CN210353626U - Self-cooling hair drier aircraft nose - Google Patents
Self-cooling hair drier aircraft nose Download PDFInfo
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- CN210353626U CN210353626U CN201920891269.1U CN201920891269U CN210353626U CN 210353626 U CN210353626 U CN 210353626U CN 201920891269 U CN201920891269 U CN 201920891269U CN 210353626 U CN210353626 U CN 210353626U
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Abstract
The utility model discloses a self-cooling hair drier head, which comprises a shell, wherein a main runner is arranged on the shell, a side runner is arranged outside the main runner, the side runner is communicated with the outside, and the main runner and the side runner are mutually separated; the main flow passage comprises an air inlet and a first air outlet, and the first air inlet is used for air generated by the fan to enter; the side flow channel comprises an air inlet and a second air outlet; the first air outlet and the second air outlet are located on the same side. Like this at first air outlet air-out in-process, can produce the negative pressure in second air outlet position, will make like this and have the air flow in the side runner, and side runner one end switches on with the external world, and the external world then belongs to cold wind, and the second air outlet can have the wind to flow this moment, and through the outflow of cold wind, can play the cooling effect to the inside of whole aircraft nose, has just so played the effect of aircraft nose cooling.
Description
Technical Field
The utility model relates to a hair-dryer field, more specifically the utility model relates to a self-cooling type hair-dryer aircraft nose that says so.
Background
The hair dryer is mainly used for drying and shaping hair, but also can be used for local drying, heating and physical therapy in laboratories, physical therapy rooms, industrial production, art designing and the like.
The head of the hair dryer also generates heat during the hot air blowing from the hair dryer, and most of the heating wires of the hair dryer are arranged on the head of the traditional hair dryer, while the head of the prior art has almost no heat dissipation capability.
SUMMERY OF THE UTILITY MODEL
To the not enough of prior art existence, the utility model aims to provide a self-cooling type hair-dryer aircraft nose.
In order to achieve the above purpose, the utility model provides a following technical scheme:
a self-cooling type hair drier head, which comprises a hair drier body,
the heat exchanger comprises a shell, wherein a main flow channel is arranged on the shell, a side flow channel is arranged outside the main flow channel, the side flow channel is communicated with the outside, and the main flow channel and the side flow channel are mutually blocked;
the main flow passage comprises an air inlet and a first air outlet, and the first air inlet is used for air generated by the fan to enter;
the side flow channel comprises an air inlet and a second air outlet;
the first air outlet and the second air outlet are located on the same side.
As a further improvement of the utility model,
the first air outlet is annular.
The second air outlet is annular.
As a further improvement of the utility model,
an inner shell is arranged in the outer shell, and the main flow passage is arranged in the inner shell;
a gap between the outer shell and the inner shell forms a side flow passage;
the air inlet is positioned on the shell.
As a further improvement of the utility model,
the air conditioner is characterized in that a baffle is arranged on the inner shell, a first gap is formed between the baffle and the inner shell, and the first gap forms a first air outlet.
As a further improvement of the utility model,
the fan baffle is connected with the inner shell through a first connecting rib.
As a further improvement of the utility model,
the shell is provided with a boss in a round table shape, the boss is provided with a via hole, and a second air outlet is formed between the inner wall of the via hole and the outer wall of the inner shell.
As a further improvement of the utility model,
the outer wall of the inner shell is connected with the inner wall of the through hole through the second connecting rib.
Through above-mentioned technical scheme, through the setting of second splice bar, provide the connection structure of inner shell and shell to play the effect of fixed inner shell and shell.
As a further improvement of the utility model,
the air inlet position is provided with a sealing plate, and the sealing plate is provided with an air inlet.
As a further improvement of the utility model,
the beneficial effects of the utility model, the relative income wind gap position of shell is provided with the draw-in groove, be provided with the buckle of detaining the draw-in groove on the shrouding.
The wind that hair-dryer fan produced enters into the sprue by the air intake, and blow out from the wind in the first air outlet, the wind that the fan produced, it is hot-blast under heating state, because first air outlet and second air outlet lie in same one side, at first air outlet air-out in-process like this, can produce the negative pressure in second air outlet position, will make like this that to have the air flow in the side runner, and side runner one end switches on with the external world, the external world then belongs to cold wind, the second air outlet can have the windy outflow this moment, and through the outflow of cold wind, can play the cooling action to the inside of whole aircraft nose, just so the effect of aircraft nose cooling has been played.
Drawings
Fig. 1 is a schematic overall structure diagram of an embodiment of the present invention;
fig. 2 is an exploded view of the overall structure of the embodiment of the present invention;
fig. 3 is a schematic diagram of an internal structure of an embodiment of the present invention.
Reference numerals:
1. a housing; 2. a main flow channel; 3. a side runner; 4. an air inlet; 5. a first air outlet; 6. an air inlet; 7. a second air outlet; 8. an inner shell; 9. a baffle plate; 10. a first slit; 11. a first connecting rib; 12. a protrusion; 13. a via hole; 14. a second connecting rib; 15. closing the plate; 16. an air inlet; 17. a card slot; 18. and (5) buckling.
Detailed Description
The present invention will be described in further detail with reference to embodiments shown in the drawings.
Referring to FIGS. 1 to 3, the present embodiment
A self-cooling type hair drier head, which comprises a hair drier body,
the heat exchanger comprises a shell 1, wherein a main flow channel 2 is arranged on the body of the shell 1, a side flow channel 3 is arranged outside the main flow channel 2, the side flow channel 3 is communicated with the outside, and the main flow channel 2 and the side flow channel 3 are mutually blocked;
the main flow passage 2 comprises an air inlet 4 and a first air outlet 5, and the air inlet 4 is used for air generated by a fan to enter;
the side runner 3 comprises an air inlet 6 and a second air outlet 7;
the first air outlet 5 and the second air outlet 7 are located on the same side.
Through the technical scheme, the wind that the hair-dryer fan produced enters into in the sprue 2 by air intake 4, and blow off from the wind in the first air outlet 5, the wind that the fan produced, it is hot-blast under the heating condition, because first air outlet 5 and second air outlet 7 lie in same one side, in 5 air-out in-process at first air outlet like this, can produce the negative pressure in 7 positions of second air outlet, will make like this have the air flow in the side runner 3, and 3 one end of side runner switches on with the external world, the external world then belongs to cold wind, second air outlet 7 can have the wind outflow this moment, and through the outflow of cold wind, can play the cooling effect to the inside of whole aircraft nose, just so played the effect of aircraft nose cooling.
As a specific embodiment of the improvement,
the first air outlet 5 is annular.
The second air outlet 7 is annular.
Through above-mentioned technical scheme, set up first air outlet 5 and second air outlet 7 annularly for the air-out is concentrated more, and the wind speed that blows off also can be bigger.
As a specific embodiment of the improvement,
an inner shell 8 is arranged in the outer shell 1, and the main flow passage 2 is arranged in the inner shell 8;
the gap between the outer shell 1 and the inner shell 8 forms a side runner 3;
the air inlet 6 is positioned on the shell 1.
Through the technical scheme, the blocking of the main flow channel 2 and the side flow channel 3 can be conveniently realized through the arrangement of the inner shell 8 and the outer shell 1.
As a specific embodiment of the improvement,
the inner shell 8 is provided with a baffle 9, a first gap 10 is formed between the baffle 9 and the inner shell 8, and the first gap 10 forms the first air outlet 5.
Through the technical scheme, the baffle 9 is arranged, so that the first gap 10 is formed between the baffle 9 and the inner shell 8, and the annular first air outlet 5 is formed.
As a specific embodiment of the improvement,
the blower baffle 9 is connected with the inside of the inner shell 8 through a first connecting rib 11.
Through the technical scheme, the baffle 9 and the inner shell 8 can be connected through the arrangement of the first connecting ribs 11.
As a specific embodiment of the improvement,
the outer shell 1 is provided with a boss 12 in a circular truncated cone shape, the boss 12 is provided with a via hole 13, and the inner wall of the via hole 13 and the outer wall of the inner shell 8 form a second air outlet 7.
Through the technical scheme, through the arrangement of the protrusion 12, the protrusion 12 is provided with the through hole 13, the inner wall of the through hole 13 and the outer wall of the inner shell 8 form the second air outlet 7, and the boss is in a circular truncated cone shape, so that the air flow can be concentrated together, and the blown air speed is higher.
As a specific embodiment of the improvement,
the outer wall of the inner casing 8 and the inner wall of the through hole 13 are connected by second connection ribs 14.
As a specific embodiment of the improvement,
a sealing plate 15 is arranged at the position of the air inlet 6, and an air inlet 16 is arranged on the sealing plate 15.
Through above-mentioned technical scheme, through the setting of shrouding 15, played the inside guard action to the aircraft nose for inside the foreign object can't enter into the aircraft nose, and 16 settings of inlet port have guaranteed that outside air current can enter into side runner 3.
As a specific embodiment of the improvement,
a clamping groove 17 is formed in the position, opposite to the air inlet 6, of the shell 1, and a buckle 18 buckled into the clamping groove 17 is arranged on the sealing plate 15.
Through above-mentioned technical scheme, realized the fixed action to shrouding 15 through draw-in groove 17 and buckle 18's cooperation, can go out through this second income wind gap 6 and carry out inside installation, directly install shrouding 15 to second income wind gap 6 department after the installation is accomplished for the installation is more simple and convenient.
It is above only the utility model discloses a preferred embodiment, the utility model discloses a scope of protection does not only confine above-mentioned embodiment, the all belongs to the utility model discloses a technical scheme under the thinking all belongs to the utility model discloses a scope of protection. It should be noted that, for those skilled in the art, various modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations should also be regarded as the protection scope of the present invention.
Claims (10)
1. A self-cooling hair dryer head, comprising:
the heat exchanger comprises a shell (1), wherein a main flow channel (2) is arranged on the body of the shell (1), a side flow channel (3) is arranged outside the main flow channel (2), the side flow channel (3) is communicated with the outside, and the main flow channel (2) and the side flow channel (3) are mutually blocked;
the main flow passage (2) comprises an air inlet (4) and a first air outlet (5), and the air inlet (4) is used for air generated by a fan to enter;
the side flow channel (3) comprises an air inlet (6) and a second air outlet (7);
the first air outlet (5) and the second air outlet (7) are located on the same side.
2. A self-cooling hair dryer head as claimed in claim 1, wherein:
the first air outlet (5) is annular.
3. A self-cooling hair dryer head as claimed in claim 1, wherein:
the second air outlet (7) is annular.
4. A self-cooling hair dryer head as claimed in claim 1, wherein:
an inner shell (8) is arranged in the outer shell (1), and the main flow channel (2) is arranged in the inner shell (8);
a gap between the outer shell (1) and the inner shell (8) forms a side runner (3);
the air inlet (6) is positioned on the shell (1).
5. A self-cooling hair dryer head according to claim 4, wherein:
be provided with baffle (9) on inner shell (8), form first gap (10) between baffle (9) and inner shell (8), first gap (10) constitute first air outlet (5).
6. A self-cooling hair dryer head according to claim 5, wherein:
the baffle (9) is connected with the inner part of the inner shell (8) through a first connecting rib (11).
7. A self-cooling hair dryer head according to claim 4, wherein:
the air conditioner is characterized in that a boss (12) in a round table shape is arranged on the outer shell (1), a through hole (13) is formed in the boss (12), and a second air outlet (7) is formed between the inner wall of the through hole (13) and the outer wall of the inner shell (8).
8. A self-cooling hair dryer head according to claim 7, wherein:
the outer wall of the inner shell (8) and the inner wall of the through hole (13) are connected through a second connecting rib (14).
9. A self-cooling hair dryer head as claimed in claim 1, wherein:
a sealing plate (15) is arranged at the position of the air inlet (6), and an air inlet hole (16) is formed in the sealing plate (15).
10. A self-cooling hair dryer head according to claim 9, wherein:
the shell (1) is provided with a clamping groove (17) relative to the air inlet (6), and the sealing plate (15) is provided with a buckle (18) buckled into the clamping groove (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920891269.1U CN210353626U (en) | 2019-06-13 | 2019-06-13 | Self-cooling hair drier aircraft nose |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920891269.1U CN210353626U (en) | 2019-06-13 | 2019-06-13 | Self-cooling hair drier aircraft nose |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210353626U true CN210353626U (en) | 2020-04-21 |
Family
ID=70264804
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920891269.1U Active CN210353626U (en) | 2019-06-13 | 2019-06-13 | Self-cooling hair drier aircraft nose |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210353626U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110089831A (en) * | 2019-06-13 | 2019-08-06 | 陈光喜 | A kind of self-cooling type hair dryer head |
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2019
- 2019-06-13 CN CN201920891269.1U patent/CN210353626U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110089831A (en) * | 2019-06-13 | 2019-08-06 | 陈光喜 | A kind of self-cooling type hair dryer head |
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