CN220986389U - Aviation ground air conditioning unit with air filtering function - Google Patents
Aviation ground air conditioning unit with air filtering function Download PDFInfo
- Publication number
- CN220986389U CN220986389U CN202323010059.2U CN202323010059U CN220986389U CN 220986389 U CN220986389 U CN 220986389U CN 202323010059 U CN202323010059 U CN 202323010059U CN 220986389 U CN220986389 U CN 220986389U
- Authority
- CN
- China
- Prior art keywords
- air
- fixedly connected
- side end
- filter
- conditioning unit
- 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.)
- Active
Links
- 238000001914 filtration Methods 0.000 title claims abstract description 60
- 238000004378 air conditioning Methods 0.000 title claims abstract description 34
- 230000007246 mechanism Effects 0.000 claims abstract description 30
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 238000004140 cleaning Methods 0.000 description 6
- 238000012423 maintenance Methods 0.000 description 6
- 235000017166 Bambusa arundinacea Nutrition 0.000 description 5
- 235000017491 Bambusa tulda Nutrition 0.000 description 5
- 241001330002 Bambuseae Species 0.000 description 5
- 235000015334 Phyllostachys viridis Nutrition 0.000 description 5
- 239000011425 bamboo Substances 0.000 description 5
- 238000009434 installation Methods 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 230000004048 modification Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000003086 colorant Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 238000012552 review Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Landscapes
- Filtering Of Dispersed Particles In Gases (AREA)
Abstract
The utility model relates to the technical field of aviation ground guarantee equipment, and discloses an aviation ground air conditioning unit with an air filtering function, wherein an air inlet component is arranged at the left side end and the right side end of a box body, a mounting frame is fixedly connected at the left side end and the right side end of the inside of the box body, a plurality of limiting mechanisms are arranged in the box body, a filtering mechanism is arranged in the box body, the filtering mechanism comprises a filtering component, a rebound component is arranged between the side ends of the filtering component, and the filtering mechanism is mounted between the two mounting frames.
Description
Technical Field
The utility model relates to the technical field of aviation ground guaranteeing equipment, in particular to an aviation ground air conditioning unit with an air filtering function.
Background
The aircraft ground air conditioning unit is taken as ground supporting equipment of an airport, and becomes one of necessary equipment of bridge-mounted equipment. Daily maintenance and regular overhauling are basic means for ensuring that air conditioning equipment is good, prolonging the service life of the equipment and obtaining the best running economic benefit and return on investment. The aircraft ground air conditioning system refers to air conditioning equipment for providing fresh air for an aircraft parked on the ground, and in order to ensure the quality of the conveying air, air filtration is carried out by adopting an air filtration device of an aircraft ground air conditioning unit.
The air filter device of the existing aircraft ground air conditioning unit is mostly an independent device and is usually externally connected to the outside of an aircraft ground air conditioning assembly, the air filter device is generally installed in a shell through a plurality of bolts, and the air filter device can be detached integrally only by screwing the bolts one by one during maintenance or cleaning, so that the installation and detachment efficiencies of the air filter device are not high enough, and maintenance and cleaning equipment are very troublesome.
Disclosure of utility model
This section is intended to outline some aspects of embodiments of the utility model and to briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section as well as in the description of the utility model and in the title of the utility model, which may not be used to limit the scope of the utility model.
In view of the above-mentioned existing air conditioning units with air filtering function, the air filtering device of the air conditioning unit on the ground of the aircraft is usually an independent device and is usually externally connected to the outside of the air conditioning unit on the ground of the aircraft, and the air filtering device is generally installed in the housing through a plurality of bolts, and the air filtering device is detached entirely only by unscrewing the bolts one by one during maintenance or cleaning, so that the efficiency of installing and removing the air filtering device is not high enough, resulting in the trouble of maintaining and cleaning equipment.
Therefore, the utility model aims to provide an aviation ground air conditioning unit with an air filtering function, which aims to: the efficiency of installing and dismantling air filter device is improved, and the air filter device is simpler and quicker when being installed and dismantled, thereby being convenient for maintenance and cleaning equipment.
In order to solve the technical problems, the utility model provides the following technical scheme: the utility model provides an aviation ground air conditioning unit with air filtering function, includes the box, the side of box rotates and is provided with the chamber door, two sides all are equipped with the subassembly that admits air about the box, two sides all fixedly connected with installing frame about the box is inside, the inside of box is equipped with a plurality of stop gear, the box is inside to be equipped with filtering mechanism, filtering mechanism includes filter unit, be equipped with the resilience subassembly between the side of filter unit, the filter constructs and installs between two installing frames.
As a preferable scheme of the aviation ground air conditioning unit with the air filtering function, the utility model comprises the following steps: the limiting mechanism comprises a hollow rod, the hollow rod is fixedly connected to the inner side end of the box body, a circular plate is arranged in the hollow rod, the side end of the circular plate is fixedly connected with a round rod, the outer end of the round rod is sleeved with a first spring, the side end of the round rod is fixedly connected with a straight plate, and the side end of the straight plate is fixedly connected with a pull rod.
As a preferable scheme of the aviation ground air conditioning unit with the air filtering function, the utility model comprises the following steps: the filter assembly comprises a first filter cylinder, a ring plate is arranged in the first filter cylinder, a second filter cylinder is fixedly connected to the side end of the ring plate, a third filter cylinder is fixedly connected to the side end of the second filter cylinder, connecting plates are fixedly connected to the side end of the first filter cylinder and the side end of the third filter cylinder, and a plurality of straight grooves are formed in each of the side ends of the connecting plates in a penetrating mode.
As a preferable scheme of the aviation ground air conditioning unit with the air filtering function, the utility model comprises the following steps: the shape of the filter cartridge III is in a conical shape.
As a preferable scheme of the aviation ground air conditioning unit with the air filtering function, the utility model comprises the following steps: the rebound assembly comprises a plurality of fixing rods, the fixing rods are fixedly connected to the inner side end of the first filter cylinder, fixing plates are fixedly connected between the side ends of the fixing rods, the shape of each fixing plate is annular, and a second spring is sleeved at the outer end of each fixing rod.
As a preferable scheme of the aviation ground air conditioning unit with the air filtering function, the utility model comprises the following steps: the annular plate is sleeved at the outer end of each fixing rod.
As a preferable scheme of the aviation ground air conditioning unit with the air filtering function, the utility model comprises the following steps: the air inlet assembly comprises an air inlet pipe, the air inlet pipe is fixedly connected to the side end of the box body, and a fan is fixedly installed on the inner side of the air inlet pipe.
The utility model has the beneficial effects that:
According to the utility model, through the cooperation arrangement of the limiting mechanism, the filtering component and the rebound component, the straight plate rotates towards the direction of the straight groove by rotating each pulling plate, at the moment, when the straight plate is not propped against the limiting connecting plate any more, the first spring can rebound against the circular plate and drive the circular rod to enter the hollow rod, the straight plate enters the straight groove, at the moment, the connecting plate at the three side ends of the filtering cylinder is pulled, so that the annular plate moves at the outer end of each fixing rod and props against the second spring to shrink, at the moment, the filtering cylinder three moves towards the direction of the filtering cylinder one, and when the connecting plate at the three side ends of the filtering cylinder is not blocked at the outer end of the mounting frame any more, the filtering mechanism can be integrally removed, so that the filtering mechanism is dismounted, and the filtering mechanism is mounted by no special tool, and the mounting and dismounting modes are simple and quick, so that the efficiency of mounting and dismounting of the air filtering device is improved, and the mounting and dismounting are simpler and quicker, and the maintenance and cleaning equipment are facilitated.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed in the description of the embodiments will be briefly described below, it being obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art. Wherein:
Fig. 1 is an exploded perspective view of an air conditioning unit for an aircraft floor with air filtering.
Fig. 2 is a schematic diagram of an internal structure of an air conditioning unit for aviation ground with air filtering function.
Fig. 3 is a schematic diagram of an exploded view of a filter cartridge of an air conditioning unit for an aircraft floor with air filtration.
Fig. 4 is a schematic view of a partial enlarged structure of a in fig. 1.
In the figure:
1. A case; 101. a door; 102. a mounting frame; 2. an air inlet pipe; 201. a blower; 3. a hollow rod; 301. a circular plate; 302. a round bar; 303. a first spring; 304. a straight plate; 305. a pull rod; 4. a first filter cartridge; 401. a ring plate; 402. a second filter cylinder; 403. a filter cartridge III; 404. a connecting plate; 405. a straight groove; 5. a fixed rod; 501. a fixing plate; 502. and a second spring.
Detailed Description
In order that the above-recited objects, features and advantages of the present utility model will become more readily apparent, a more particular description of the utility model will be rendered by reference to specific embodiments thereof which are illustrated in the appended drawings.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present utility model, but the present utility model may be practiced in other ways other than those described herein, and persons skilled in the art will readily appreciate that the present utility model is not limited to the specific embodiments disclosed below.
Further, reference herein to "one embodiment" or "an embodiment" means that a particular feature, structure, or characteristic can be included in at least one implementation of the utility model. The appearances of the phrase "in one embodiment" in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments.
Further, in describing the embodiments of the present utility model in detail, the cross-sectional view of the device structure is not partially enlarged to a general scale for convenience of description, and the schematic is only an example, which should not limit the scope of protection of the present utility model. In addition, the three-dimensional dimensions of length, width and depth should be included in actual fabrication.
Referring to fig. 1-4, the present utility model provides a technical solution: the utility model provides an aviation ground air conditioning unit with air filtering function, including box 1, the side rotation of box 1 is provided with chamber door 101, two side all is equipped with the subassembly that admits air about box 1, the subassembly that admits air includes intake pipe 2, intake pipe 2 fixed connection is in the side of box 1, the inboard fixed mounting of intake pipe 2 has fan 201, the inside equal fixedly connected with installing frame 102 of two sides about box 1, the inside of box 1 is equipped with a plurality of stop gear, the inside filtering mechanism that is equipped with of box 1, filtering mechanism includes the filter component, be equipped with the resilience subassembly between the side of filtering component, filtering mechanism installs between two installing frames 102, through setting up in with the air exhaust box 1 in the air inlet pipe 2, air is got into in the filtering mechanism through fan 201 afterwards, air after the filtration carries into the aircraft again through external equipment, thereby improve the air quality in the aircraft, the cooperation setting of stop gear, filtering component and resilience subassembly, make and install filter mechanism's dismantlement and installation all need not install through specialized tool, installation and dismantlement mode are simple and convenient and quick, thereby have improved air filter efficiency and easy to detach and easy to install and repair when having made the equipment.
As an implementation manner in this embodiment, as shown in fig. 1 and fig. 4, the limiting mechanism includes a hollow rod 3, the hollow rod 3 is fixedly connected to an inner side end of the box body 1, a circular plate 301 is disposed in the hollow rod 3, a circular rod 302 is fixedly connected to a side end of the circular plate 301, a first spring 303 is sleeved on an outer end of the circular rod 302, a straight plate 304 is fixedly connected to a side end of the circular rod 302, a pull rod 305 is fixedly connected to a side end of the straight plate 304, and the limiting mechanism can fix and detach the filter assembly.
As shown in fig. 2 and 3, as an implementation manner in this embodiment, the filter assembly includes a first filter cartridge 4, a ring plate 401 is disposed inside the first filter cartridge 4, a second filter cartridge 402 is fixedly connected to a side end of the ring plate 401, a third filter cartridge 403 is fixedly connected to a side end of the second filter cartridge 402, a connecting plate 404 is fixedly connected to side ends of the first filter cartridge 4 and the third filter cartridge 403, the third filter cartridge 403 is in a conical shape, the connecting plates 404 are conveniently abutted, a plurality of straight grooves 405 are formed in the side ends of each connecting plate 404 in a penetrating manner, and in implementation, by rotating each pulling plate, the straight plates 304 rotate towards the direction of the straight grooves 405, at this time, when the straight plates 304 do not press the limiting connecting plates 404 any more, the first springs 303 rebound against the circular plates 301, and drive the circular rods 302 to enter the hollow rods 3, and the straight plates 304 enter the straight grooves 405, so that the filter assembly is convenient to detach.
Further, the rebound assembly comprises a plurality of fixing rods 5, the plurality of fixing rods 5 are fixedly connected to the inner side end of the first filter cylinder 4, a fixing plate 501 is fixedly connected between the side ends of the plurality of fixing rods 5, the shape of the fixing plate 501 is annular, a second spring 502 is sleeved at the outer end of each fixing rod 5, a ring plate 401 is sleeved at the outer end of each fixing rod 5, the ring plate 401 moves at the outer end of each fixing rod 5 by pulling a connecting plate 404 of the side end of the third filter cylinder, the second spring 502 is pressed to shrink, the third filter cylinder 403 moves towards the first filter cylinder 4 at the moment, and when the connecting plate 404 of the side end of the third filter cylinder is not clamped at the outer end of the mounting frame 102, the whole filter mechanism can be removed, so that the disassembly of the filter mechanism is completed, and the disassembly and the assembly of the filter mechanism do not need to be carried out through special tools.
Working principle: this aviation ground air conditioning unit with air filtering function, through setting up two intake pipes 2 afterwards, in the box 1 is advanced with the air through fan 201, air gets into in the filtering mechanism and realizes air filtration afterwards, air after filtering carries into the aircraft again through external equipment, thereby improve the air quality in the aircraft, then as shown in fig. 1 and fig. 4, filtering mechanism is in the state of installation completion this moment, when need dismantle filtering mechanism, through rotating every arm-tie, make straight board 304 rotate towards the direction of straight flute 405, when straight board 304 no longer supports and presses spacing connecting plate 404, at this moment, spring one 303 will spring back against plectane 301, and drive in round bar 302 gets into hollow bar 3, straight board 304 gets into straight flute 405, this moment is through pulling the connecting plate 404 of straining a section of thick bamboo three 403 side ends, make annular plate 401 remove at every dead lever 5 outer end, and press spring two 502 to shrink, straining a section of thick bamboo three 403 and remove towards straining a section of thick bamboo one direction of thick bamboo 4 this moment, and when straining the connecting plate 404 of a section thick bamboo three side ends no longer blocks at the outer end of installing frame 102, just can take down filtering mechanism wholly, thereby dismantle the filter mechanism and detach and install and detach the device and install and detach the device more conveniently and fast and conveniently.
It is important to note that the construction and arrangement of the utility model as shown in the various exemplary embodiments is illustrative only. Although only a few embodiments have been described in detail in this disclosure, those skilled in the art who review this disclosure will readily appreciate that many modifications are possible (e.g., variations in sizes, dimensions, structures, shapes and proportions of the various elements, values of parameters (e.g., temperature, pressure, etc.), mounting arrangements, use of materials, colors, orientations, etc.) without materially departing from the novel teachings and advantages of the subject matter described in this application. For example, elements shown as integrally formed may be constructed of multiple parts or elements, the position of elements may be reversed or otherwise varied, and the nature or number of discrete elements or positions may be altered or varied. Accordingly, all such modifications are intended to be included within the scope of present utility model. The order or sequence of any process or method steps may be varied or re-sequenced according to alternative embodiments. In the claims, any means-plus-function clause is intended to cover the structures described herein as performing the recited function and not only structural equivalents but also equivalent structures. Other substitutions, modifications, changes and omissions may be made in the design, operating conditions and arrangement of the exemplary embodiments without departing from the scope of the present utility models. Therefore, the utility model is not limited to the specific embodiments, but extends to various modifications that nevertheless fall within the scope of the appended claims.
Furthermore, in an effort to provide a concise description of the exemplary embodiments, all features of an actual implementation may not be described (i.e., those not associated with the best mode presently contemplated for carrying out the utility model, or those not associated with practicing the utility model).
It should be noted that the above embodiments are only for illustrating the technical solution of the present utility model and not for limiting the same, and although the present utility model has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the technical solution of the present utility model may be modified or substituted without departing from the spirit and scope of the technical solution of the present utility model, which is intended to be covered in the scope of the claims of the present utility model.
Claims (7)
1. The utility model provides an aviation ground air conditioning unit with air filtering capability, includes box (1), the side of box (1) rotates and is provided with chamber door (101), both sides end all is equipped with the subassembly of admitting air, its characterized in that about box (1): the novel filter is characterized in that the left side end and the right side end of the box body (1) are fixedly connected with mounting frames (102), a plurality of limiting mechanisms are arranged in the box body (1), a filter mechanism is arranged in the box body (1) and comprises a filter assembly, a rebound assembly is arranged between the side ends of the filter assembly, and the filter mechanism is mounted between the two mounting frames (102).
2. An air conditioning unit for aviation ground having an air filtering function according to claim 1, wherein: the limiting mechanism comprises a hollow rod (3), the hollow rod (3) is fixedly connected to the inner side end of the box body (1), a circular plate (301) is arranged in the hollow rod (3), a round rod (302) is fixedly connected to the side end of the circular plate (301), a first spring (303) is sleeved on the outer end of the round rod (302), a straight plate (304) is fixedly connected to the side end of the round rod (302), and a pull rod (305) is fixedly connected to the side end of the straight plate (304).
3. An air conditioning unit for aviation ground having an air filtering function according to claim 1, wherein: the filter assembly comprises a first filter cylinder (4), a ring plate (401) is arranged in the first filter cylinder (4), a second filter cylinder (402) is fixedly connected to the side end of the ring plate (401), a third filter cylinder (403) is fixedly connected to the side end of the second filter cylinder (402), connecting plates (404) are fixedly connected to the side end of the first filter cylinder (4) and the side end of the third filter cylinder (403), and a plurality of straight grooves (405) are formed in each of the side ends of the connecting plates (404) in a penetrating mode.
4. An air conditioning unit for aviation ground having an air filtering function according to claim 3, characterized in that: the shape of the filter cartridge III (403) is in a conical shape.
5. An air conditioning unit for aviation ground having an air filtering function according to claim 3, characterized in that: the rebound assembly comprises a plurality of fixing rods (5), the fixing rods (5) are fixedly connected to the inner side ends of the first filter cylinder (4), fixing plates (501) are fixedly connected between the side ends of the fixing rods (5), the shape of each fixing plate (501) is annular, and springs II (502) are sleeved at the outer ends of the fixing rods (5).
6. An air conditioning unit for aviation ground having an air filtering function according to claim 3, characterized in that: the annular plate (401) is sleeved at the outer end of each fixing rod (5).
7. An air conditioning unit for aviation ground having an air filtering function according to claim 1, wherein: the air inlet assembly comprises an air inlet pipe (2), the air inlet pipe (2) is fixedly connected to the side end of the box body (1), and a fan (201) is fixedly arranged on the inner side of the air inlet pipe (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323010059.2U CN220986389U (en) | 2023-11-08 | 2023-11-08 | Aviation ground air conditioning unit with air filtering function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323010059.2U CN220986389U (en) | 2023-11-08 | 2023-11-08 | Aviation ground air conditioning unit with air filtering function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220986389U true CN220986389U (en) | 2024-05-21 |
Family
ID=91069820
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323010059.2U Active CN220986389U (en) | 2023-11-08 | 2023-11-08 | Aviation ground air conditioning unit with air filtering function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220986389U (en) |
-
2023
- 2023-11-08 CN CN202323010059.2U patent/CN220986389U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN220986389U (en) | Aviation ground air conditioning unit with air filtering function | |
| CN216457295U (en) | Raw material filtering device for alcohol-based fuel production | |
| CN210693105U (en) | SVG power cabinet inlet air channel dust filtration structure | |
| CN210049975U (en) | Air filter applied to new energy automobile hydraulic system | |
| CN219974657U (en) | Make things convenient for car air cleaner of dismouting | |
| CN221084893U (en) | Quick detach formula rotary filter screen | |
| CN219013016U (en) | Compression-resistant protective metal mesh enclosure | |
| CN217682043U (en) | Convenient-to-replace diesel filter for filter element | |
| CN220395853U (en) | Engine convenient to maintenance | |
| CN217271005U (en) | Noise reduction type fan convenient for replacing fan blades | |
| CN221074770U (en) | Axial flow fan with noise reduction function | |
| CN220248231U (en) | Dismounting mechanism for automobile filter | |
| CN218972835U (en) | Fresh air purifying unit | |
| CN220176395U (en) | Automatic filter screen replacing device and high-large space air conditioner | |
| CN221096791U (en) | Filter system of air compressor | |
| CN214035858U (en) | Automobile heat dissipation module | |
| CN218901188U (en) | Novel atmospheric purification environmental protection tower | |
| CN219735517U (en) | Ventilating device | |
| CN220078984U (en) | Natural gas pipeline filter convenient to maintain | |
| CN221333275U (en) | Waste gas recycling mechanism for calcium hypochlorite production | |
| CN220453879U (en) | Portable air purifier | |
| CN216278568U (en) | Energy-concerving and environment-protective type centrifugal fan convenient to clearance | |
| CN221277868U (en) | Inlet air filter device of mute unit of diesel generator | |
| CN220228848U (en) | Built-in automobile headlight that radiating effect is good | |
| CN218207252U (en) | Centrifugal fan convenient to clearance |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |