CN209163907U - A kind of aircraft exhaust gas cleaner of aerospace - Google Patents
A kind of aircraft exhaust gas cleaner of aerospace Download PDFInfo
- Publication number
- CN209163907U CN209163907U CN201821328863.1U CN201821328863U CN209163907U CN 209163907 U CN209163907 U CN 209163907U CN 201821328863 U CN201821328863 U CN 201821328863U CN 209163907 U CN209163907 U CN 209163907U
- Authority
- CN
- China
- Prior art keywords
- tail gas
- storehouse
- layer
- main body
- exhaust gas
- 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
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Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A50/00—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE in human health protection, e.g. against extreme weather
- Y02A50/20—Air quality improvement or preservation, e.g. vehicle emission control or emission reduction by using catalytic converters
- Y02A50/2351—Atmospheric particulate matter [PM], e.g. carbon smoke microparticles, smog, aerosol particles, dust
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine management systems
Landscapes
- Filtering Of Dispersed Particles In Gases (AREA)
Abstract
The utility model discloses a kind of aircraft exhaust gas cleaners of aerospace, including apparatus main body, air inlet pipe is provided at the top of apparatus main body, the outer surface of apparatus main body is provided with door, the aircraft exhaust gas cleaner of this kind of aerospace, it is provided with prefiltration storehouse, adsorb storehouse and ionization separator, aircraft tail gas, which enters the first filter layer of prefiltration storehouse, may filter that a part of particle object in tail gas, the second filter layer can be by the water vapor absorption in tail gas simultaneously, it is entered back into absorption storehouse by the tail gas handled for the first time, impeller drives tail gas to generate swirling eddy abutting adsorption layer, adsorption layer can be by the nitrogen oxide absorbent in tail gas at the same time, tail gas enters back into electric separator, particulate matter remaining in tail gas can be adsorbed on the surface of electrically separated layer by electric separator by way of electrostatic, it finally can be by two in tail gas by air purifier Carbonoxide is removed from tail gas, achievees the purpose that tail gas clean-up.
Description
Technical field
The utility model relates to aircraft tail gas purification techniques field, the aircraft tail gas clean-ups of specially a kind of aerospace
Device.
Background technique
Aircraft (aeroplane, airplane) refers to that the power device with a tool or more tool engines generates advance
Thrust or pulling force generate lift by the fixation wing of fuselage, and in the aircraft for overweighting air of endoatmosphere flight, aircraft is most
A kind of common Fixed-Wing, the engine type used according to it can be divided into jet airplane and propeller aeroplane again,
After aircraft invention, aircraft has become the indispensable vehicles of modern civilization.It its deep change and affects
People's lives open people and conquer blue sky history.
For existing aerospaceplane in flight, fuel burns in engine generates exhaust gas, which is exactly us
The aircraft " cloud " seen, that is, the aircraft tail gas for needing to purify, in cruising altitude, which stablizes, and tail gas is easy to be resident,
Ultraviolet radioactive is sufficient here simultaneously, is photochemically reactive ideal place, the main component in tail gas has carbon dioxide, nitrogen oxidation
Object, steam and particulate matter, carbon dioxide can generate direct greenhouse effects, and nitrogen oxides is the predominant emissions of engine, in light
Under chemical reaction, nitrogen oxides can be such that the ozone in upper atmosphere reduces, to reinforce the radiation of sunlight, further speed up complete
Ball warms, while water and particulate matter allow greenhouse effects to be significantly increased at night for the absorption of earth's surface long-wave radiation.
Utility model content
The purpose of this utility model is to provide a kind of aircraft exhaust gas cleaners of aerospace, to solve above-mentioned back
It is proposed that carbon dioxide, steam and particulate matter lead to direct greenhouse effects in scape technology, nitrogen oxides makes the ozone in upper atmosphere
The problem of reduction causes radiation to be reinforced.
To achieve the above object, the utility model provides the following technical solutions: a kind of aircraft tail gas of aerospace is net
Makeup is set, including apparatus main body, and air inlet pipe is provided at the top of described device main body, and the outer surface of described device main body is provided with
Door, the outer surface of the door are fixed with knob, and the side of described device main body is provided with air outlet, described device main body
Interior side is provided with prefiltration storehouse, and air inlet pipe, the inner upper in the prefiltration storehouse are provided at the top of the prefiltration storehouse
It is provided with the first filter layer, the lower inside in the prefiltration storehouse is provided with the second filter layer, under the side in the prefiltration storehouse
Side is connected with absorption storehouse by first pipe, and the inner surface in the absorption storehouse is provided with adsorption layer, and the inside in the absorption storehouse is set
It is equipped with shaft, the outer surface of the shaft is provided with impeller, and the absorption storehouse is provided with ionization along the end direction of second pipe
Separator, the ionization separator are internally provided with ionization separating layer, and side of the ionization separator far from absorption storehouse is logical
It crosses third pipeline and is provided with air purifier, the one of the air purifier is provided with air outlet, and the inside of the air outlet is set
It is equipped with air monitor.
Preferably, the electrically separated layer is provided with multilayer, and it is in " netted ", while electrically separated layer described in multilayer is successively handed over
Mistake arrangement.
Preferably, the impeller is in " arc ", and it is in " arrangement of circular array column-shaped ", while the impeller is closely welded in
The outer surface of shaft.
Preferably, first filter layer passes through fixed bracket dismantling connection in the inside in prefiltration storehouse, and second filters
Layer is provided with multilayer, while the height of second filter layer is higher than the height of first pipe.
Preferably, the door is connected to the outer surface of apparatus main body by articulate, and it is in " arc ".
Preferably, the adsorption layer is made using active carbon.
Compared with prior art, the utility model has the beneficial effects that the aircraft tail gas clean-up dress of this kind of aerospace
It sets, is provided with prefiltration storehouse, absorption storehouse and ionization separator, aircraft tail gas, which enters the first filter layer of prefiltration storehouse, may filter that tail gas
In a part of particle object, while the second filter layer can enter back into the water vapor absorption in tail gas by the tail gas handled for the first time
It adsorbs in storehouse, impeller drives tail gas to generate swirling eddy abutting adsorption layer, and adsorption layer can be by the nitrogen oxidation in tail gas at the same time
Object absorption, tail gas enter back into electric separator, and particulate matter remaining in tail gas can be adsorbed on by electric separator by way of electrostatic
Carbon dioxide in tail gas can finally be removed by air purifier from tail gas, it is net to reach tail gas by the surface of electrically separated layer
The purpose of change.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model;
Fig. 2 is utility model device body sections structural schematic diagram;
Fig. 3 is the utility model impeller side structural schematic diagram.
In figure: 1, apparatus main body, 2, air inlet pipe, 3, hinge, 4, door, 5, knob, 6, air outlet, the 7, first filter layer,
8, prefiltration storehouse, the 9, second filter layer, 10, first pipe, 11, absorption storehouse, 12, adsorption layer, 13, shaft, 14, impeller, 15, the
Two pipelines, 16, ionization separator, 17, ionization separating layer, 18, third pipeline, 19, air purifier, 20, air monitor,
21, fixed bracket.
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.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: a kind of aircraft tail gas clean-up dress of aerospace
It sets, including apparatus main body 1, air inlet pipe 2, hinge 3, door 4, knob 5, air outlet 6, the first filter layer 7, prefiltration storehouse 8, second
Filter layer 9, first pipe 10, absorption storehouse 11, adsorption layer 12, shaft 13, impeller 14, second pipe 15, ionization separator 16, electricity
From separating layer 17, third pipeline 18, air purifier 19, air monitor 20 and fixed bracket 21, the top of apparatus main body 1 is set
It is equipped with air inlet pipe 2, the outer surface of apparatus main body 1 is provided with door 4, and the outer surface of door 4 is fixed with knob 5, apparatus main body 1
Side is provided with air outlet 6, and the interior side of apparatus main body 1 is provided with prefiltration storehouse 8, the top in prefiltration storehouse 8 be provided with into
Tracheae 2, the inner upper in prefiltration storehouse 8 are provided with the first filter layer 7, and the lower inside in prefiltration storehouse 9 is provided with the second filtering
One side-lower of layer 9, prefiltration storehouse 9 is connected with absorption storehouse 11 by first pipe 10, and the inner surface in absorption storehouse 11 is provided with suction
Attached layer 12, absorption storehouse 11 are internally provided with shaft 13, and the outer surface of shaft 13 is provided with impeller 14, and absorption storehouse 11 is along the second pipe
The end direction in road 15 is provided with ionization separator 16, and ionization separator 16 is internally provided with ionization separating layer 17, ionization point
Air purifier 19, a setting of air purifier 19 are provided with by third pipeline 18 far from the side in absorption storehouse 11 from device 16
There is air outlet 6, air outlet 6 is internally provided with air monitor 20.
Preferably, electrically separated layer 17 is provided with multilayer, and it is in " netted ", while the electrically separated layer 17 of multilayer successively staggered row
Cloth, the contact area of tail gas Yu electrically separated layer 17 can be improved in multilayer network structure, staggered to can further improve tail gas and electricity
The contact area of separating layer 17, to promote the effect of electrostatic removing impurities.
Preferably, impeller 14 is in " arc ", and it is in " arrangement of circular array column-shaped ", while impeller 14 is closely welded in shaft
13 outer surface, impeller 14 are rotated with exhaust gas flow, and impeller 14 equally makes tail gas form swirling eddy at the same time, make tail gas
It is close to adsorption layer 12, improves the efficiency of 12 absorbing NOx of adsorption layer.
Preferably, the first filter layer 7 passes through fixed 21 dismantling connection of bracket in the inside in prefiltration storehouse 8, and second filters
Layer 9 is provided with multilayer, while the height of the second filter layer 9 is higher than the height of first pipe 10, and the first filter layer 7 can will be in tail gas
Larger particles filtering, dismantling connection is convenient for changing and cleans, and the second filter layer 9 can reinforce the water vapor absorption in tail gas
Clean-up effect.
Preferably, door 4 is movably connected on the outer surface of apparatus main body 1 by hinge 3, and it is in " arc ", by beating
Storehouse door opening 4 can directly open prefiltration storehouse 8, thus to inside prefiltration storehouse 8 the first filter layer 7 and the second filter layer 9 clean
Or replacement, it is user-friendly, while reducing cleaning replacement cost.
Preferably, adsorption layer 12 is made using active carbon, and active carbon can be by the major pollutants in tail gas but oxidation
Object absorption protects atmospheric air to purify aircraft tail gas.
Working principle: firstly, staff checks whether all parts performance is normal, if finding some component capabilities not just
It after often, should be repaired or replaced in time, after each component capabilities to be checked are normal, device is placed in the exhaust of aircraft tail gas
At pipe, and air inlet pipe 2 is connected to aircrafts exhaust bobbin carriage, powers on start-up operation, aircraft engine work generates tail gas warp
It crosses air inlet pipe 2 to enter in prefiltration storehouse 8, the first filter layer 7 filters the large-volume particulate object in tail gas, using the second filtering
Water vapor absorption in tail gas can be reduced the moisture content in tail gas, pass through first pipe 10 again by the tail gas of prefiltration by layer 9
Into in absorption storehouse 11, tail gas rotates impeller 14, and impeller 14 makes tail gas form swirling eddy while rotation, and tail gas is close to
In 12 apparent motion of adsorption layer, the nitrogen oxide absorbent in tail gas, tail gas are entered ionization point from second pipe again by adsorption layer 12
From device 16, ionizes separating layer 17 and generate electrostatic for the tiny particles content absorption in tail gas, tail gas enters through third pipeline 18 empty again
In gas purifier 19, the carbon dioxide in exhaust gas, purified tail gas can be passed through again air outlet 6 and be discharged by air purifier 19
When, air monitor 20 can detect exhaust gas component, then will test data and be sent to aircraft handling room, provide real time data.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of aircraft exhaust gas cleaner of aerospace, including apparatus main body (1), it is characterised in that: described device master
It is provided at the top of body (1) air inlet pipe (2), the outer surface of described device main body (1) is provided with door (4), the door (4)
Outer surface is fixed with knob (5), and the side of described device main body (1) is provided with air outlet (6), described device main body (1) it is interior
Portion side is provided with prefiltration storehouse (8), is provided with air inlet pipe (2) at the top of the prefiltration storehouse (8), the prefiltration storehouse (8)
Inner upper be provided with the first filter layer (7), the lower inside of the prefiltration storehouse (8) is provided with the second filter layer (9), institute
The side-lower for stating prefiltration storehouse (8) is connected with absorption storehouse (11), the interior table of absorption storehouse (11) by first pipe (10)
Face is provided with adsorption layer (12), and absorption storehouse (11) is internally provided with shaft (13), and the outer surface of the shaft (13) is set
It is equipped with impeller (14), absorption storehouse (11) is provided with ionization separator (16) along the end direction of second pipe (15), described
Being internally provided with for ionization separator (16) ionizes separating layer (17), and the one of separate absorption storehouse (11) of ionization separator (16)
Side is provided with air purifier (19) by third pipeline (18), and the one of the air purifier (19) is provided with air outlet (6),
The air outlet (6) is internally provided with air monitor (20).
2. a kind of aircraft exhaust gas cleaner of aerospace according to claim 1, it is characterised in that: the ionization
Separating layer (17) is provided with multilayer, and it is in " netted ", while ionization separating layer (17) described in multilayer is successively staggered.
3. a kind of aircraft exhaust gas cleaner of aerospace according to claim 1, it is characterised in that: the impeller
(14) it is in " arc ", and it is in " arrangement of circular array column-shaped ", while the impeller (14) is closely welded in the appearance of shaft (13)
Face.
4. a kind of aircraft exhaust gas cleaner of aerospace according to claim 1, it is characterised in that: described first
Filter layer (7) passes through fixed bracket (21) dismantling connection in the inside of prefiltration storehouse (8), and the second filter layer (9) be provided with it is more
Layer, while the height of second filter layer (9) is higher than the height of first pipe (10).
5. a kind of aircraft exhaust gas cleaner of aerospace according to claim 1, it is characterised in that: the door
(4) outer surface of apparatus main body (1) is movably connected on by hinge (3), and it is in " arc ".
6. a kind of aircraft exhaust gas cleaner of aerospace according to claim 1, it is characterised in that: the absorption
Layer (12) is made using active carbon.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821328863.1U CN209163907U (en) | 2018-08-17 | 2018-08-17 | A kind of aircraft exhaust gas cleaner of aerospace |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821328863.1U CN209163907U (en) | 2018-08-17 | 2018-08-17 | A kind of aircraft exhaust gas cleaner of aerospace |
Publications (1)
Publication Number | Publication Date |
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CN209163907U true CN209163907U (en) | 2019-07-26 |
Family
ID=67329696
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201821328863.1U Expired - Fee Related CN209163907U (en) | 2018-08-17 | 2018-08-17 | A kind of aircraft exhaust gas cleaner of aerospace |
Country Status (1)
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CN (1) | CN209163907U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112807889A (en) * | 2020-12-24 | 2021-05-18 | 中国科学院长春光学精密机械与物理研究所 | Air filter and photoelectric equipment |
-
2018
- 2018-08-17 CN CN201821328863.1U patent/CN209163907U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112807889A (en) * | 2020-12-24 | 2021-05-18 | 中国科学院长春光学精密机械与物理研究所 | Air filter and photoelectric equipment |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190726 Termination date: 20200817 |
|
CF01 | Termination of patent right due to non-payment of annual fee |