressure, temperature calibration system construction drawing, such as Fig. 1 of the utility model embodiment based on jet stream wind-tunnel It is shown, the system comprises:
Controller 1, vacuum pump 2, refrigeration unit 3, evaporator 4, jet stream wind-tunnel 5, blower 6, seal cavity 7;
The evaporator 4, the jet stream wind-tunnel 5 and the blower 6 are arranged inside the seal cavity;
The size of the evaporator 4 is 2.7 × 0.55 × 0.6m, since the volume of the evaporator 4 is larger, steam The installation of hair device 4 is contemplated that the compatibility of air inlet and the outlet and the wind field in seal cavity 7, and there are air inlets for evaporator 4 Problem, therefore evaporator 4 is mounted remotely to the side of the efflux nozzle of jet stream wind-tunnel 4, the i.e. leftmost side in seal cavity 7.
Since refrigeration unit 3 and the vacuum pump 2 need good ventilation and heat, by 3 He of refrigeration unit The vacuum pump 2 is mounted on outside the seal cavity 7, so as to good ventilation heat dissipation.
The controller 1 is also disposed at the outside of the seal cavity 7;
The blower 6 is arranged in the jet stream wind-tunnel, controls the revolving speed of the blower 6 by controller 1 to control wind The size of speed, the model HL3-2A of the blower, power 15KW;
The controller 1 be also used to by control the refrigeration unit 3, the jet stream wind-tunnel 5 and the vacuum pump 2 come Change temperature, wind speed and the pressure in the seal cavity 7, and the temperature in seal cavity 7 minimum reachable subzero 20 is taken the photograph Family name's degree is to subzero 30 degrees Celsius.
Known highest wind velocity is 50m/s, and highest dynamic pressure is
Maximum stream flow Q=sectional area * speed * 3600=3.14* (0.15)2* 3600*50m/s=12717m3/h。
When selecting contraction section, to obtain flow field more evenly, shrinkage ratio should be greater than 4, select the maximum gauge of contraction section For 800mm.(shrinkage ratio=air inlet open area/outlet open area=π (0.4)2/π(0.15)2=0.711) jet stream wind-tunnel is considered It is to work in a limited space, sinuous flow easy to form, it is difficult to ensure that the uniformity of uniform field, is being considered as higher contraction Than except, lesser cell dimensions are also selected, be 4.8mm.
Specifically, the seal cavity 7 is also provided with door body (not shown), the size of the door body is 1 × 1.5m, Testee enters in seal cavity 7 from door body, and people can enter in seal cavity, carries out operation control.
Specifically, what the seal cavity 7 was made of insulation board, the outer surface of the insulation board is coated with waterproof cement, institute The size for stating seal cavity is 2 × 2.8 × 2.2m.
Specifically, the top of the seal cavity 7 is additionally provided with hanging plate (not shown), offered on the hanging plate more A hole, for hanging instrument to be calibrated.
Specifically, the evaporator 4 specifically includes: the first evaporator, the second evaporator, third evaporator.
Specifically, the diameter of the efflux nozzle of the jet stream wind-tunnel is 300mm.
As shown in Figure 1, the length of the control room of the controller be a, a=2000mm, the wall to evaporator away from It is c, c=805mm from the distance for b, b=1555mm, the evaporator to jet stream wind-tunnel, the length of the jet stream wind-tunnel is d, D=3770mm, the distance of the jet stream wind-tunnel to another wall are c, c=8520mm.
The wind speed based on jet stream wind-tunnel, pressure, temperature calibration system in the utility model have compared with the existing technology Following advantages:
Calibration system in the utility model can be realized by being arranged jet stream wind-tunnel in seal cavity to wind speed, pressure The accurate simulation of power, temperature, and then can be realized and all appts of environmental classes are demarcated, for example, particle sampler exists Cutting efficiency under different wind speed has what variation, variation of the gas apparatus under different pressure and different temperatures, ring Border influence of the exposure storehouse to people, animal, and minimum in the utility model can simulate subzero 20 degrees Celsius to subzero 30 of low temperature Degree Celsius environment, flow through stable section peak flow rate (PFR) be 0.64m/s.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other The difference of embodiment, the same or similar parts in each embodiment may refer to each other.
Specific case used herein is expounded the principles of the present invention and embodiment, above embodiments Explanation be merely used to help understand the method and its core concept of the utility model;Meanwhile for the general technology of this field Personnel, based on the idea of the present invention, there will be changes in the specific implementation manner and application range.In conclusion The content of the present specification should not be construed as a limitation of the present invention.

Claims (8)

1.一种基于射流风洞的风速、压力、温度标定系统,其特征在于,所述系统包括:1. a wind speed, pressure, temperature calibration system based on jet wind tunnel, is characterized in that, described system comprises: 控制器、真空泵、制冷机组、蒸发器、射流风洞、风机、密封腔体;Controller, vacuum pump, refrigeration unit, evaporator, jet wind tunnel, fan, sealed cavity; 所述蒸发器、所述射流风洞以及所述风机设置在所述密封腔体内部;The evaporator, the jet wind tunnel and the fan are arranged inside the sealed cavity; 所述控制器、所述制冷机组以及所述真空泵设置在所述密封腔体的外部;the controller, the refrigeration unit and the vacuum pump are arranged outside the sealed cavity; 所述风机设置在所述射流风洞内;the fan is arranged in the jet wind tunnel; 所述控制器用于通过控制所述制冷机组、所述射流风洞以及所述真空泵来改变所述密封腔体内的温度、风速以及压力。The controller is used for changing the temperature, wind speed and pressure in the sealed cavity by controlling the refrigeration unit, the jet wind tunnel and the vacuum pump. 2.根据权利要求1所述的基于射流风洞的风速、压力、温度标定系统,其特征在于,所述密封腔体还开设有门体,所述门体的尺寸为1×1.5m。2 . The wind speed, pressure and temperature calibration system based on a jet wind tunnel according to claim 1 , wherein the sealed cavity is further provided with a door body, and the size of the door body is 1×1.5m. 3 . 3.根据权利要求1所述的基于射流风洞的风速、压力、温度标定系统,其特征在于,所述密封腔体由保温板构成,所述保温板的外表面涂有防水水泥,所述密封腔体的尺寸为2×2.8×2.2m。3 . The wind speed, pressure and temperature calibration system based on a jet wind tunnel according to claim 1 , wherein the sealed cavity is composed of a thermal insulation board, and the outer surface of the thermal insulation board is coated with waterproof cement, and the The dimensions of the sealed cavity are 2×2.8×2.2m. 4.根据权利要求1所述的基于射流风洞的风速、压力、温度标定系统,其特征在于,所述密封腔体的顶部还设置有挂板,所述挂板上开设有多个孔,用于悬挂待标定仪器。4. The wind speed, pressure and temperature calibration system based on jet wind tunnel according to claim 1, wherein the top of the sealed cavity is further provided with a hanging plate, and the hanging plate is provided with a plurality of holes, Used to hang the instrument to be calibrated. 5.根据权利要求1所述的基于射流风洞的风速、压力、温度标定系统,其特征在于,所述蒸发器具体包括:第一蒸发器、第二蒸发器、第三蒸发器。5 . The wind speed, pressure and temperature calibration system based on a jet wind tunnel according to claim 1 , wherein the evaporator specifically comprises: a first evaporator, a second evaporator, and a third evaporator. 6 . 6.根据权利要求1所述的基于射流风洞的风速、压力、温度标定系统,其特征在于,所述风机的功率为15KW。6 . The wind speed, pressure and temperature calibration system based on a jet wind tunnel according to claim 1 , wherein the power of the fan is 15KW. 7 . 7.根据权利要求1所述的基于射流风洞的风速、压力、温度标定系统,其特征在于,所述射流风洞的射流喷口的直径为300mm。7 . The wind speed, pressure and temperature calibration system based on a jet wind tunnel according to claim 1 , wherein the diameter of the jet nozzle of the jet wind tunnel is 300 mm. 8 . 8.根据权利要求1所述的基于射流风洞的风速、压力、温度标定系统,其特征在于,所述蒸发器的尺寸为2.7×0.55×0.6m,且所述蒸发器位于所述射流风洞的射流喷口的另一侧。8 . The wind speed, pressure and temperature calibration system based on a jet wind tunnel according to claim 1 , wherein the size of the evaporator is 2.7×0.55×0.6m, and the evaporator is located in the jet wind tunnel. 9 . The other side of the hole's jet vent.
CN201821397667.XU 2018-08-29 2018-08-29 A wind speed, pressure and temperature calibration system based on jet wind tunnel Active CN208537061U (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108709666A (en) * 2018-08-29 2018-10-26 中国环境科学研究院 A kind of wind speed based on jet stream wind-tunnel, pressure, temperature calibration system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108709666A (en) * 2018-08-29 2018-10-26 中国环境科学研究院 A kind of wind speed based on jet stream wind-tunnel, pressure, temperature calibration system

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