CN201964582U - Gear coordination structure - Google Patents
Gear coordination structure Download PDFInfo
- Publication number
- CN201964582U CN201964582U CN2010206872260U CN201020687226U CN201964582U CN 201964582 U CN201964582 U CN 201964582U CN 2010206872260 U CN2010206872260 U CN 2010206872260U CN 201020687226 U CN201020687226 U CN 201020687226U CN 201964582 U CN201964582 U CN 201964582U
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- gear
- gear groove
- groove
- panel
- coordination structure
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Abstract
The utility model relates to the technical field of air conditioners, in particular to a gear coordination structure for a horizontal wind plate and a panel of a window type air conditioner. The gear coordination structure comprises a first gear groove, a second gear groove and locating columns, wherein the first gear groove and the second gear groove are respectively arranged at both ends of the horizontal wind plate; the locating columns are arranged on the panel and are matched with the positions of the first gear groove and the second gear groove; and the first gear groove and the second gear groove are semi-open type and are opposite in open notch directions. The assembled gear coordination structure has good hand feeling; the horizontal wind plate 1 and the panel 6 have moderate degree of tightness when being coordinated by the gear coordination structure so as to achieve the purpose that the horizontal wind plate has a very good gear function by manually rotating the horizontal wind plate and can supply air to different directions. The gear coordination structure has high coordination precision, good manufacturability and low cost and is safe and reliable.
Description
Technical field
The utility model relates to the air-conditioner technical field, specifically is the gear fit structure of horizontal aerofoil of a kind of window machine and panel.
Background technology
In order to satisfy the rotation that low cost requires the horizontal aerofoil of present window machine all is manually control, and want reality manually just to need a gear fit structure to the different directions air-supply reliably, owing to be to realize that horizontal aerofoil cooperates with the gear that has between panel, this gear structure is most important, if cooperate the tension can't the horizontal aerofoil of hand rotation, if cooperated pine just not have the gear effect, can not blow to different directions, therefore it is simple to be starved of an assembling, the reliable gear fit structure that uses, and the gear structure of using at present is the fit structure of gear groove and panel reference column, and two ends gear groove adopts mode in the same way, in promptly being to the gear groove or be export-oriented gear groove, as Fig. 1, Fig. 2 and shown in Figure 3, the gear groove 11 at horizontal aerofoil 1 two ends, be illustrated as interior among the figure to the gear groove, the shortcoming that this fit system exists is: 1. the excesssive gap that exists between gear groove and the panel reference column just causes no gear effect easily, 2. if laterally the rotating shaft 3 of aerofoil 1 and the fit clearance of panel greatly also can cause gear groove and panel reference column excesssive gap, thereby gear lost efficacy, and the rotating shaft 3 of horizontal aerofoil produces big gap with the wearing and tearing of panel cooperation place and also can produce above-mentioned bad the cooperation equally after 3. long-term the use.
The utility model content
The technical problems to be solved in the utility model is to overcome above-mentioned shortcoming and gear fit structure that horizontal aerofoil of a kind of reliable realization and panel are provided.This gear fit structure feel is good, and the gear effect is strong, and good manufacturability is safe and reliable, and is with low cost.
For solving the problems of the technologies described above, technical scheme of the present utility model is:
A kind of gear fit structure, the reference column that comprises the first gear groove and the second gear groove that are located at horizontal aerofoil two ends respectively, is located on the panel and is complementary with the first gear groove and the second gear groove position, the described first gear groove and the second gear groove all adopt semi-open type, and open breach direction is opposite.The first gear groove is opposite with the second gear groove direction, with reference column gear no-float, quality of fit height.
Further, the described first gear groove is an arc, and the center of circle of the reference column that the center of circle of the first gear groove is corresponding with it is concentric.The described second gear groove is an arc, and the center of circle of the reference column that the center of circle of the second gear groove is corresponding with it is concentric.The first gear groove and the second gear groove are controlled at concentric reference column respectively in the rotary motion trace, also can guarantee to play the gear effect no matter how the first gear groove of horizontal aerofoil and the second gear groove and reference column gap change.
The utility model with respect to the beneficial effect of prior art is:
This gear fit structure feel of the utility model is good, guarantees precision easily, and good manufacturability, and is safe and reliable, with low cost.
Description of drawings
Below in conjunction with drawings and Examples the utility model is described in further detail.
The structural representation of the horizontal aerofoil gear of Fig. 1 prior art groove structure;
Fig. 2 is the schematic diagram of K direction among Fig. 1;
Fig. 3 is the schematic diagram of F direction among Fig. 1;
The structural representation of the horizontal aerofoil gear of Fig. 4 the utility model groove structure;
Fig. 5 is the schematic diagram of K direction among Fig. 4;
Fig. 6 is the schematic diagram of F direction among Fig. 4;
Fig. 7 is the panel construction schematic diagram that the utility model was used;
Fig. 8 is the assembling schematic diagram of horizontal aerofoil of the present utility model and panel.
The specific embodiment
As Fig. 4, Fig. 5, Fig. 6 and shown in Figure 7,
The utility model gear fit structure, the reference column 5 that comprises the first gear groove 2 and the second gear groove 4 that are located at horizontal aerofoil 1 two ends respectively, is located on the panel 6 and is complementary with the first gear groove 2 and the second gear groove, 4 positions, the first gear groove 2 and the second gear groove 4 all adopt semi-open type, and open breach direction is opposite, as the figure first gear groove 2 is interior to the gear groove, the second gear groove 4 is export-oriented gear groove, can certainly design the first gear groove 2 and be export-oriented gear groove, the second gear groove 4 is interior to the gear groove.
The first gear groove 2 and the second gear groove 4 are arc, the center of circle of the reference column 5 that their center of circle is all corresponding with it is concentric, the first gear groove and the second gear groove are controlled at concentric reference column in the rotary motion trace respectively, also can guarantee to play the gear effect no matter how the first gear groove of horizontal aerofoil and the second gear groove and reference column gap change, the gear of two gear grooves was corresponding when laterally aerofoil 1 rotated can change, thereby realizes blowing to different directions.
Fig. 8 is the assembling schematic diagram of horizontal aerofoil of the present utility model and panel.The gear fit structure feel that assembles is good, and elasticity was moderate when laterally 6 of aerofoil 1 and panels cooperated by this gear fit structure, reached the horizontal aerofoil of hand rotation and can play the gear effect well, guaranteed to blow to different directions.
The utility model quality of fit height, and good manufacturability, safe and reliable, with low cost.
Claims (3)
1. gear fit structure, the reference column (5) that comprises the first gear groove (2) and the second gear groove (4) that are located at horizontal aerofoil (1) two ends respectively, is located at that panel (6) is gone up and is complementary with the first gear groove (2) and second gear groove (4) position, it is characterized in that: the described first gear groove (2) and the second gear groove (4) all adopt semi-open type, and open breach direction is opposite.
2. gear fit structure according to claim 1 is characterized in that: the described first gear groove (2) is an arc, and the center of circle of the reference column (5) that the center of circle of the first gear groove (2) is corresponding with it is concentric.
3. gear fit structure according to claim 1 is characterized in that: the described second gear groove (4) is an arc, and the center of circle of the reference column (5) that the center of circle of the second gear groove (4) is corresponding with it is concentric.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010206872260U CN201964582U (en) | 2010-12-29 | 2010-12-29 | Gear coordination structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010206872260U CN201964582U (en) | 2010-12-29 | 2010-12-29 | Gear coordination structure |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201964582U true CN201964582U (en) | 2011-09-07 |
Family
ID=44527123
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2010206872260U Expired - Fee Related CN201964582U (en) | 2010-12-29 | 2010-12-29 | Gear coordination structure |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN201964582U (en) |
-
2010
- 2010-12-29 CN CN2010206872260U patent/CN201964582U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110907 Termination date: 20151229 |
|
EXPY | Termination of patent right or utility model |