CN206160329U - Cooling fan - Google Patents
Cooling fan Download PDFInfo
- Publication number
- CN206160329U CN206160329U CN201620819018.9U CN201620819018U CN206160329U CN 206160329 U CN206160329 U CN 206160329U CN 201620819018 U CN201620819018 U CN 201620819018U CN 206160329 U CN206160329 U CN 206160329U
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- CN
- China
- Prior art keywords
- water tank
- fuselage
- thermantidote
- pedestal
- water
- 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.)
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Abstract
The utility model discloses a cooling fan, include: the fuselage, to the extension about the fuselage is, a water pump, the water pump leads to pipe to be connected the lower extreme of fuselage, and water tank, the water tank can be dismantled the connection and be in the lower extreme of fuselage to set up uncovered have up, uncovered use for the water pump stretches into in the water tank. The technical scheme of the utility model can realize conveniently separating the water tank from the lower extreme of fuselage is whole.
Description
Technical field
The utility model is related to household appliance technical field, more particularly to a kind of thermantidote.
Background technology
At present, in thermantidote common on the market, water tank is generally assembled to fuselage using the mounting structure of half odd test.It is aobvious
So, the water tank of half odd test is difficult to integrally separate from the fuselage of thermantidote, after in user's long-time using thermantidote, it is difficult to
Water tank is cleaned comprehensively.
Utility model content
Main purpose of the present utility model is to propose a kind of thermantidote, it is intended to realized water tank easily from the lower end of fuselage
Entirety is separated.
For achieving the above object, the utility model proposes thermantidote include：
Fuselage, the fuselage extends in upward and downward；
Water pump, the water pump is connected to the lower end of the fuselage by water pipe；And
Water tank, the water tank is detachably connected on the lower end of the fuselage, and open with what is opened up upward, described open
With stretching in the water tank for the water pump.
Preferably, the thermantidote also includes the connecting seat being located between the fuselage and the water tank, the connecting seat
Upper end be detachably connected with the lower end of the fuselage, the lower end of the connecting seat is detachably connected with the upper end of the water tank.
Preferably, the connecting seat includes arranging in ring frame-shaped and axial direction pedestal along the vertical direction, the pedestal
Upper end connect the week edge of the fuselage lower end, the lower end of the pedestal connects the week edge of the water tank upper end.
Preferably, it is provided with the upper end of the pedestal vertically to the stud for extending and the fixed back-off for extending upward,
The stud is provided with internal thread hole, the inner edge of the fuselage lower end be provided with just the internal thread hole is arranged installation through-hole,
And the first button hole fastened with the fixed back-off.
Preferably, the thermantidote also includes locking wrench, and the lower end of the pedestal passes through institute with the upper end of the water tank
State locking wrench connection.
Preferably, at least provided with two, the opposite sides of the water tank is respectively provided with least described in one locks the locking wrench
Button spanner.
Preferably, docked by way of interlocking between along the week with the water tank upper end in the week of the pedestal lower end.
Preferably, horizontally extending dividing plate is provided with the pedestal, the dividing plate is provided with and is passed through for the water pipe
Pore.
Preferably, the periphery of the dividing plate lower surface is interval with multiple guiding projections, and the guiding projection protrudes from institute
State the lower end of pedestal.
Preferably, the cross section of the water tank is adapted with the cross section of the fuselage, and the water tank has multiple, Duo Gesuo
The height for stating water tank is differed, and the lower end of the fuselage is connected with the upper end of arbitrary water tank.
The technical solution of the utility model with water tank open upward by will be connected to fuselage lower end, and water tank and machine
It is detachably connected between body, thus, work as thermantidote after long-time use, when needing to clean water tank, can be square
Just water tank is carried out into entirety from fuselage lower end to separate, so as to comprehensively clean water tank.
Description of the drawings
In order to be illustrated more clearly that the utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, in the premise for not paying creative work
Under, other accompanying drawings can be obtained with the structure according to these accompanying drawings.
Fig. 1 is the structural representation of the embodiment of the utility model thermantidote one；
Fig. 2 is the explosive view of thermantidote in Fig. 1；
Fig. 3 is the structural representation of the connecting seat of thermantidote in Fig. 1；
Fig. 4 is the structural representation of the fuselage in Fig. 1 on cold wind.
Drawing reference numeral explanation：
The realization of the utility model purpose, functional characteristics and advantage will be described further referring to the drawings in conjunction with the embodiments.
Specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the present utility model, rather than all
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not making creative work premise
Lower obtained every other embodiment, belongs to the scope of the utility model protection.
If it is to be appreciated that relate in the utility model embodiment directionality indicate (such as upper and lower, left and right, it is front,
Afterwards ...), then directionality indicates to be only used for explaining relative between each part under a certain particular pose (as shown in drawings)
Position relationship, motion conditions etc., if the particular pose changes, directionality indicates also correspondingly to change therewith.
If in addition, relate to the description of " first ", " second " etc. in the utility model embodiment, should " first ", " the
Two " description etc. is only used for describing purpose, and it is not intended that indicating or implying its relative importance or implicit indicate indication
The quantity of the technical characteristic for showing.Thus, " first " is defined, the feature of " second " can express or implicitly include at least one
Individual this feature.In addition, the technical scheme between each embodiment can be combined with each other, but must be with ordinary skill
Personnel can be implemented as basis, when the combination appearance of technical scheme is conflicting or cannot realize it will be understood that this technical side
The combination of case is not present, also not within the protection domain that the utility model is required.
The utility model proposes a kind of thermantidote.
See figures.1.and.2, in the embodiment of the utility model one, the thermantidote includes：
Fuselage 1, the fuselage 1 extends in upward and downward；
Water pump (not shown), the water pump is connected to the lower end of fuselage 1 by water pipe；And
Water tank 2, the water tank 2 is detachably connected on the lower end of fuselage 1, and open with what is opened up upward, this it is open to
Supply-water pump is stretched in water tank 2.
In the present embodiment, the cross section of the water tank 2 preferably has the size and shape being adapted with the cross section of fuselage 1,
Thus, can avoid occurring fuselage 1 in the vertical direction protruding from water tank 2, or water tank 2 protrudes from the phenomenon of fuselage 1, so as to protect
Hold the integrally succinct outward appearance of thermantidote.In addition, water tank 2 may be configured with multiple, the height specification of the plurality of water tank 2 is differed, machine
The lower end of body 1 can be connected with the upper end of any one in multiple water tanks 2；Obviously, the volume of the water tank 2 of differing heights specification is not
Together, user can the water tank 2 of specifically chosen desired height specification according to actual needs configured.Right the design not limited to this, in
In other embodiment, also water tank 2 can be designed to Height Adjustable water tank 2, in order to user water is adjusted according to actual needs
The storing water amount of case 2.
The technical solution of the utility model with water tank 2 open upward by will be connected to the lower end of fuselage 1, and water tank 2
It is detachably connected between fuselage 1, thus, working as thermantidote after long-time use, needs to clean water tank 2
When, it is convenient to water tank 2 is carried out into entirety from the lower end of fuselage 1 and is separated, so as to comprehensively be cleaned to water tank 2.
Further, the thermantidote also includes the connecting seat 3 being located between fuselage 1 and water tank 2, the upper end of the connecting seat 3
It is detachably connected with the lower end of fuselage 1, lower end is then detachably connected with the upper end of water tank 2.In the present embodiment, the upper end of water tank 2
The lower end of fuselage 1 is attached to by connecting seat 3 indirectly, thus, can be by the removable mounting structure matched with water tank 2 of fuselage 1
Connecting seat 3, or even the directly fuselage of thermantidote of the multiplexing with half odd test water tank 2 are transferred to, especially, for injection mo(u)lding
Fuselage, can directly be multiplexed the injection mold of fuselage, reduce R＆D costs.Right the design not limited to this, in other embodiment,
The upper end of water tank 2 can be directly connected to the lower end of fuselage 1.
In the lump with reference to Fig. 3, in the present embodiment, connecting seat 3 preferably include to be arranged in ring frame-shaped and axial direction vertically
The pedestal 31 in direction, the week edge of upper end connection fuselage 1 lower end of the pedestal 31, lower end then connects the week edge of the upper end of water tank 2.Can be with
Understand, it is in ring frame-shaped that pedestal 31 is arranged, and can further keep the integrally succinct outward appearance of thermantidote, and can play hiding water tank 2
With the effect of the internal structure of fuselage 1.
Further, horizontally extending dividing plate 32 is preferably provided with pedestal 31, the dividing plate 32 is provided with feed pipe
The pore 321 for passing through.It should be noted that herein indication dividing plate 32 is horizontally extending, refer to dividing plate 32 approximately along level
Direction extends, i other words, dividing plate 32 also can slightly favour horizontal plane setting.In the present embodiment, by setting up dividing plate 32, on the one hand
After water tank 2 is disassembled, it is to avoid the internal structure of fuselage 1 can be seen from the lower end of pedestal 31；On the other hand, thermantidote is being moved
During, can the water that splashes from water tank 2 of barrier, prevent the water in water tank 2 from splashing in the internal structure of fuselage 1.
With reference to Fig. 2 to Fig. 4, in the present embodiment, specifically, it is provided with the upper end of pedestal 31 vertically to the stud for extending
(not shown) and the fixed back-off 311 for extending upward, and the stud is provided with internal thread hole.The inner edge of the lower end of fuselage 1 is then
It is provided with the installation through-hole 101 that positive internal threads hole is arranged and the first button hole 102 fastened for the fixed adaptation of back-off 311.It is aobvious
So, it is to be realized detachably admittedly by screw lock adhering arrangement and buckle connecting structure between the lower end of the upper end of pedestal 31 and fuselage 1
Fixed, thus, compared to the scheme being only fixed using screw lock adhering arrangement, the efficiency of assembling of the technical program is higher, into
This is lower；And compared to the scheme being only fixed using buckle connecting structure, the assembling intensity of the technical program is higher, more
It is firm.
See figures.1.and.2, further, the thermantidote also includes locking wrench 4, and the lower end of pedestal 31 is upper with water tank 2
End is attached by the locking wrench 4.In the present embodiment, specifically, locking wrench 4 is articulated in the upper end of water tank 2, pedestal 31
Lower end is then provided with the second button hole 312 fastened for the lock adaptation of locking wrench 4, so, it is only necessary to by the lock of locking wrench 4
Depart from the second button hole 312, you can water tank 2 is pulled down from pedestal 31, is actually facilitated.Certainly, the design not limited to this, in other
In embodiment, also locking wrench 4 can be articulated in the lower end of pedestal 31, and arrange suitable for the lock of locking wrench 4 in the upper end of water tank 2
With the second button hole 312 for fastening.
It is to improve the Assembly stability between water tank 2 and connecting seat 3 in the present embodiment, locking wrench 4 is at least provided with two
It is individual, and the opposite sides of water tank 2 and pedestal 31 is respectively provided with an at least locking wrench 4.So the design not limited to this, implement in other
In example, especially, in the 31 accordingly rounded setting of water tank 2 and pedestal, locking wrench 4 is preferably provided with three, and this three
The uniform intervals of individual locking wrench 4 are laid in the upper end of cylindrical tank 2.
In addition, to make that closed connection can be obtained between the lower end of pedestal 31 and the upper end of water tank 2, week of the lower end of pedestal 31 along with
The week of the upper end of water tank 2 is preferably docked between by way of interlocking.With reference to Fig. 2, in the present embodiment, specifically, the upper end of water tank 2
End face be formed with first step 201, the end face of the lower end of pedestal 31 is then formed with the second step being adapted with first step 201
(not shown), ensures that pedestal 31 can be completely closed by the upper end of water tank 2 by first step 201 with the cooperation of second step.When
So, in other embodiment of the present utility model, also projection piece can be convexly equipped with the end face of the upper end of water tank 2, the lower end of pedestal 31
End face is then arranged with the groove being adapted with projection piece, ensures that pedestal 31 can be by water tank 2 by the cooperation of projection piece and groove
Upper end is completely closed.
In the lump with reference to Fig. 3, in the present embodiment, the periphery of the lower surface of dividing plate 32 is preferably by being provided with multiple guiding projections
33, certainly, the guiding projection 33 is the lower end for protruding from pedestal 31.It is appreciated that the setting of guiding projection 33 can be in connection
When water tank 2 and connecting seat 3, reduce the magnitude of misalignment between the upper end of water tank 2 and the lower end of pedestal 31, so as to conveniently realize on water tank 2
End and docking between the lower end of pedestal 31；In addition, after water tank 2 of dismantling, guiding projection 33 may also function as supporting the work of fuselage 1
With so as to prevent fuselage 1 from scratching.Without loss of generality, the substantially square ring frame-shaped of pedestal 31 is arranged, and dividing plate 32 is accordingly in side
Tabular setting, water tank 2 and its open also accordingly substantially square setting, at least provided with four, this four are led guiding projection 33
Set up four corners in dividing plate 32 separately to projection 33, thus, can conveniently realize between the upper end of water tank 2 and the lower end of pedestal 31
Positioning docking.
Preferred embodiment of the present utility model is the foregoing is only, the scope of the claims of the present utility model is not thereby limited,
It is every under inventive concept of the present utility model, the equivalent structure made using the utility model specification and accompanying drawing content is become
Change, or directly/be used in other related technical fields indirectly and be included in scope of patent protection of the present utility model.
Claims (10)
1. a kind of thermantidote, it is characterised in that include：
Fuselage, the fuselage extends in upward and downward；
Water pump, the water pump is connected to the lower end of the fuselage by water pipe；And
Water tank, the upper end of the water tank is detachably connected on the lower end of the fuselage, and the water tank has what is opened up upward to open
Mouthful, it is described open with stretching in the water tank for the water pump.
2. thermantidote as claimed in claim 1, it is characterised in that the thermantidote also includes being located at the fuselage with the water
Connecting seat between case, the upper end of the connecting seat is detachably connected with the lower end of the fuselage, the lower end of the connecting seat with
The upper end of the water tank is detachably connected.
3. thermantidote as claimed in claim 2, it is characterised in that the connecting seat includes arranging in ring frame-shaped and axial direction
Pedestal along the vertical direction, the upper end of the pedestal connects the week edge of the fuselage lower end, and the lower end connection of the pedestal is described
The week edge of water tank upper end.
4. thermantidote as claimed in claim 3, it is characterised in that be provided with the upper end of the pedestal vertically to the spiral shell for extending
Post and the fixed back-off for extending upward, the stud is provided with internal thread hole, and the inner edge of the fuselage lower end is provided with just to institute
The installation through-hole for stating internal thread hole setting and the first button hole fastened with the fixed back-off.
5. thermantidote as claimed in claim 3, it is characterised in that the thermantidote also includes locking wrench, the pedestal
Lower end is connected with the upper end of the water tank by the locking wrench.
6. thermantidote as claimed in claim 5, it is characterised in that the locking wrench at least provided with two, the water tank
Opposite sides is respectively provided with locking wrench at least described in.
7. thermantidote as claimed in claim 5, it is characterised in that the week of the pedestal lower end is along the week with the water tank upper end
Docked by way of interlocking between.
8. the thermantidote as described in any one of claim 3 to 7, it is characterised in that be provided with the pedestal and prolong in the horizontal direction
The dividing plate stretched, the dividing plate is provided with the pore passed through for the water pipe.
9. thermantidote as claimed in claim 8, it is characterised in that the periphery of the dividing plate lower surface is interval with multiple guiding
Projection, the guiding projection protrudes from the lower end of the pedestal.
10. thermantidote as claimed in claim 1, it is characterised in that the cross section of the cross section of the water tank and the fuselage
It is adapted, the water tank has multiple, the height of multiple water tanks is differed, the lower end of the fuselage and arbitrary water tank
Upper end connects.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620819018.9U CN206160329U (en) | 2016-07-29 | 2016-07-29 | Cooling fan |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620819018.9U CN206160329U (en) | 2016-07-29 | 2016-07-29 | Cooling fan |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206160329U true CN206160329U (en) | 2017-05-10 |
Family
ID=58647557
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620819018.9U Active CN206160329U (en) | 2016-07-29 | 2016-07-29 | Cooling fan |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206160329U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108548257A (en) * | 2018-05-07 | 2018-09-18 | 广东美的环境电器制造有限公司 | Water tank transition sleeve, cistern assembly and the cooling fan of cooling fan |
| WO2019214202A1 (en) * | 2018-05-07 | 2019-11-14 | 广东美的环境电器制造有限公司 | Water tank transitioning sleeve of cooling fan, water tank component, and cooling fan |
-
2016
- 2016-07-29 CN CN201620819018.9U patent/CN206160329U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108548257A (en) * | 2018-05-07 | 2018-09-18 | 广东美的环境电器制造有限公司 | Water tank transition sleeve, cistern assembly and the cooling fan of cooling fan |
| WO2019214202A1 (en) * | 2018-05-07 | 2019-11-14 | 广东美的环境电器制造有限公司 | Water tank transitioning sleeve of cooling fan, water tank component, and cooling fan |
| CN108548257B (en) * | 2018-05-07 | 2024-02-13 | 广东美的环境电器制造有限公司 | Water tank transition sleeve of cooling fan, water tank assembly and cooling fan |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |