CN207284926U - Aircraft carbon dioxide Mouse killing trap - Google Patents
Aircraft carbon dioxide Mouse killing trap Download PDFInfo
- Publication number
- CN207284926U CN207284926U CN201721338128.4U CN201721338128U CN207284926U CN 207284926 U CN207284926 U CN 207284926U CN 201721338128 U CN201721338128 U CN 201721338128U CN 207284926 U CN207284926 U CN 207284926U
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- China
- Prior art keywords
- carbon dioxide
- probe
- storehouse
- gas
- pressure
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- 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.)
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Abstract
The utility model provides a kind of aircraft carbon dioxide Mouse killing trap, including mobile platform, be mounted with mobile platform for produce gaseous carbon dioxide generation storehouse, for for gas be pumped into provide power power bin, Comprehensive Control case, carbon dioxide conveyance conduit and gas pump;Occur to be equipped with the first pressure probe for being used for detecting pressure in storehouse and the temperature measuring probe for detection temperature in storehouse, storehouse occurs for connection and the carbon dioxide conveyance conduit of gas pump is equipped with the measurement of gas flow probe for being used to measure carbon dioxide flow rate, gas pump pipe end installation second pressure probe and carbon dioxide concentration probe, first pressure probe, temperature measuring probe, measurement of gas flow probe, gas pump, second pressure probe, carbon dioxide concentration probe are connected with Comprehensive Control case respectively.The beneficial effects of the utility model are:The device cannot be only used for airport aircraft deratization deinsectization, can be used for the place such as confined space, such as container, closed warehouse suffocating treatment.
Description
Technical field
It the utility model is related to aviation to kill mouse field, more specifically to a kind of aircraft carbon dioxide Mouse killing trap.
Background technology
Existing mouse killing method has the equipment of machinery mousing, chemical deratization medicine etc., but rodent poison bait can cause environmental pollution etc.
Into undesirable chain reaction and disastrous effect.Carbon dioxide is heavier than air, is killed mouse with it pollution-free, and effect is good, easy to operate.
But although carbon dioxide is not toxic in itself, excessive concentration can be unfavorable to health.In the reality that ground carries out
Test and show, if somewhere carbon dioxide content is more than 150,0/1,000,000, respiratory system just has the symptom of significant discomfort, institute
With in the space of this relative closure of aircraft, exceeded carbon dioxide content is even more that unfavorable shadow can be caused to health
Ring, so needing the content of carbon dioxide in stringent control cabin.
At present, aircraft entirety suffocating treatment technology lacks, and without easy to operate, perfect in shape and function integration apparatus, deposits
To liquid or solid carbon dioxide gasification process speed is relatively slow, gas be pumped into aircraft method differ, gas point in aircraft
Cloth and concentration lack the problems such as effectively monitoring.
Therefore, how to solve the above problems as the technical problem of those skilled in the art's urgent need to resolve.
Utility model content
The utility model overcomes deficiency of the prior art, there is provided a kind of aircraft carbon dioxide Mouse killing trap, should
Device cannot be only used for airport aircraft deratization deinsectization, can be used for the place such as confined space, such as container, closed warehouse and smokes
Steaming is handled.
The purpose of this utility model is achieved by following technical proposals.
A kind of aircraft carbon dioxide Mouse killing trap, including mobile platform, are mounted with the mobile platform for producing
The generation storehouse of gaseous carbon dioxide, power bin, Comprehensive Control case, carbon dioxide delivery pipe for being pumped into offer power for gas
Road and the gas pump;The gas that storehouse generation occurs is transmitted to the gas pump by the carbon dioxide conveyance conduit,
Be sent to again by the carbon dioxide conveyance conduit in aircraft, it is described occur to be equipped with storehouse for detect pressure in storehouse the
One pressure probe and the temperature measuring probe for detection temperature, the carbon dioxide for connecting the generation storehouse and the gas pump are defeated
Pipeline is sent to be equipped with the measurement of gas flow probe for being used to measure carbon dioxide flow rate, the gas pump pipe end installation second
Pressure probe and carbon dioxide concentration probe, the first pressure probe, the temperature measuring probe, the measurement of gas flow
Probe, the gas pump, second pressure probe, carbon dioxide concentration probe are connected with the Comprehensive Control case respectively.
Further, the side that storehouse occurs is equipped with liquid carbon dioxide entrance, and opposite side is equipped with gas outlet, the outlet
Solenoid valve is equipped with mouthful, the solenoid valve is connected with the Comprehensive Control case.
Further, the Comprehensive Control case is equipped with display panel, with suitable for the pressure in storehouse occurs described in real-time display
Power, it is described occur the temperature in storehouse, in the carbon dioxide conveyance conduit carbon dioxide flow velocity, the carbon dioxide conveyance conduit
The concentration of carbon dioxide in interior pressure and aircraft.
Further, the power bin is diesel engine.
Further, the bottom of the mobile platform is equipped with roller.
The beneficial effects of the utility model are:
Integration apparatus, can be transferred quickly to airport processing scene;
Carbon dioxide is produced rapidly by heating unit, carbon dioxide produces speed and is more than 300m3/ h, equipped with solenoid valve,
Gas storehouse can be closed, can also open, and is connected after unlatching by pipeline with gas pump;
Carbon dioxide can be pumped into aircraft or other large-scale confined spaces by gas pump, be pumped into speed and be more than 300m3/ h,
It can be switched at the same time by pipeline and space be exhausted processing, formed with the negative pressure space of low pressure-sensitive power;
By detecting temperature, pressure, carbon dioxide flow rate and gas concentration lwevel, controlled, adjusted by Comprehensive Control case
The coordinated signals of each several part;
And the pressure in storehouse, the generation temperature in storehouse, the flow velocity of carbon dioxide, titanium dioxide can occur with real-time display
The concentration of carbon dioxide in pressure and aircraft in carbon conveyance conduit;
Pressure and temperature in storehouse occurs for generation storehouse installation first pressure probe and temperature test probe, monitoring;
Gas pipeline installation the measurement of gas flow probe, be pumped into pipe end installation pressure, carbon dioxide concentration probe, two
It is continuously adjustable that storehouse heating unit power occurs for carbonoxide, can adjust manually, it is continuously adjustable to occur the heating unit power in storehouse, can
, can also be by the way that storehouse pressure negative regulator occur to adjust manually, when pressure exceedes warning pressure, heating power declines, and pressure subtracts
It is small, when carbon dioxide flow rate cannot reach normal speed, heating power increase;
Gas pump has automatic start-stop device, as low as guards against pressure when storehouse pressure occurs, can be with emergent stopping.
Brief description of the drawings
Fig. 1 is the utility model structure diagram;
Fig. 2 is each member connection structure figure of the utility model;
In figure:
1st, mobile platform;2nd, storehouse occurs;3rd, power bin;4th, Comprehensive Control case;5th, carbon dioxide conveyance conduit;6th, gas
Pump;7th, roller;8th, liquid carbon dioxide entrance;9th, gas outlet.
Embodiment
The technical solution of the utility model is further described below by specific embodiment.
A kind of aircraft carbon dioxide Mouse killing trap, including mobile platform 1, are mounted with mobile platform 1 for producing gas
The generation storehouse 2 of state carbon dioxide, diesel engine 3, Comprehensive Control case 4, the carbon dioxide conveying for being pumped into offer power for gas
Pipeline 5 and gas pump 6;The gas that storehouse 2 produces occurs gas pump 6 is transmitted to by carbon dioxide conveyance conduit 5, then pass through dioxy
Change carbon conveyance conduit 5 to be sent in aircraft, occur to be equipped with the first pressure probe for being used to detect pressure in storehouse in storehouse 2 and be used for
The temperature measuring probe of detection temperature, storehouse 2 occurs for connection and the carbon dioxide conveyance conduit 5 of gas pump 6 is equipped with for measuring
The measurement of gas flow probe of carbon dioxide flow rate, the gas pump pipe end installation second pressure probe and dense carbon dioxide
Degree probe, the first pressure probe, the temperature measuring probe, the measurement of gas flow probe, the gas pump, second
Pressure probe, carbon dioxide concentration probe are connected with Comprehensive Control case 4 respectively;
It is heating unit in generation storehouse 2, liquid carbon dioxide can be converted into gaseous carbon dioxide;
The first pressure probe and temperature test probe are installed in generation storehouse 2, can monitor the pressure occurred in storehouse 2
And temperature;
Storehouse 2 occurs for connection and the carbon dioxide conveyance conduit 5 of gas pump 6 is popped one's head in equipped with the measurement of gas flow, for surveying
Measure carbon dioxide flow rate;
The pipe end installation second pressure probe of gas pump 6 and carbon dioxide concentration probe, the outlet side of gas pump 6 lead to
Carbon dioxide conveyance conduit 5 is crossed with aircraft to be connected, by detecting from the gas concentration lwevel at the pipe end of gas pump 6,
And extrapolate concentration and accumulative carbon dioxide volume in aircraft;
The side that storehouse occurs is equipped with liquid carbon dioxide entrance 8, and opposite side is equipped with gas outlet 9, is equipped with gas outlet 9
Solenoid valve, the solenoid valve are connected with Comprehensive Control case 4;
Comprehensive Control case 4 is equipped with display panel, with suitable for the pressure in storehouse, the generation occur described in real-time display
The flow velocity of carbon dioxide, pressure and aircraft in carbon dioxide conveyance conduit 5 in the temperature in storehouse, carbon dioxide conveyance conduit 5
The concentration of interior carbon dioxide;
The bottom of mobile platform 1 is equipped with roller 7, can be transferred quickly to airport processing scene.
The course of work of the utility model:The gas that storehouse 2 produces occurs gas is transmitted to by carbon dioxide conveyance conduit 5
Pump 6, then be sent to by carbon dioxide conveyance conduit 5 in aircraft, by monitoring the pressure and temperature occurred in storehouse 2, and
Carbon dioxide in the carbon dioxide flow rate of carbon dioxide conveyance conduit 5, the pressure in carbon dioxide conveyance conduit 5 and aircraft
Concentration, when the pressure occurred in storehouse 2 detected exceedes warning pressure, heating power declines;When the pressure in the generation storehouse 2 detected
Power reduces, and when carbon dioxide flow rate cannot reach normal speed, heating power increase, as low as guards against pressure when 2 pressure of storehouse occurs,
6 emergent stopping of gas pump, the heating unit power in generation storehouse 2 is continuously adjustable, kills mouse until the gas concentration lwevel being passed through meets
Requirement.
One embodiment of the utility model is described in detail above, but the content is only the utility model
Preferred embodiment, it is impossible to be construed as limiting the scope of the utility model.It is all to be made according to application scope of the utility model
All the changes and improvements etc., should all still belong within the patent covering scope of the utility model.
Claims (5)
- A kind of 1. aircraft carbon dioxide Mouse killing trap, it is characterised in that:Including mobile platform, it is mounted with the mobile platform For producing the generation storehouse of gaseous carbon dioxide, for being pumped into the power bin for providing power, Comprehensive Control case, titanium dioxide for gas Carbon conveyance conduit and the gas pump;The gas that storehouse generation occurs is transmitted to described by the carbon dioxide conveyance conduit Gas pump, then be sent to by the carbon dioxide conveyance conduit in aircraft, it is equipped with the generation storehouse and is used to detect in storehouse The first pressure probe of pressure and the temperature measuring probe for detection temperature, connect the two of the generation storehouse and the gas pump Carbonoxide conveyance conduit is equipped with the measurement of gas flow probe for being used to measure carbon dioxide flow rate, the gas pump pipe end Second pressure probe and carbon dioxide concentration probe, the first pressure probe, the temperature measuring probe, the gas are installed Flow measurement probe, the gas pump, the second pressure probe, the carbon dioxide concentration probe are controlled with the synthesis respectively Case processed is connected.
- 2. aircraft carbon dioxide Mouse killing trap according to claim 1, it is characterised in that:The side that storehouse occurs is set Have liquid carbon dioxide entrance, opposite side is equipped with gas outlet, is equipped with solenoid valve at the gas outlet, the solenoid valve with it is described comprehensive Control cabinet is closed to be connected.
- 3. aircraft carbon dioxide Mouse killing trap according to claim 2, it is characterised in that:Set on the Comprehensive Control case There is display panel, with suitable for pressure in storehouse occurs described in real-time display, described the temperature in storehouse, the carbon dioxide occurs The concentration of carbon dioxide in flow velocity, the pressure in the carbon dioxide conveyance conduit and aircraft.
- 4. aircraft carbon dioxide Mouse killing trap according to claim 1, it is characterised in that:The power bin is diesel oil Machine.
- 5. aircraft carbon dioxide Mouse killing trap according to claim 1, it is characterised in that:The bottom of the mobile platform Equipped with roller.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721338128.4U CN207284926U (en) | 2017-10-18 | 2017-10-18 | Aircraft carbon dioxide Mouse killing trap |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721338128.4U CN207284926U (en) | 2017-10-18 | 2017-10-18 | Aircraft carbon dioxide Mouse killing trap |
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Publication Number | Publication Date |
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CN207284926U true CN207284926U (en) | 2018-05-01 |
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ID=62272661
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201721338128.4U Expired - Fee Related CN207284926U (en) | 2017-10-18 | 2017-10-18 | Aircraft carbon dioxide Mouse killing trap |
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CN (1) | CN207284926U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021237290A1 (en) * | 2020-05-26 | 2021-12-02 | Fintran Australia Pty Ltd | System and method for fumigating a vessel with crew protection |
-
2017
- 2017-10-18 CN CN201721338128.4U patent/CN207284926U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2021237290A1 (en) * | 2020-05-26 | 2021-12-02 | Fintran Australia Pty Ltd | System and method for fumigating a vessel with crew protection |
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180501 Termination date: 20201018 |
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CF01 | Termination of patent right due to non-payment of annual fee |