CN206627417U - A kind of gas attack experimental facilities - Google Patents
A kind of gas attack experimental facilities Download PDFInfo
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- CN206627417U CN206627417U CN201720318467.XU CN201720318467U CN206627417U CN 206627417 U CN206627417 U CN 206627417U CN 201720318467 U CN201720318467 U CN 201720318467U CN 206627417 U CN206627417 U CN 206627417U
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- gas
- fuselage cover
- camera
- experimental facilities
- chamber door
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Abstract
The utility model discloses a kind of gas attack experimental facilities, including fuselage cover, camera and gas generating unit, the inner top side of the fuselage cover is provided with a camera, a temperature sensor and a humidity sensor are installed at the top of the interior side of the fuselage cover, the bottom inside of the fuselage cover is provided with a heater, the opposite side of four pipelines is connected with blending bin, the blending bin is connected with turbine, the side of the turbine is provided with a motor, the bottom of the turbine is provided with an outlet pipe, a purifying box is provided with the top of the fuselage cover, one mounting table is installed inside the fuselage cover, an experiment chamber door is also equipped with the outside of the fuselage cover.The gas attack experimental facilities is provided with a camera, and camera is rotatable device, can record change of the experiment slice in experimentation, and shooting is convenient, and the present apparatus uses more convenient, design more hommization.
Description
Technical field
Chemical engineering experiment equipment technical field is the utility model is related to, specially a kind of gas attack experimental facilities.
Background technology
Mixed gas experiment is mainly used in determining mixed gas existing for the indoor environment of work or storage to electrotechnical, electronic
The influence of product element, system and material, particularly contact are influenceed with connector by these mixing gas attacks.Gaseous mixture
Body experimental system can be assembled into a subsystem respectively or be assembled into a complete system, rotten according to flowing mixed gas
The information given by system test is lost, can be helped to carry out material, manufacturing process and member on the basis of corrosion resistance is compared to each other
The selection of part design.
Equipment for mixed gas experiment has to comply with the requirement of flowing gas corrosion test, in the casing of specified volume
Portion persistently imports certain density mixed gas, and material or product are carried out in the case of making concentration, temperature, relative humidity constant
Corrosion test, reappear the destructiveness that material or product are subjected in the range of certain time.System can be used for examining material
And its ability of the anti-mixed gas corrosion of overcoat, and the processing quality of similar overcoat compares, and may also be used for examining
The ability of some anti-mixed gas corrosion of product.
Existing gas attack experimental facilities in-convenience in use, change of the experiment slice in experimentation can not record, need
Manually to observe, observation is relatively tired for a long time.
Utility model content
The purpose of this utility model is to provide a kind of gas attack experimental facilities, to solve to propose in above-mentioned background technology
Existing gas attack experimental facilities in-convenience in use, change of the experiment slice in experimentation can not be recorded, it is necessary to artificial
Observation, the problem of relatively tired is observed for a long time.
To achieve the above object, the utility model provides following technical scheme:A kind of gas attack experimental facilities, including machine
Body shell, camera, temperature sensor, humidity sensor, heater, water tank, steam generator, turbine, motor, valve,
Gas generating unit, gas chamber door, gas cabinet, gas-metering device, purifying box, blending bin, mounting table and experiment chamber door, it is described
The inner top side of fuselage cover is provided with a camera, and a temperature is provided with the top of the interior side of the fuselage cover and is passed
Sensor and a humidity sensor, the bottom inside of the fuselage cover are provided with a heater, the fuselage cover
Bottom inside is also equipped with a water tank, and the top side of the water tank is provided with a steam generator, and the one of the fuselage cover
Side is provided with a gas cabinet, and the gas cabinet is internally provided with four gas generating units, is also equipped with the gas cabinet
One gas chamber door, the side of four gas generating units are provided with a pipeline, one are provided with the pipeline
Valve and a gas-metering device, the opposite side of four pipelines are connected with blending bin, and the blending bin is connected with turbine,
The side of the turbine is provided with a motor, and the bottom of the turbine is provided with an outlet pipe, the fuselage cover
Top is provided with a purifying box, and a mounting table is provided with inside the fuselage cover, is also installed on the outside of the fuselage cover
There is an experiment chamber door.
Preferably, one layer of sealing joint strip is posted inside the gas chamber door and experiment chamber door.
Preferably, the mounting table is network structure.
Preferably, the camera is rotatable device, and angle rotatable is 360 °.
Preferably, a cloche is provided with outside the camera.
Preferably, the purifying box is built with absorbent charcoal material.
Compared with prior art, the beneficial effects of the utility model are:The gas attack experimental facilities is provided with a shooting
Head, camera are rotatable device, can record change of the experiment slice in experimentation, and shooting is convenient, outside camera
Be provided with a cloche, internal toxic gas corrosion camera can be prevented, mounting table is network structure, be easy to internal gas and
Experiment slice contacts, and improves the degree of accuracy, posts one layer of sealing joint strip inside gas chamber door and experiment chamber door, good airproof performance, prevent
Toxic gas leaks, and the present apparatus uses more convenient, design more hommization.
Brief description of the drawings
Fig. 1 is the utility model structure diagram;
Fig. 2 is the utility model mounting table overlooking the structure diagram.
In figure:Fuselage cover -1;Camera -2;Temperature sensor -3;Humidity sensor -4;Heater -5;Water tank -6;
Steam generator -7;Turbine -8;Motor -9;Valve -10;Gas generating unit -11;Gas chamber door -12;Gas cabinet -13;Gas
Metering device -14;Purifying box -15;Blending bin -16;Mounting table -17;Test chamber door -18.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Fig. 1-2 is referred to, the utility model provides a kind of technical scheme:A kind of gas attack experimental facilities, including fuselage
Shell 1, camera 2, temperature sensor 3, humidity sensor 4, heater 5, water tank 6, steam generator 7, turbine 8, motor
9th, valve 10, gas generating unit 11, gas chamber door 12, gas cabinet 13, gas-metering device 14, purifying box 15, blending bin 16,
Mounting table 17 and experiment chamber door 18, the inner top side of fuselage cover 1 are provided with a camera 2, the interior side of fuselage cover 1
Top is provided with a temperature sensor 3 and a humidity sensor 4, and the bottom inside of fuselage cover 1 is provided with a heating
Device 5, the bottom inside of fuselage cover 1 are also equipped with a water tank 6, and the top side of water tank 6 is provided with a steam generator 7,
The side of fuselage cover 1 is provided with a gas cabinet 13, and gas cabinet 13 is internally provided with four gas generating units 11, gas cabinet
A gas chamber door 12 is also equipped with 13, the side of four gas generating units 11 is provided with a pipeline, pacified on pipeline
Equipped with a valve 10 and a gas-metering device 14, the opposite side of four pipelines is connected with blending bin 16, blending bin 16 with
Turbine 8 connects, and the side of turbine 8 is provided with a motor 9, and the bottom of turbine 8 is provided with an outlet pipe, fuselage cover 1
Top be provided with a purifying box 15, a mounting table 17 is installed, the outside of fuselage cover 1 is also installed inside fuselage cover 1
There is an experiment chamber door 18.
In above-described embodiment, specifically, posting one layer of sealing joint strip inside gas chamber door 12 and experiment chamber door 18, seal
Property is good, prevents toxic gas from leaking;
In above-described embodiment, specifically, mounting table 17 is network structure, it is easy to internal gas and experiment slice to contact, improves
The degree of accuracy;
In above-described embodiment, specifically, camera 2 is rotatable device, angle rotatable is 360 °, and shooting is convenient;
In above-described embodiment, specifically, being provided with a cloche outside camera 2, it can prevent that internal toxic gas is rotten
Lose camera;
In above-described embodiment, specifically, purifying box 15 can be filtered tentatively built with absorbent charcoal material when gas discharges
Toxic gas.
Operation principle:Experiment chamber door 18 is opened, experiment slice is placed on mounting table 17, experiment chamber door 18 is closed, uses control
Panel processed sets the burst size of four kinds of gas, and control gas generating unit 11 is run, and valve 10 is opened, and gas-metering device 14 is counted
Gas flow is calculated, when reaching target flow, control valve 10 is closed, and gas enters in blending bin 16, then mixed by turbine 8
Outwards sprayed after conjunction, into experimental box in contact and react with the experiment slice on mounting table 17, the camera 2 at top can be remembered
Lower change of the experiment slice in experimentation is recorded, a cloche is provided with outside camera 2, can prevent that internal toxic gas is rotten
Erosion camera controls the operation of steam generator during humidification, tested, it is necessary to heat the operation of time control refrigerating/heating apparatus 5
Cheng Hou, gas is extracted out by purifying box 15, open experiment chamber door 18 and take out experiment slice, and then complete a series of operation stream
Journey.
In summary, although the utility model is described in detail with reference to the foregoing embodiments, for this area
For technical staff, it can still modify to the technical scheme described in foregoing embodiments, or to which part
Technical characteristic carries out equivalent substitution, all within the spirit and principles of the utility model, any modification for being made, equivalent substitution,
Improve etc., it should be included within the scope of protection of the utility model.
Claims (6)
1. a kind of gas attack experimental facilities, including fuselage cover (1), camera (2), temperature sensor (3), humidity sensor
(4), heater (5), water tank (6), steam generator (7), turbine (8), motor (9), valve (10), gas generating unit
(11), gas chamber door (12), gas cabinet (13), gas-metering device (14), purifying box (15), blending bin (16), mounting table
(17) and experiment chamber door (18), it is characterised in that:The inner top side of the fuselage cover (1) is provided with a camera (2), institute
State and a temperature sensor (3) and a humidity sensor (4), the machine are installed at the top of the interior side of fuselage cover (1)
The bottom inside of body shell (1) is provided with a heater (5), and the bottom inside of the fuselage cover (1) is also equipped with one
Individual water tank (6), the top side of the water tank (6) are provided with a steam generator (7), and the side of the fuselage cover (1) is set
There is a gas cabinet (13), the gas cabinet (13) is internally provided with four gas generating units (11), the gas cabinet (13)
On be also equipped with a gas chamber door (12), the side of four gas generating units (11) is provided with a pipeline, institute
State and a valve (10) and a gas-metering device (14) are installed on pipeline, the opposite side of four pipelines and blending bin
(16) connect, the blending bin (16) is connected with turbine (8), and the side of the turbine (8) is provided with a motor (9), described
The bottom of turbine (8) is provided with an outlet pipe, and a purifying box (15), institute are provided with the top of the fuselage cover (1)
State and a mounting table (17) is installed inside fuselage cover (1), an experiment chamber door is also equipped with the outside of the fuselage cover (1)
(18)。
A kind of 2. gas attack experimental facilities according to claim 1, it is characterised in that:The gas chamber door (12) and reality
One layer of sealing joint strip is posted inside tryoff door (18).
A kind of 3. gas attack experimental facilities according to claim 1, it is characterised in that:The mounting table (17) is netted
Structure.
A kind of 4. gas attack experimental facilities according to claim 1, it is characterised in that:The camera (2) is to revolve
Rotary device, angle rotatable are 360 °.
A kind of 5. gas attack experimental facilities according to claim 1, it is characterised in that:Set outside the camera (2)
It is equipped with a cloche.
A kind of 6. gas attack experimental facilities according to claim 1, it is characterised in that:The purifying box (15) built with
Absorbent charcoal material.
Priority Applications (1)
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CN201720318467.XU CN206627417U (en) | 2017-03-29 | 2017-03-29 | A kind of gas attack experimental facilities |
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CN201720318467.XU CN206627417U (en) | 2017-03-29 | 2017-03-29 | A kind of gas attack experimental facilities |
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CN206627417U true CN206627417U (en) | 2017-11-10 |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112666068A (en) * | 2020-12-26 | 2021-04-16 | 华测检测认证集团股份有限公司 | Mixed gas corrosion test box |
-
2017
- 2017-03-29 CN CN201720318467.XU patent/CN206627417U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112666068A (en) * | 2020-12-26 | 2021-04-16 | 华测检测认证集团股份有限公司 | Mixed gas corrosion test box |
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