CN204182600U - Aerodynamic Inverse tabula rasa - Google Patents
Aerodynamic Inverse tabula rasa Download PDFInfo
- Publication number
- CN204182600U CN204182600U CN201420644995.0U CN201420644995U CN204182600U CN 204182600 U CN204182600 U CN 204182600U CN 201420644995 U CN201420644995 U CN 201420644995U CN 204182600 U CN204182600 U CN 204182600U
- Authority
- CN
- China
- Prior art keywords
- fixed screw
- air cylinder
- reflective plate
- cylinder
- plate bracket
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses a kind of Aerodynamic Inverse tabula rasa, comprise cylinder, air cylinder support and reflector, described air cylinder support bottom is by air cylinder support fixed screw permanent plant, cylinder is fixed by cylinder fixed screw in described air cylinder support top, described Telescopic-cylinder top connects reflective plate bracket, described reflective plate bracket is bending in " Z " type, and the other end fixes reflector by reflective plate bracket fixed screw.The utility model structure is simple, and overcome the shortcoming that motor gear device drives reflector shakiness, new Aerodynamic Inverse filter plate device stability is high.
Description
Technical field
The utility model belongs to pneumatic means technical field, is specifically related to a kind of novel pneumatic reflector.
Background technology
The reflector device of existing color selector inside, be that stability in use is poor, and cost is high, and now provide one to utilize pneumatic promotion, stability is high with motor gear driven reflector displacement and commutation, structure is simple, the novel pneumatic reflector device that cost is low.
Utility model content
The purpose of this utility model is the pneumatic transposition reflector providing a kind of stability high.
The purpose of this utility model can be achieved through the following technical solutions:
Aerodynamic Inverse tabula rasa, comprise cylinder, air cylinder support and reflector, described air cylinder support bottom is by air cylinder support fixed screw permanent plant, cylinder is fixed by cylinder fixed screw in described air cylinder support top, described Telescopic-cylinder top connects reflective plate bracket, described reflective plate bracket is bending in " Z " type, and the other end fixes reflector by reflective plate bracket fixed screw.
Described support fixed screw, reflective plate bracket fixed screw, cylinder fixed screw all have two, are arranged in juxtaposition.
The beneficial effects of the utility model: Aerodynamic Inverse tabula rasa stability is high, structure is simple, and cost is low, overcomes the reflector device of original color selector power inside machine gear driven reflector displacement and commutation, the shortcoming of stability in use difference.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation.
In figure: 1, cylinder, 2, air cylinder support, 3, reflective plate bracket, 4, reflector, 5, air cylinder support fixed screw, 6, reflective plate bracket fixed screw, 7 cylinder fixed screws.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
As shown in Figure 1, Aerodynamic Inverse tabula rasa, comprise cylinder 1, air cylinder support 2 and reflector 4, described air cylinder support 2 bottom is by air cylinder support fixed screw 5 permanent plant, cylinder 1 is fixed by cylinder fixed screw 7 in described air cylinder support 2 top, described cylinder 1 stretch top connect reflective plate bracket 3, the bending in " Z " type of described reflective plate bracket 3, the other end fixes reflector 4 by reflective plate bracket fixed screw 6, described support fixed screw 5, reflective plate bracket fixed screw 6, cylinder fixed screw 7 all have two, are arranged in juxtaposition.
Operation principle: as shown in Figure 1, Aerodynamic Inverse tabula rasa, air cylinder support 2 bottom is by two air cylinder support fixed screw 5 permanent plants, and cylinder 1 is fixed by two cylinder fixed screws 7 in air cylinder support 2 top, and cylinder 1 top of stretching connects reflective plate bracket 3, reflective plate bracket 3 is bending in " Z " type, the other end fixes reflector 4 by two reflective plate bracket fixed screws 6, and by the retractility of cylinder 1, reflective plate bracket 3 drives reflector 4 to move up and down, utilize pneumatic promotion, stability is high.
Above content is only to the utility model structure example and explanation; affiliated those skilled in the art make various amendment to described instantiation or supplement or adopt similar mode to substitute; only otherwise depart from the structure of utility model or surmount this scope as defined in the claims, the protection domain of utility model all should be belonged to.
Claims (2)
1. Aerodynamic Inverse tabula rasa, comprise cylinder (1), air cylinder support (2) and reflector (4), it is characterized in that, described air cylinder support (2) bottom is by air cylinder support fixed screw (5) permanent plant, described air cylinder support (2) top is by the fixing cylinder (1) of cylinder fixed screw (7), the flexible top of described cylinder (1) connects reflective plate bracket (3), described reflective plate bracket (3) is bending in " Z " type, and the other end is by the fixing reflector (4) of reflective plate bracket fixed screw (6).
2. Aerodynamic Inverse tabula rasa according to claim 1, it is characterized in that, described support fixed screw (5), reflective plate bracket fixed screw (6), cylinder fixed screw (7) all have two, are arranged in juxtaposition.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420644995.0U CN204182600U (en) | 2014-10-30 | 2014-10-30 | Aerodynamic Inverse tabula rasa |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420644995.0U CN204182600U (en) | 2014-10-30 | 2014-10-30 | Aerodynamic Inverse tabula rasa |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204182600U true CN204182600U (en) | 2015-03-04 |
Family
ID=52614631
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420644995.0U Expired - Fee Related CN204182600U (en) | 2014-10-30 | 2014-10-30 | Aerodynamic Inverse tabula rasa |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204182600U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104289453A (en) * | 2014-10-30 | 2015-01-21 | 安徽捷迅光电技术有限公司 | Pneumatic reflector |
-
2014
- 2014-10-30 CN CN201420644995.0U patent/CN204182600U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104289453A (en) * | 2014-10-30 | 2015-01-21 | 安徽捷迅光电技术有限公司 | Pneumatic reflector |
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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: 20150304 Termination date: 20181030 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |