CN204555248U - Clarifier and shell structure thereof - Google Patents
Clarifier and shell structure thereof Download PDFInfo
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- CN204555248U CN204555248U CN201420872639.4U CN201420872639U CN204555248U CN 204555248 U CN204555248 U CN 204555248U CN 201420872639 U CN201420872639 U CN 201420872639U CN 204555248 U CN204555248 U CN 204555248U
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Abstract
The utility model belongs to purification technology field, aim to provide a kind of clarifier and shell structure thereof, this shell structure comprises fuselage main body, procapsid, ornamental strip and back casing, wherein, procapsid, ornamental strip and back casing are interlocked with fuselage main body respectively, and jointly enclose the shell structure of formation one contour curve slitless connection.The utility model, by offering at least one buckle slot in fuselage main body, the madial wall of procapsid at least arranges first snap component, wherein, one sidewall of each buckle slot is provided with the first back-off part, each first snap component comprised support reinforcing effect the first buckle base and be located at this first buckle base there is flexible buckle pin, the clamping part of each buckle pin is umbrella and is arranged on the first corresponding back-off part, like this, be convenient to very much the dismounting of clarifier and shell structure thereof, save the time of dismounting, also be not easy to during dismounting damage each parts, and do not affect the outward appearance of shell structure on the whole.
Description
Technical field
The utility model belongs to purification technology field, relates to a kind of shell structure, particularly relates to a kind of clarifier and shell structure thereof.
Background technology
Clarifier is also known as cleaner or cleaner, and the clarifier of indication refers in particular to air purifier usually here.Along with the development of industrial technology, air pollution is more and more serious, and for giving the air ambient of the indoor live and work Creating Comfort cleaning of people, air purifier obtains to be applied more and more widely.
In prior art, air purifier is primarily of parts compositions such as motor, fan, screen modules and control units, wherein, screen modules is mainly in order to air pollutants such as the dust in filtered air, PM2.5, peculiar smell, obviously, after using a period of time, these air pollutants can be adsorbed in screen modules, for guaranteeing the purification of air degree of air purifier, thus, the shell structure of regular dismounting air purifier must be needed, to remove and install the parts such as the screen modules in chamber within it, and regular cleaning is carried out to it.But the shell structure of existing air purifier adopts screw or the fixing detachable housing of screw or movable door structure mostly, like this, obviously not only inconvenient dismounting, expend time in long and dismounting time easily damage parts, thus, the demand of existing fast assembling-disassembling can not be met.
Utility model content
The purpose of this utility model is to provide a kind of clarifier and shell structure thereof, easily damages the technical problem of parts during the time that shell structure inconvenience dismounting, dismounting in order to solve existing clarifier expend long and dismounting.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is: the shell structure providing a kind of clarifier, this shell structure comprises fuselage main body and procapsid, described procapsid is connected by the first buckle structure buckle with described fuselage main body, described first buckle structure comprises at least one first snap component of at least one buckle slot being opened in described fuselage main body and the madial wall being located at described procapsid, and each described first snap component is arranged in corresponding described buckle slot.
Further, each described first snap component comprise the madial wall being located at described procapsid the first buckle base and be located at described first buckle base there is flexible buckle pin, the side cell wall of each described buckle slot is provided with the first back-off part, each described buckle pin is contained in corresponding described buckle slot, and back-off is on the described first back-off part of correspondence.
Further, each described first buckle base comprises the first reinforcement that at least two interradicular spaces are connected, and each described buckle pin is located on the sidewall of arbitrary described first reinforcement of the first corresponding buckle base.
Further, each described buckle pin comprises clamping part and is located at the connecting portion of sidewall of corresponding described first reinforcement, the afterbody of described clamping part is connected with described connecting portion, the head sizes of described clamping part is less than its tail dimension, and the afterbody of described clamping part is supported mutually with described first back-off part.
Further, described clamping part is umbrella or any one structure in being extended to the inner chamber of described procapsid by described connecting portion or being extended to chamber, the side wall of described procapsid by described connecting portion.
Further, this shell structure also comprises back casing, and described back casing is connected by the second buckle structure buckle with described fuselage main body; Described second buckle structure comprises at least one second snap component and at least one the 3rd snap component, each described second snap component to be located in described fuselage main body and to be comprised the second back-off part, the madial wall that each described 3rd snap component is located at described back casing comprises fastener, and each described second back-off part is snapped on corresponding described fastener.
Further, each described second snap component also comprises the second buckle base, each described second buckle base is formed by least two second reinforcement recessed bond ing, and each described second back-off part is located on the sidewall that connects between the second reinforcement described in corresponding adjacent two; Each described 3rd snap component also comprises the 3rd buckle base, and each described 3rd buckle base is formed by least two the 3rd reinforcement recessed bond ing, and each described fastener is located on the lateral wall of corresponding arbitrary described 3rd reinforcement.
Further, this shell structure also comprises ornamental strip, described ornamental strip is connected with described fuselage main body is detachable, one side of described ornamental strip is connected on described procapsid by the first position limiting structure, another side is connected on described back casing by the second position limiting structure, and described ornamental strip, described procapsid and described back casing enclose formation one enclosed cavity volume around described fuselage main body.
Further, described first position limiting structure comprises the first positive stop strip and at least one first limit assembly, described first positive stop strip is located at the side that described ornamental strip is connected with described procapsid, and each described first limit assembly is all located on the madial wall of described procapsid; Each described first limit assembly comprises at least one first locating part, and each described first locating part all offers the first stopper slot, and described first positive stop strip is arranged in each described first stopper slot simultaneously;
Described second position limiting structure comprises the second positive stop strip and at least one second limit assembly, and described second positive stop strip is located at the side that described ornamental strip is connected with described back casing, and each described second limit assembly is all located on the madial wall of described back casing; Each described second limit assembly comprises at least one second locating part, and each described second locating part all offers the second stopper slot, and described second positive stop strip is arranged in each described second stopper slot simultaneously.
Compared with prior art, the beneficial effect of the shell structure of clarifier that the utility model provides is:
(1) by offering at least one buckle slot in the fuselage main body of clarifier, the madial wall of its procapsid at least arranges first snap component, and each first snap component is fastened in corresponding buckle slot, with this, procapsid buckle is connected in fuselage main body, thus the dismounting be convenient between procapsid and fuselage main body, because be that buckle connects, the time thus needed for dismounting is shorter.
(2) because the first snap component comprises the first buckle base of the madial wall being located at procapsid, with be located at this first buckle base there is flexible buckle pin, wherein, this first buckle base mainly plays a part to strengthen intensity, this ensures that, the bonding strength of the shell structure of clarifier; In addition, because of buckle pin be have flexible, and this buckle pin the head sizes of clamping part be less than its tail dimension, thus, be easy to back-off on the first back-off part, like this, be not only easy to dismounting, the excellent of each parts can also be guaranteed.
(3) by being newly equipped with panel, and the first positive stop strip is set at a side of this ornamental strip, another side arranges the second positive stop strip, and allow the first positive stop strip be arranged in each first stopper slot of procapsid simultaneously, allow the second positive stop strip be arranged in each second stopper slot of back casing simultaneously, with this, on the basis ensureing connective stability good between procapsid, ornamental strip and back casing, also achieve the seamless link between three, and then make the shell structure of clarifier more attractive in appearance.
The utility model additionally provides a kind of clarifier, and this clarifier comprises above-mentioned shell structure.
Compared with prior art, the beneficial effect of the clarifier that the utility model provides is: be connected by the buckle used between flexible buckle pin with the first back-off part, facilitate the dismounting between procapsid and fuselage main body; Being connected with the buckle between fastener by using the second back-off part card, facilitating the dismounting between back casing and fuselage main body; By using ornamental strip, at a side of this ornamental strip, the first positive stop strip is set, another side arranges the second positive stop strip, and this first positive stop strip is arranged in each first stopper slot of procapsid simultaneously, this second positive stop strip is arranged in simultaneously in each second stopper slot of back casing, with this, on the basis ensureing connective stability good between procapsid, ornamental strip and back casing, also achieve the seamless link between three, and then make the monnolithic case of clarifier more attractive in appearance.
Accompanying drawing explanation
Fig. 1 is the perspective view of the shell structure of clarifier in the utility model embodiment;
Fig. 2 is the perspective view of the shell structure of the clarifier removing back casing and side ornamental strip in Fig. 1;
Fig. 3 is one of perspective view of the fuselage main body of clarifier in Fig. 1;
Fig. 4 is the perspective view of the procapsid of clarifier in Fig. 1;
Fig. 5 is the close-up schematic view at A place in Fig. 4;
Fig. 6 is the perspective view of the shell structure of the clarifier removing procapsid and side ornamental strip in Fig. 1;
Fig. 7 is the perspective view two of the fuselage main body of clarifier in Fig. 1;
Fig. 8 is the perspective view of the back casing of clarifier in Fig. 1;
Fig. 9 is the close-up schematic view at B place in Fig. 9;
Figure 10 is the perspective view of the ornamental strip of clarifier in Fig. 1;
Figure 11 is the perspective view of the agent structure of clarifier in Fig. 1.
Label in accompanying drawing is as follows:
1 fuselage main body, 11 buckle slots, 111 first back-off parts, 12 second snap component, 121 second back-off parts, 122 second buckle bases, 1,221 second reinforcements, 13 installing holes, 14 the 3rd back-off parts;
2 procapsids, 21 first snap component, 211 first buckle bases, 2,111 first reinforcements, 212 buckle pin, 2121 clamping parts, 2122 connecting portions, 22 first limit assemblies, 221 first locating parts, 2,211 first stopper slots;
3 back casings, 31 the 3rd snap component, 311 fasteners, 312 the 3rd buckle bases, 3121 the 3rd reinforcements, 32 second limit assemblies, 321 second locating parts, 3,211 second stopper slots, 33 installation components, 34 the 4th snap component, 341 plug-in card parts;
4 ornamental strips, 41 first positive stop strips, 42 second positive stop strips, 5 control panels.
Detailed description of the invention
In order to make technical problem to be solved of the present utility model, technical scheme and advantage clearly understand, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
Below in conjunction with concrete accompanying drawing, realization of the present utility model is described in detail.
It should be noted that, when parts are called as " being fixed on " or " being arranged at " another parts, it can directly on another parts or may there are parts placed in the middle simultaneously.When parts are known as " being connected to " another parts, it can be directly connected to another parts or may there are parts placed in the middle simultaneously.
Also it should be noted that, the corresponding same or analogous parts of same or analogous label in the accompanying drawing of the utility model embodiment, in description of the present utility model, it will be appreciated that, if have term " on ", D score, " left side ", orientation or the position relationship of the instruction such as " right side " are based on orientation shown in the drawings or position relationship, only the utility model and simplified characterization for convenience of description, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore, the term of position relationship is described only for exemplary illustration in accompanying drawing, the restriction to this patent can not be interpreted as, for the ordinary skill in the art, the concrete meaning of above-mentioned term can be understood as the case may be.
As shown in Fig. 1 ~ Figure 11, a kind of clarifier provided for the utility model one preferred embodiment and shell structure thereof.
As shown in Fig. 1 ~ Figure 10, the shell structure of clarifier comprises fuselage main body 1 and procapsid 2, for ease of the dismounting of this shell structure, shorten the time needed for dismounting, wherein, procapsid 2 is connected by the first buckle structure (not shown) buckle with fuselage main body 1, it should be noted that, this first buckle structure to be connected with procapsid 2 buckle by fuselage main body 1 and jointly to be formed, and is mainly applicable to the shell structure of clarifier, certainly, other shell structure is also applicable to.
In the present embodiment, as shown in Figures 2 to 5, first buckle structure comprises at least one buckle slot 11, with at least one the first snap component 21, wherein, each buckle slot 11 is all opened on the fuselage of fuselage main body 1, and each first snap component 21 is all located on the madial wall of procapsid 2, and each first snap component 21 is arranged in corresponding buckle slot 11.Certainly, each buckle slot 11 also can be opened on the madial wall of procapsid 2, and each first snap component 21 also can be arranged on the fuselage of fuselage main body 1, is not specifically described further here.
It should be noted that, for ease of forming shell structure attractive in appearance, after procapsid 2 and fuselage main body 1 are interlocked, procapsid 2 is that envelope fuselage main body 1 and fuselage main body 1 is interlocked, also namely, fuselage main body 1 is contained in the inner chamber of procapsid 2, and the two side ends of the two side ends of procapsid 2 and fuselage main body 1 has certain distance, obviously, each buckle slot 11 is opened on the fuselage of fuselage main body 1.
Further, as shown in Figure 2 and Figure 4, each first snap component 21 comprises the first buckle base 211 and is located at the buckle pin 212 of the first buckle base 211, wherein, first buckle base 211 is located at the madial wall of procapsid 2, is mainly used in supporting firm first snap component 21.In fact, this first buckle base 211 adopts featheredge to be connected with the connecting portion 2122 of the madial wall of procapsid 2, like this, can prevent the shrink of mould in production technology.Specifically as shown in Figure 4, buckle pin 212 departs from the madial wall of procapsid 2 and is arranged on the end of the first buckle base 211, for ease of the fastening between each buckle slot 11 or dismounting, and prevent from damaging each parts in fastening or unloading process, this buckle pin 212 is vertical shape relative to the first buckle base 211, and also has elasticity.
As shown in Figures 2 and 3, the side cell wall of each buckle slot 11 is provided with the first back-off part 111, and each buckle pin 212 is contained in corresponding buckle slot 11, and back-off is on the first back-off part 111 of correspondence.Specifically as shown in Figure 3, each first back-off part 111 is also provided with at least one reinforcement (not shown) in order to support firm first back-off part 111.Specifically as shown in Figure 2, obviously, first back-off part 111 is provided with back-off portion (not shown) and buckle pin 212 phase buckle, it should be noted that, this back-off portion is positioned at the top of buckle slot 11, goes out easily into the buckle pin 212 in this buckle slot 11 in order to prevent from holding from disengaging in this buckle slot 11.
Further, on the basis of support strength ensureing each first buckle base 211, for making the external hull surface of this shell structure neatly smooth, save material etc., as shown in Figure 4, each first buckle base 211 comprises the first reinforcement 2111 that at least two interradicular spaces are connected, to form the housing base of the larger hollow of thickness.Again as shown in Figure 4, each buckle pin 212 is located on the sidewall of arbitrary first reinforcement 2111 of the first corresponding buckle base 211, wherein, mainly be arranged on the outside of the sidewall of the first reinforcement 2111, certainly, the setting position of its concrete each buckle pin 212, can determine according to the position of the structure around each buckle slot 11 of fuselage main body 1 and each buckle slot 11.
Further, in the preferred embodiment that the utility model provides, as shown in Figure 2 and Figure 4, each buckle pin 212 comprises clamping part 2121 and is located at the connecting portion 2122 of sidewall of the first corresponding reinforcement 2111, the afterbody of clamping part 2121 is connected with connecting portion 2122, and the afterbody of clamping part 2121 is supported mutually with the first back-off part 111, understandably, connecting portion 2122 is main in order to be connected with the first reinforcement 2111, and clamping part 2121 is mainly used in being snapped in buckle slot 11.
Again as shown in Figure 4, for ease of buckle pin 212 is arranged in buckle slot 11, the head sizes of clamping part 2121 is less than its tail dimension, understandably, like this, being convenient to buckle pin 212 holds in buckle slot 11, when buckle pin 212 enters in buckle slot 11, buckle pin 212 can restore to the original state under the effect of its screen resilience, now, clamping part 2121 can be resisted against the first back-off part 111, completes snap action with this.
Further, in the preferred embodiment that the utility model provides, as shown in Fig. 2, Fig. 4 and Fig. 5, for ease of realizing the buckle function between buckle pin 212 and buckle slot 11, the clamping part 2121 of buckle pin 212 is in umbrella, or this clamping part 2121 is extended by the inner chamber of connecting portion 2122 to procapsid 2, or this clamping part 2121 is extended by chamber, the side wall of connecting portion 2122 to procapsid 2, in a word, this clamping part 2121 can be any one in these three kinds of structures.It should be noted that, here the direction of extending along the inner chamber of procapsid 2 of indication, the direction of extending with chamber, the side wall along procapsid 2 is relative, and the planform of concrete clamping part 2121 should be determined according to the position shape in the back-off portion of the first back-off part 111 on buckle slot 11.
Further, as shown in Fig. 1 and Fig. 6 to Fig. 9, this shell structure also comprises back casing 3, for ease of the dismounting of shell structure, shorten the time needed for dismounting, wherein, back casing 3 is connected by the second buckle structure (not shown) buckle with fuselage main body 1, it should be noted that, this second buckle structure to be connected with back casing 3 buckle by fuselage main body 1 and jointly to be formed, mainly be applicable to the shell structure of clarifier, certainly, be also applicable to other shell structure.
In the preferred embodiment that the utility model provides, as shown in Figures 6 to 9, second buckle structure comprises at least one second snap component 12 and at least one the 3rd snap component 31, wherein, each second snap component 12 is located in fuselage main body 1, and each second snap component 12 includes the second back-off part 121, each 3rd snap component 31 is located on the madial wall of back casing 3, and each 3rd snap component 31 includes fastener 311, when back casing 3 is snapped in fuselage main body 1, each second back-off part 121 is snapped on corresponding fastener 311.
It should be noted that, more firm for ease of the annexation between back casing 3 and fuselage main body 1, also need between back casing 3 and fuselage main body 1 to be fixedly connected with by installation component 33 is detachable, in the preferred embodiment specifically provided at the utility model, on back casing 3 and fuselage main body 1, offer the installing hole 13 that at least one is mutually corresponding respectively, and be mutually permanently connected with screw or the fixture such as screw or bolt.
In addition, in the preferred embodiment that the utility model provides, back casing 3 is also provided with the 4th snap component 34, fuselage main body 1 is provided with one the 3rd back-off part 14, wherein, the 4th snap component 34 is provided with a plug-in card part 341, while back casing 3 being snapped in fuselage main body 1 by the second buckle structure, this plug-in card part 341 is also oppositely plugged on the 3rd back-off part 14 of fuselage main body 1, strengthens the connection between back casing 3 and fuselage main body 1 further with this.
Further, in the preferred embodiment that the utility model provides, as shown in Figure 7, each second snap component 12 also comprises the second buckle base 122, wherein, and the support housing of the second buckle base 122 also in hollow, main in order to support firm second back-off part 121, and then guarantee the steadiness that the buckle between back casing 3 with fuselage main body 1 is connected, specifically in the present embodiment, each second buckle base 122 is formed by least two second reinforcement 1221 recessed bond ing.Again as shown in Figure 7, each second back-off part 121 is located on the sidewall of connection between corresponding adjacent two second reinforcements 1221.Specifically in the present embodiment, each second buckle base 122 has three second reinforcements 1221, to form the support frame of two hollows.
As shown in Figure 8 and Figure 9, each 3rd snap component 31 also comprises the 3rd buckle base 312, wherein, the support housing of 3rd buckle base 312 also in hollow, main in order to support fuselage main body 1 and to be firmly located at the fastener 311 on the 3rd buckle base 312, specifically in the present embodiment, each 3rd buckle base 312 is formed by least two the 3rd reinforcement 3121 recessed bond ing, and each fastener 311 is located on the lateral wall of the 3rd buckle base 312, particularly, each fastener 311 is located on the lateral wall of corresponding arbitrary 3rd reinforcement 3121.
Further, as shown in figs. 6 and 10, in the preferred embodiment that the utility model provides, more neatly smooth for making whole shell structure enclose the surface of the shell body of formation, and make the curve sense of shell body stronger, this shell structure also comprises ornamental strip 4, and for ease of dismounting, ornamental strip 4 is connected with fuselage main body 1 is detachable, moreover, for spacing further to this ornamental strip 4, one side of ornamental strip 4 is connected on procapsid 2 by the first position limiting structure, another side is connected on back casing 3 by the second position limiting structure, also be, ornamental strip 4 is connected between procapsid 2 and back casing 3, wherein, the curved surface profile of the profile of the madial wall of this ornamental strip 4 and the sidewall of fuselage main body 1 is suitable.Obviously, ornamental strip 4, procapsid 2 and back casing 3 enclose formation one enclosed cavity volume around fuselage main body 1, and also, ornamental strip 4, procapsid 2 and back casing 3 enclose the common Outer housing component forming this shell structure.
Further, as Fig. 2, Fig. 4, Fig. 5, shown in Figure 10, first position limiting structure comprises first positive stop strip 41 and at least one first limit assembly 22, it should be noted that, first position limiting structure is formed jointly by ornamental strip 4 and procapsid 2, wherein, first positive stop strip 41 is located at the side that ornamental strip 4 is connected with procapsid 2, each first limit assembly 22 is all located on the madial wall of procapsid 2, and it is stepped in one between the first positive stop strip 41 and the main casing of ornamental strip 4, understandably, when ornamental strip 4 is located on procapsid 2, the lateral wall of ornamental strip 4 just can form a smooth curved surface with the lateral wall of procapsid 2.
Concrete as Fig. 2, Fig. 4, shown in Fig. 5, each first limit assembly 22 comprises at least one first locating part 221, each first locating part 221 all offers the first stopper slot 2211, first positive stop strip 41 is arranged in each first stopper slot 2211 simultaneously, in the preferred embodiment specifically provided at the utility model, each first limit assembly 22 has two or three first locating parts 221 be parallel to each other, wherein, each first locating part 221 is rib, each first stopper slot 2211 is opened in the side that each rib is connected with the madial wall of procapsid 2, and each first stopper slot 2211 is formed jointly by the rib of each correspondence and the madial wall of procapsid 2, like this, so that ornamental strip 4 is connected the rear shell body formed curve form with procapsid 2 is more smooth.In addition, for preventing to interfere, each first buckle base 211 also offers this first stopper slot 2211.It should be noted that, each first stopper slot 2211 is all positioned on curve, and this curve and the first positive stop strip 41 suitable.
In like manner, as Fig. 6, shown in Fig. 8 to Figure 10, second position limiting structure comprises second positive stop strip 42 and at least one second limit assembly 32, it should be noted that, second position limiting structure is formed jointly by ornamental strip 4 and back casing 3, wherein, second positive stop strip 42 is located at the side that ornamental strip 4 is connected with back casing 3, each second limit assembly 32 is all located on the madial wall of back casing 3, and it is stepped in one between the second positive stop strip 42 and the main casing of ornamental strip 4, understandably, when ornamental strip 4 is located on back casing 3, the lateral wall of ornamental strip 4 just can form a smooth curved surface with the lateral wall of back casing 3.
Specifically as shown in Figure 6 and Figure 8, each second limit assembly 32 comprises at least one second locating part 321, and each second locating part 321 all offers the second stopper slot 3211, second positive stop strip 42 and is arranged in each second stopper slot 3211 simultaneously.In the preferred embodiment specifically provided at the utility model, each second limit assembly 32 has two or three second locating parts 321 be parallel to each other, wherein, each second locating part 321 is rib, each first stopper slot 2211 is opened in the side that each rib is connected with the madial wall of back casing 3, and each second stopper slot 3211 is formed jointly by the rib of each correspondence and the madial wall of back casing 3, like this, so that the curve form of shell body that formed after being connected with back casing 3 of ornamental strip 4 is more smooth.In addition, for preventing to interfere, each second buckle base 122 also offers this second stopper slot 3211.It should be noted that, each second stopper slot 3211 is all positioned on curve, and this curve and the second positive stop strip 42 suitable.
The utility model embodiment still provides a kind of clarifier, as shown in figure 11, this clarifier comprises above-mentioned shell structure, also comprise control panel 5, wherein, this shell structure and control panel 5 form the shell body of clarifier jointly, obviously, this clarifier is connected by the buckle between its procapsid 2 and side fuselage of fuselage main body 1, also be connected by the buckle between its back casing 3 and opposite side fuselage of fuselage main body 1, and the buckle between ornamental strip 4 and the two side of fuselage main body 1 is connected, make not only to be convenient to this clarifier of dismounting, save the time of dismounting, and in disassembly process not fragile parts, and the shell body curved surface of this clarifier also can be made more smooth, and then make monnolithic case more attractive in appearance.
The foregoing is only preferred embodiment of the present utility model, be not limited to the utility model.For a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within right of the present utility model.
Claims (10)
1. the shell structure of clarifier, comprise fuselage main body and procapsid, it is characterized in that: described procapsid is connected by the first buckle structure buckle with described fuselage main body, described first buckle structure comprises at least one first snap component of at least one buckle slot being opened in described fuselage main body and the madial wall being located at described procapsid, and each described first snap component is arranged in corresponding described buckle slot.
2. the shell structure of clarifier as claimed in claim 1, it is characterized in that: each described first snap component comprise the madial wall being located at described procapsid the first buckle base and be located at described first buckle base there is flexible buckle pin, the side cell wall of each described buckle slot is provided with the first back-off part, each described buckle pin is contained in corresponding described buckle slot, and back-off is on the described first back-off part of correspondence.
3. the shell structure of clarifier as claimed in claim 2, it is characterized in that: each described first buckle base comprises the first reinforcement that at least two interradicular spaces are connected, each described buckle pin is located on the sidewall of arbitrary described first reinforcement of the first corresponding buckle base.
4. the shell structure of clarifier as claimed in claim 3, it is characterized in that: each described buckle pin comprises clamping part and is located at the connecting portion of sidewall of corresponding described first reinforcement, the afterbody of described clamping part is connected with described connecting portion, the head sizes of described clamping part is less than its tail dimension, and the afterbody of described clamping part is supported mutually with described first back-off part.
5. the shell structure of clarifier as claimed in claim 4, is characterized in that: described clamping part is umbrella or any one structure in being extended to the inner chamber of described procapsid by described connecting portion or being extended to chamber, the side wall of described procapsid by described connecting portion.
6. the shell structure of clarifier as claimed in claim 1, it is characterized in that: this shell structure also comprises back casing, described back casing is connected by the second buckle structure buckle with described fuselage main body; Described second buckle structure comprises at least one second snap component and at least one the 3rd snap component, each described second snap component to be located in described fuselage main body and to be comprised the second back-off part, the madial wall that each described 3rd snap component is located at described back casing comprises fastener, and each described second back-off part is snapped on corresponding described fastener.
7. the shell structure of clarifier as claimed in claim 6, it is characterized in that: each described second snap component also comprises the second buckle base, each described second buckle base is formed by least two second reinforcement recessed bond ing, and each described second back-off part is located on the sidewall that connects between the second reinforcement described in corresponding adjacent two; Each described 3rd snap component also comprises the 3rd buckle base, and each described 3rd buckle base is formed by least two the 3rd reinforcement recessed bond ing, and each described fastener is located on the lateral wall of corresponding arbitrary described 3rd reinforcement.
8. the shell structure of clarifier as claimed in claims 6 or 7, it is characterized in that: this shell structure also comprises ornamental strip, described ornamental strip is connected with described fuselage main body is detachable, one side of described ornamental strip is connected on described procapsid by the first position limiting structure, another side is connected on described back casing by the second position limiting structure, and described ornamental strip, described procapsid and described back casing enclose formation one enclosed cavity volume around described fuselage main body.
9. the shell structure of clarifier as claimed in claim 8, it is characterized in that: described first position limiting structure comprises the first positive stop strip and at least one first limit assembly, described first positive stop strip is located at the side that described ornamental strip is connected with described procapsid, and each described first limit assembly is all located on the madial wall of described procapsid; Each described first limit assembly comprises at least one first locating part, and each described first locating part all offers the first stopper slot, and described first positive stop strip is arranged in each described first stopper slot simultaneously;
Described second position limiting structure comprises the second positive stop strip and at least one second limit assembly, and described second positive stop strip is located at the side that described ornamental strip is connected with described back casing, and each described second limit assembly is all located on the madial wall of described back casing; Each described second limit assembly comprises at least one second locating part, and each described second locating part all offers the second stopper slot, and described second positive stop strip is arranged in each described second stopper slot simultaneously.
10. clarifier, is characterized in that: comprise the shell structure as described in any one of claim 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420872639.4U CN204555248U (en) | 2014-12-31 | 2014-12-31 | Clarifier and shell structure thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420872639.4U CN204555248U (en) | 2014-12-31 | 2014-12-31 | Clarifier and shell structure thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204555248U true CN204555248U (en) | 2015-08-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201420872639.4U Active CN204555248U (en) | 2014-12-31 | 2014-12-31 | Clarifier and shell structure thereof |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106482312A (en) * | 2015-08-28 | 2017-03-08 | 青岛海尔空调器有限总公司 | Housing for radial pattern indoor apparatus of air conditioner and radial pattern indoor apparatus of air conditioner |
| CN106765642A (en) * | 2016-12-28 | 2017-05-31 | 广东美的环境电器制造有限公司 | Air purifier |
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2014
- 2014-12-31 CN CN201420872639.4U patent/CN204555248U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106482312A (en) * | 2015-08-28 | 2017-03-08 | 青岛海尔空调器有限总公司 | Housing for radial pattern indoor apparatus of air conditioner and radial pattern indoor apparatus of air conditioner |
| CN106482312B (en) * | 2015-08-28 | 2019-07-02 | 青岛海尔空调器有限总公司 | Shell and radial pattern air conditioner indoor unit for radial pattern air conditioner indoor unit |
| CN106765642A (en) * | 2016-12-28 | 2017-05-31 | 广东美的环境电器制造有限公司 | Air purifier |
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