CN2825332Y - Tyres for prototype aircraft or vehicle - Google Patents
Tyres for prototype aircraft or vehicle Download PDFInfo
- Publication number
- CN2825332Y CN2825332Y CN 200520063293 CN200520063293U CN2825332Y CN 2825332 Y CN2825332 Y CN 2825332Y CN 200520063293 CN200520063293 CN 200520063293 CN 200520063293 U CN200520063293 U CN 200520063293U CN 2825332 Y CN2825332 Y CN 2825332Y
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- model
- tire
- tyre
- soft rubber
- strengthening core
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Abstract
The utility model relates to a tyre for a prototype aircraft or a vehicle. The utility model has the structure that a soft rubber tyre is used, the tyre is composed of the soft rubber tyre, and a left and a right wheel frames which are arranged on the inner annular hole of the soft rubber tyre, wherein the left and the right wheel frames form a wheel hub; the inner part of the soft rubber tyre is provided with a hard annular reinforcing core which is used for shaping the soft rubber tyre; the reinforcing core is adjacent to the inner annular hole of the soft rubber tyre and is concentric with the inner annular hole. The tyre has the advantages of good damping effect and easy replacement; because the inner part of the tyre is provided with the annular reinforcing core, and the shaping is good; when the tyre moves and is impacted heavily, such as the prototype aircraft lands heavily, the tyre is not easy to divorce from the wheel hub because of deformation.
Description
Technical field
The utility model relates to a kind of model of an airplane or for motor vehicle tire of model.
Background technology
The for motor vehicle tire of the existing model of an airplane or model generally is made of rubber tire and the left and right frame of taking turns that is installed on the interior annular distance of this rubber tire, and the wherein left and right frame of taking turns constitutes wheel hub.Described rubber tire has two kinds of soft rubber tire and hard rubber tires, and for the soft rubber tire, its advantage is a good damping effect, easily change during wear on tyres, but when being hit, when heavily landing as the model of an airplane, tire breaks away from wheel hub easily; For hard rubber tire, though tire be difficult for to break away from wheel hub, its damping effect is bad, and the wheel frame, hard rubber tire deforms or change relatively difficulty during wear on tyres, and hard rubber tire is heavier.
Summary of the invention
The purpose of this utility model is a kind of model of an airplane of design or for motor vehicle tire new construction, to avoid the existing model of an airplane or the existing drawback of for motor vehicle tire of model.
The design-calculated model of an airplane of the present utility model or for motor vehicle tire, adopt the soft rubber tire, constitute by soft rubber tire and the left and right frame of taking turns that is installed on the interior annular distance of this rubber tire, the wherein left and right frame of taking turns constitutes wheel hub, it is characterized in that having in the described soft rubber tire body the annular strengthening core of a hard, rubber tire is formalized, this strengthening core with near the interior annular distance of rubber tire and with this in annular distance concentric.
Soft rubber tire of the present utility model is one-body molded with annular strengthening core during fabrication.
Described annular strengthening core can have 1～3 loop projection on its outer ring surface, to strengthen the setting effect to rubber tire.
Described annular strengthening core can adopt metal or hard plastic matter.
For alleviating the weight of tire, described annular strengthening core can adopt hollow structure.
The for motor vehicle tire of the model of an airplane of the present utility model or model, adopt the soft rubber tire, have this tire good damping effect, when wear on tyres, changing of tire is relatively easy to advantage, and owing to have described annular strengthening core in the tire body, formalize, when tire motion is subjected to heavily impacting, when heavily landing as the model of an airplane, tire can be because of distortion break away from wheel hub, owing to can use hollow strengthening core, the rubber tire total weight can be made gentlyer well.
Description of drawings
Fig. 1 is the member assembling scheme drawing of the model of an airplane of the present utility model or for motor vehicle tire;
Fig. 2 is the front appearance figure of the model of an airplane of the present utility model or for motor vehicle tire;
Fig. 3 is the cutaway view of the model of an airplane of the present utility model or for motor vehicle tire;
Fig. 4 is the outside drawing of a kind of embodiment of annular strengthening core of the model of an airplane of the present utility model or for motor vehicle tire;
Fig. 5 is the cutaway view of the rubber wheel carcass among Fig. 3;
Fig. 6 is that the A-A of Fig. 5 is to cutaway view;
Fig. 7 is that the B-B of Fig. 5 is to cutaway view;
Fig. 8 is the cutaway view of the another kind of rubber wheel carcass of the utility model embodiment;
Fig. 9 is that the C-C of Fig. 8 is to cutaway view.
The specific embodiment
Embodiment one
Each member of the tire of present embodiment is made up of soft rubber tire body 1, revolver frame 2, right wheel frame 3 as shown in Figure 1, and the left and right frame of taking turns is respectively from pack into the interior annular distance of rubber wheel carcass 1 of the and arranged on left and right sides of soft rubber tire body 1, and is fixing with screw 5, the formation wheel hub; The tire of dressing up is whole as Fig. 2, shown in Figure 3; In the body of rubber wheel carcass 1, has an annular strengthening core 4, as Fig. 3, shown in Figure 5, this annular strengthening core 4 is a metal material, be positioned near the position of the annular distance of rubber tire and concentric with this annular distance, have 2 loop projections 41 on the outer ring surface of this annular strengthening core 4, this annular strengthening core 4 and rubber tire body by integral forming, the shape and structure of annular strengthening core 4 such as Fig. 4, Fig. 6, shown in Figure 7.
Embodiment two
Present embodiment is the version of the another kind of model of an airplane of the utility model or for motor vehicle tire.Fig. 8, Fig. 9 have shown the structure of the tire body of this tire.Have the annular strengthening core 4 of a duroplasts material in this soft rubber tire body 1, both are integrated.The described annular strengthening core 4 of present embodiment has cavity 6, is hollow structure, thereby the tire body of present embodiment not only formalizes better, and weight is lighter.Wheel hub structure of this tire and embodiment one are basic identical.
Claims (4)
1, a kind of model of an airplane or for motor vehicle tire, constitute by soft rubber tire (1) and the left and right frame (2,3) of taking turns that is installed on the interior annular distance of this rubber tire, the wherein left and right frame of taking turns constitutes wheel hub, it is characterized in that having in described soft rubber tire (1) body the annular strengthening core (4) of a hard, this strengthening core (4) with near the interior annular distance of rubber tire and with this in annular distance concentric.
2, the model of an airplane according to claim 1 or for motor vehicle tire is characterized in that having 1～3 loop projection (41) on the outer ring surface of described annular strengthening core (4).
3, the model of an airplane according to claim 1 or for motor vehicle tire is characterized in that described annular strengthening core (4) is hollow structure.
4,, it is characterized in that described annular strengthening core (4) is metal or hard plastic matter according to claim 1, the 2 or 3 described model of an airplanes or for motor vehicle tire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200520063293 CN2825332Y (en) | 2005-08-22 | 2005-08-22 | Tyres for prototype aircraft or vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200520063293 CN2825332Y (en) | 2005-08-22 | 2005-08-22 | Tyres for prototype aircraft or vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2825332Y true CN2825332Y (en) | 2006-10-11 |
Family
ID=37065518
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200520063293 Expired - Fee Related CN2825332Y (en) | 2005-08-22 | 2005-08-22 | Tyres for prototype aircraft or vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2825332Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101780753A (en) * | 2010-03-03 | 2010-07-21 | 厦门连科工业有限公司 | Disconnection preventing solid tyre |
| CN110481661A (en) * | 2019-09-24 | 2019-11-22 | 履地科技(天津)有限公司 | A kind of combined type bogie wheel of rubber belt track running gear |
| CN110654165A (en) * | 2019-10-29 | 2020-01-07 | 嘉兴智悦橡塑有限公司 | Antiskid rubber wheel and production process thereof |
-
2005
- 2005-08-22 CN CN 200520063293 patent/CN2825332Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101780753A (en) * | 2010-03-03 | 2010-07-21 | 厦门连科工业有限公司 | Disconnection preventing solid tyre |
| CN110481661A (en) * | 2019-09-24 | 2019-11-22 | 履地科技(天津)有限公司 | A kind of combined type bogie wheel of rubber belt track running gear |
| CN110654165A (en) * | 2019-10-29 | 2020-01-07 | 嘉兴智悦橡塑有限公司 | Antiskid rubber wheel and production process thereof |
| CN110654165B (en) * | 2019-10-29 | 2023-10-31 | 嘉兴智悦橡塑股份有限公司 | Anti-skid rubber wheel and production process thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |