CN201082662Y - Plateau type aviation tyre - Google Patents
Plateau type aviation tyre Download PDFInfo
- Publication number
- CN201082662Y CN201082662Y CNU2007200814861U CN200720081486U CN201082662Y CN 201082662 Y CN201082662 Y CN 201082662Y CN U2007200814861 U CNU2007200814861 U CN U2007200814861U CN 200720081486 U CN200720081486 U CN 200720081486U CN 201082662 Y CN201082662 Y CN 201082662Y
- Authority
- CN
- China
- Prior art keywords
- tire
- tyre
- plateau type
- tyre surface
- type aircraft
- 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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- Tires In General (AREA)
- Tyre Moulding (AREA)
Abstract
The utility model provides a plateau type aircraft tire. The utility model is mainly characterized in that two wide angle belted full reinforced cord fabric layers are arranged outside an upper tire tread, the width is extended to the outside of a tire bead wire ring, 1 to 2 layers of wide angle reinforced cord fabric layers are arranged between the upper tire tread and the lower tire tread, and the width extended to the outside of a tire shoulder. The plateau type aircraft tire has the advantages that the tire structure has the behavior and characteristics of high load and high velocity, the aircraft tire can meet the using requirement of the aircraft in the air rarefied plateau area, and fill up the blank that no plateau type aircraft tire is produced in China.
Description
Technical field:
The utility model relates to aircraft tyre, specifically a kind of suiting at the plateau type aircraft tyre of highlands use.
Background technology:
China western part is vast in territory, mostly based on the plateau landform, the highest Qinghai-Tibet Platean, the world is arranged, and height above sea level the highest high-altitude aerodrome in the world's is arranged.Because the density of air of highlands is low, aircraft is high more about 25% than region of no relief in the speed of highlands landing, so the performance of aircraft tyre is had more exacting requirements.At present China's plateau type aircraft tyre supporting with it not also developed the plateau type aircraft tyre, and China civil aviaton and air force's aircraft in the safe landing of high-altitude aerodrome, are had very important meaning.
The utility model content:
The purpose of this utility model is that a kind of plateau type aircraft tyre that can satisfy aircraft at highlands landing operating needs will be provided.
The utility model comprises study on tire pattern, goes up the full reinforcement carcass plies of tread strip bundle, goes up tyre surface, tyre surface, reinforcement carcass plies, casingply, air-retaining liner, bead coil, triangle glue between tyre surface up and down down, unlike the prior art be: it is more thinner than the last tyre surface of existing aircraft tyre to go up tyre surface, thickness is 5-6mm, the band that is outside equipped with two-layer wide-angle at last tyre surface is restrainted full reinforcement carcass plies, its width is until the bead bundle place, be provided with 1-2 layer wide-angle reinforcement carcass plies between last tyre surface and following tyre surface, its width is to the tire shoulder place.
Advantage of the present utility model is: tire construction has high load capacity, and high-speed performance characteristics can satisfy the requirement that aircraft uses in the highlands of rarefied air, fills up the blank that China does not have the plateau type aircraft tyre.
Description of drawings:
Fig. 1 is the section structure scheme drawing of the utility model plateau type aircraft tyre.
The specific embodiment:
The utility model plateau type aircraft tyre by groove 1, go up the full reinforcement carcass plies 2 of tread strip bundle, go up tyre surface 3, down tyre surface 4, reinforcement carcass plies 5, casingply 6, air-retaining liner 7, bead coil 8, triangle glue 9 are formed between tyre surface up and down.The last tyre surface 3 of this tire is more thinner than the last tyre surface of general aircraft tyre, thickness is 5-6mm, the band that two-layer and tire radial centre lines is 60 °～65 ° is set last tyre surface 3 outside simultaneously restraints full reinforcement nylon carcass plies 2, its width is up to bead bundle 8 places; Following tyre surface 4 thick 1.5-2mm up and down are being provided with the 1-2 layer between the tyre surface and the tire radial centre lines is 60 °～65 ° reinforcement nylon carcass pliess 5, and its width is to the tire shoulder place, and triangle glue 9 is arranged in the cord of bead part.
Claims (3)
1. plateau type aircraft tyre, comprise: groove (1), last tyre surface (3), following tyre surface (4), casingply (6), air-retaining liner (7), tyre bead (8), triangle glue (9), it is characterized in that: the band that is outside equipped with two-layer wide-angle at last tyre surface (3) is restrainted full reinforcement carcass plies (2), its width is located up to bead bundle (8), between last tyre surface (3) and following tyre surface (4) 1-2 layer wide-angle reinforcement carcass plies (5) is set, its width is to the tire shoulder place.
2. plateau type aircraft tyre as claimed in claim 1 is characterized in that: the cord of the band full reinforcement carcass plies of bundle (2) and the angle of tire radial centre lines are 60 °-65 °.
3. plateau type aircraft tyre as claimed in claim 1 is characterized in that: the cord of reinforcement carcass plies (5) and the angle of tire radial centre lines are 60 °-65 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200814861U CN201082662Y (en) | 2007-09-30 | 2007-09-30 | Plateau type aviation tyre |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200814861U CN201082662Y (en) | 2007-09-30 | 2007-09-30 | Plateau type aviation tyre |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201082662Y true CN201082662Y (en) | 2008-07-09 |
Family
ID=39625127
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007200814861U Expired - Fee Related CN201082662Y (en) | 2007-09-30 | 2007-09-30 | Plateau type aviation tyre |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201082662Y (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103998255A (en) * | 2011-12-20 | 2014-08-20 | 米其林集团总公司 | Crown for an aircraft tire |
| CN104309413A (en) * | 2014-11-04 | 2015-01-28 | 中国化工集团曙光橡胶工业研究设计院有限公司 | Bias belted aircraft tire |
| CN104844849A (en) * | 2015-05-04 | 2015-08-19 | 中国化工集团曙光橡胶工业研究设计院有限公司 | Aviation tire with tire bead reinforcing rubber and formula of reinforcing rubber |
| CN106926647A (en) * | 2017-03-13 | 2017-07-07 | 成都科力夫科技有限公司 | For the automobile tire of altitude environment |
| CN110053424A (en) * | 2019-05-14 | 2019-07-26 | 中国化工集团曙光橡胶工业研究设计院有限公司 | A kind of tread structure of high speed aircraft tyre |
| CN110877503A (en) * | 2019-12-30 | 2020-03-13 | 中国化工集团曙光橡胶工业研究设计院有限公司 | Carcass structure suitable for small-size and low-section aircraft tire |
-
2007
- 2007-09-30 CN CNU2007200814861U patent/CN201082662Y/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103998255A (en) * | 2011-12-20 | 2014-08-20 | 米其林集团总公司 | Crown for an aircraft tire |
| CN103998255B (en) * | 2011-12-20 | 2017-03-08 | 米其林集团总公司 | Crown for aircraft tire |
| CN104309413A (en) * | 2014-11-04 | 2015-01-28 | 中国化工集团曙光橡胶工业研究设计院有限公司 | Bias belted aircraft tire |
| CN104309413B (en) * | 2014-11-04 | 2016-11-30 | 中国化工集团曙光橡胶工业研究设计院有限公司 | A kind of belt diagonal aircraft tire |
| CN104844849A (en) * | 2015-05-04 | 2015-08-19 | 中国化工集团曙光橡胶工业研究设计院有限公司 | Aviation tire with tire bead reinforcing rubber and formula of reinforcing rubber |
| CN106926647A (en) * | 2017-03-13 | 2017-07-07 | 成都科力夫科技有限公司 | For the automobile tire of altitude environment |
| CN110053424A (en) * | 2019-05-14 | 2019-07-26 | 中国化工集团曙光橡胶工业研究设计院有限公司 | A kind of tread structure of high speed aircraft tyre |
| CN110877503A (en) * | 2019-12-30 | 2020-03-13 | 中国化工集团曙光橡胶工业研究设计院有限公司 | Carcass structure suitable for small-size and low-section aircraft tire |
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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: 20080709 Termination date: 20150930 |
|
| EXPY | Termination of patent right or utility model |