Title:
REDUCED WEIGHT AIRCRAFT TIRE
Document Type and Number:
Japanese Patent JP2017047891
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide an aircraft tire capable of meeting high speed, high load capacity and reduced weight requirements.SOLUTION: A pneumatic tire has a carcass and a belt reinforcing structure. The belt reinforcing structure has: a zigzag belt reinforcing structure formed of a strip of multiple reinforcement cords, the strip of reinforcement cords being inclined 5° to 30° relative to the centerplane of the tire extending in alternation to turnaround points at each lateral edge, where the zigzag strip of cords is formed from two different cords made of different materials, and a low angle belt of the tire having a higher EPI than the zigzag belt.SELECTED DRAWING: Figure 3
Inventors:
JOAN ELIZABETH SHAW
FRANK ANTHONY KMIECIK
LEONARD JAMES REITER
FRANK ANTHONY KMIECIK
LEONARD JAMES REITER
Application Number:
JP2016166773A
Publication Date:
March 09, 2017
Filing Date:
August 29, 2016
Export Citation:
Assignee:
GOODYEAR TIRE & RUBBER
International Classes:
B60C9/20; B60C9/00; B60C9/13; B60C9/22; D02G3/48
Domestic Patent References:
| JP2012001206A | 2012-01-05 |
Foreign References:
| WO2006035940A1 | 2006-04-06 |
Attorney, Agent or Firm:
Akio Miyazaki
Masaaki Ogata
Masaaki Ogata
Previous Patent: A tire for airplanes by which the weight saving was carried out
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