CN205016749U - Electric shock coupled structure of clarifier aircraft nose and fuselage - Google Patents
Electric shock coupled structure of clarifier aircraft nose and fuselage Download PDFInfo
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- CN205016749U CN205016749U CN201520773039.7U CN201520773039U CN205016749U CN 205016749 U CN205016749 U CN 205016749U CN 201520773039 U CN201520773039 U CN 201520773039U CN 205016749 U CN205016749 U CN 205016749U
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- coupling
- fuselage
- head
- female end
- aircraft nose
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Abstract
The utility model provides an electric shock coupled structure of clarifier aircraft nose and fuselage, includes aircraft nose and fuselage, its characterized in that aircraft nose dismantlement formula is assembled on the fuselage, and the aircraft nose is connected in the mutual electricity of coupler each other through setting up with the fuselage, the coupler includes public end of coupling and the female end of coupling, in the time of the assembly of aircraft nose and fuselage, in the public terminal pair of coupling should be inserted and locate the female end of coupling, when the aircraft nose is dismantled with the fuselage, public end of coupling and the female end separation of coupling. The utility model discloses an aircraft nose and the assembly of fuselage dismantlement formula set up public end of coupling and the female end of coupling respectively on its fitting surface to it is connected to realize the aircraft nose and the electricity of fuselage through the intercoordination. During the assembly, public end of coupling and the female end automatic negotiation of coupling, during the dismantlement, public end of coupling and the female end autosegregation of coupling when effectively having guaranteed the circular telegram coupling, have made things convenient for fuselage and aircraft nose to realize the separation, have also solved the circular telegram problem of present split type clarifier aircraft nose electrical part part.
Description
Technical field
The utility model relates to a kind of air purifier, particularly the electric shock coupled structure of clarifier head and fuselage.
Background technology
The electric components such as blower fan are placed in fuselage interior by the product of the most tower clarifier in current air purifier field, it is inconvenient that the structure of the layout that electric device and filter interlock causes changing filter screen, troublesome poeration, for solving the problem, market engenders the structure that head and fuselage detachable assemble, the power supply of corresponding head connects, and is all generally that power supply connects the assembling separate operation with head, thus causes the installation of head to bother.Therefore, be necessary to make further improvements.
Summary of the invention
The purpose of this utility model aim to provide a kind of simple and reasonable, convenient to disassembly, be electrically connected stable clarifier head and the electric shock coupled structure of fuselage, to overcome weak point of the prior art.
A kind of clarifier head designed by this object and the electric shock coupled structure of fuselage, comprise head and fuselage, it is characterized in that described head detachable is assemblied on fuselage, and head and fuselage are electrically connected to each other by the coupler be arranged at each other; Described coupler comprises coupling male end and coupling female end, and while described head and fuselage assemble, coupling male end corresponding inserted is in coupling female end, and while described head and fuselage are dismantled, coupling male end is separated with coupling female end.Electrical connection between head and fuselage completes with both assemblings simultaneously, need not operate in addition, enormously simplify assembly manipulation, in addition, while effectively ensureing energising coupling, facilitates fuselage and realizes being separated with head.
Described head is equipped with machine head base, and coupling male end is fixed on machine head base by male end seat.It is fixing that male end seat makes coupling male end locate,
Described fuselage is provided with the sealed head for snap close head, described coupling female end is fixed in sealed head by female end seat, and sealed head correspondence coupling female end is provided with location division, and coupling male end is inserted in coupling female end through location division.After coupling male end plugs coupling female end, location division is effectively located coupling male end, guarantees that the stability connected damages coupling male end with preventing.
Described fuselage both sides arrange at least one pair of coupling female end and female end seat respectively by sealed head, and coupling male end correspondence coupling female end is arranged.Multiple coupler is set as required, can resistance be effectively reduced.
Described coupling male end and coupling female end are conductive material, and coupling male end is rhabodoid, coupling female end body in a tubular form; Described coupling male end electrical connection head, described coupling female end is electrically connected domestic power supply by plug, and by the cooperation of coupling male end with the female end that is coupled, head can be electrically connected domestic power supply.
The beneficial effects of the utility model are:
Head of the present utility model and fuselage detachable assemble, and its fitting surface are arranged respectively coupling male end and the female end that is coupled, and realize the electrical connection of head and fuselage by intercoupling.During assembling, coupling male end and the female end automatic coupling that is coupled, during dismounting, coupling male end is separated automatically with coupling female end, while effectively ensure that energising coupling, facilitate fuselage and realize being separated with head, also solve the energising problem of existing split type clarifier head electric device part.It has simple and reasonable, convenient to disassembly, be electrically connected stable feature.
Accompanying drawing explanation
Fig. 1 is the decomposition texture schematic diagram of the utility model one embodiment.
Fig. 2 is the profile of the utility model one embodiment.
Fig. 3 is the structure for amplifying schematic diagram at A place in Fig. 1.
Fig. 4 is the structure for amplifying schematic diagram at B place in Fig. 2.
Embodiment
Below in conjunction with drawings and Examples, the utility model is further described.
See Fig. 1 and Fig. 2, the electric shock coupled structure of this clarifier head and fuselage, comprise head 1 and fuselage 2, head 1 from top to bottom detachable is assemblied in above fuselage 2, and head 1 and fuselage 2 realize being electrically connected to each other by the coupler be arranged at each other, and this coupler comprises coupling male end 7 and coupling female end 8, while head 1 and fuselage 2 assemble, coupling male end 7 corresponding inserted is in coupling female end 8, and while head 1 and fuselage 2 are dismantled, coupling male end 7 is separated with coupling female end 8.Electrical connection between head 1 and fuselage 2 completes with both assemblings simultaneously, need not operate in addition, enormously simplify assembly manipulation, in addition, while effectively ensureing energising coupling, facilitates fuselage 2 and realizes being separated with head 1.
Further, see Fig. 4, be equipped with machine head base 3 bottom head 1, coupling male end 7 is fixed in head 1 base by male end seat 6.It is fixing that male end seat 6 makes coupling male end 7 locate, and male end seat 6 is conductive material, and coupling male end 7 realizes being electrically connected with head 1 by male end seat 6.
Further, see Fig. 2 and Fig. 3, fuselage 2 is provided with sealed 4 for snap close head 1, coupling female end 8 is fixed in sealed 4 by female end seat 9, sealed 4 corresponding coupling female end 8 is provided with location division 4.1, and coupling male end 7 is inserted in coupling female end 8 through location division 4.1.After coupling male end 7 plugs coupling female end 8, location division 4.1 is effectively located coupling male end 7, guarantees that the stability connected damages coupling male end 7 with preventing.
Further, fuselage both sides arrange one sealed 4 respectively, arrange two to coupling female end 8 and female end seat 9 in each sealed 4, and the every side of coupling male end 7 correspondence coupling female end 8 arranges two.
Further, coupling male end 7 and coupling female end 8 are conductive material, and wherein, coupling male end 7 is in rhabodoid, and its upper end connects male end seat 6, and lower end is unsettled, coupling female end 8 body in a tubular form; Coupling male end 7 is electrically connected head 1, and coupling female end 8 is electrically connected domestic power supply by plug, and by the cooperation of coupling male end 7 with the female end 8 that is coupled, head 1 can be electrically connected domestic power supply.
Above-mentioned is preferred version of the present utility model, shows and describes general principle of the present utility model, principal character and advantage of the present utility model.Those skilled in the art should understand the utility model and not be restricted to the described embodiments; what describe in above-described embodiment and specification just illustrates principle of the present utility model; under the prerequisite not departing from the utility model spirit and scope, the utility model also has various changes and modifications, and these changes and improvements all fall within the scope of claimed the utility model.The claimed scope of the utility model is defined by appending claims and equivalent thereof.
Claims (5)
1. the electric shock coupled structure of a clarifier head and fuselage, comprise head (1) and fuselage (2), it is characterized in that described head (1) detachable is assemblied on fuselage (2), head (1) and fuselage (2) are electrically connected to each other by the coupler be arranged at each other; Described coupler comprises coupling male end (7) and coupling female end (8), while described head (1) and fuselage (2) assemble, coupling male end (7) corresponding inserted is in coupling female end (8), while described head (1) and fuselage (2) are dismantled, coupling male end (7) is separated with coupling female end (8).
2. the electric shock coupled structure of clarifier head and fuselage according to claim 1, is characterized in that described head (1) is equipped with machine head base (3), and coupling male end (7) is fixed on machine head base (3) by male end seat (6).
3. the electric shock coupled structure of clarifier head and fuselage according to claim 1, it is characterized in that described fuselage (2) being provided with the sealed head (4) for snap close head (1), described coupling female end (8) is fixed in sealed head (4) by female end seat (9), sealed head (4) correspondence coupling female end (8) is provided with location division (4.1), and coupling male end (7) is inserted in coupling female end (8) through location division (4.1).
4. the electric shock coupled structure of clarifier head and fuselage according to claim 3, it is characterized in that described fuselage (2) both sides arrange at least one pair of coupling female end (8) and female end seat (9) respectively by sealed head (4), coupling male end (7) correspondence coupling female end (8) is arranged.
5. the electric shock coupled structure of clarifier head and fuselage according to any one of claim 1-4, is characterized in that described coupling male end (7) and coupling female end (8) are conductive material, coupling male end (7) in rhabodoid, coupling female end (8) body in a tubular form; Described coupling male end (7) electrical connection head (1), described coupling female end (8) is electrically connected domestic power supply by plug.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520773039.7U CN205016749U (en) | 2015-10-06 | 2015-10-06 | Electric shock coupled structure of clarifier aircraft nose and fuselage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520773039.7U CN205016749U (en) | 2015-10-06 | 2015-10-06 | Electric shock coupled structure of clarifier aircraft nose and fuselage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205016749U true CN205016749U (en) | 2016-02-03 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520773039.7U Active CN205016749U (en) | 2015-10-06 | 2015-10-06 | Electric shock coupled structure of clarifier aircraft nose and fuselage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205016749U (en) |
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2015
- 2015-10-06 CN CN201520773039.7U patent/CN205016749U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: Room 2616, 129 Liuhe Road, Xihu District, Hangzhou City, Zhejiang Province Patentee after: Hangzhou Shijing Technology Co., Ltd Address before: 100000, No. 14, building 3, building 11, 1708 Ying Road, Beijing, Chaoyang District, 4 Patentee before: BEIJING ERACLEAN TECHNOLOGY Co.,Ltd. |