Meridian aircraft tire capable of reducing interface shear stress and improving bead durability

A technology for aviation tires and shear stress, which is applied to tire parts, reinforcing layers of pneumatic tires, tire edges, etc., can solve problems that cannot meet the requirements of airworthiness standards, and achieve the effect of improving the durability of the bead

Active Publication Date: 2013-04-03
中国化工集团曙光橡胶工业研究设计院有限公司
View PDF11 Cites 9 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

These methods have a better effect on improving the fatigue resistance of aviation tire beads, but they stil

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Meridian aircraft tire capable of reducing interface shear stress and improving bead durability
  • Meridian aircraft tire capable of reducing interface shear stress and improving bead durability

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0011] exist figure 2 In the existing technologies shown in the embodiments, the meridial aerial tires are tire gum 1. Band layer 2, carcass curtain layer 3A, carcass curtain layer 3B, a pair of steel wire circles 4, one layer of stress buffer 5, etc.For the composition, the carcass curtain layer 3A from the tire crown passes through the tire side and wraps the steel wire ring 4 from the inner side to the outer side;Set up the beam layer 2 on the 3b; the tire glue 1 is set on the beam layer 2; the outer stress buffer 5 is set on the outer side of the carcass curtain layer 3B.Shaw's hardness of stress buffer 5 is 65 degrees, and the thickness is 6mm.

[0012] exist figure 1 In the embodiments of the present invention, the meridial aviation tires from tire glue 1. Bid layer 2, carcass curtain layer 3A, carcass curtain layer 3B, a pair of steel wire circles 4. One layer of transition glue 5A, two layers of bufferFiber curtain layer 5B, one layer of stress buffer 5, etc.Sendor curtain...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

PropertyMeasurementUnit
Thicknessaaaaaaaaaa
Angleaaaaaaaaaa
Shore hardnessaaaaaaaaaa
Login to view more

Abstract

The invention discloses a meridian aircraft tire capable of reducing interface shear stress and improving bead durability. The tire is characterized in that one layer of transition glue is arranged at a bead part and positioned on the outer side of a carcass ply, is 2-4 mm in thickness, and is 60-70 degrees in shore hardness; two layers of buffer fiber cord ply are arranged outside the transition glue; the density of cord threads is 35-90 piece/100 mm; the included angles between the cord threads and the peripheral direction are 20-90 degrees; and warps of the two layers of fly are across arranged corresponding to the radial direction. The improved meridian aircraft tire can reduce interface stress, strain and themogenesis between the carcass at the bead part and the rubbers at the outer side, and can improve the bead durability by more than 80% under the rigorous conditions; and the dynamic performance of the tire can meet the requirements of airworthiness standard (GJB683A).

Description

Technical field [0001] The present invention involves aviation tires, especially the sub -meridial aviation tires that can reduce interface shear stress and improve durability under the durability of tires. Background technique [0002] Under the strict dynamic conditions of the meridial aviation tires, due to the low stiffness of the tire side, the tire ring part is large, and it is easy to cause the fetal body curtain or tire ring to enhance the layer of the outer rubber.The fatigue and safety performance of the tire cannot meet the requirements of the airworthiness standard.At present, the method of reducing the strain, stress and heat of the fetal ring parts include: (1) adjust the height of the carcass reflux; (2) to set the tire ring enhancement layer; (3)Set high elasticity, low -growing hot rubber.These methods have a good improvement of fatigue resistance of aviation tire circles, but they still cannot meet the requirements of airworthiness standards under the requiremen...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): B60C9/04B60C15/06
Inventor 韦进明关伟平高香丽傅云翠
Owner 中国化工集团曙光橡胶工业研究设计院有限公司
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap