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Title:
PNEUMATIC RADIAL TIRE FOR AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2019/124470
Kind Code:
A1
Abstract:
A pneumatic radial tire for an aircraft. The pneumatic radial tire for an aircraft comprises: a pair of bead cores that comprise a cable bead; a radial carcass that comprises a plurality of plies that extend toroidally between the bead cores; and stiffeners that are adjacent to the bead cores on the tire-radial-direction outside of the bead cores. The radial carcass includes: at least one turn-up ply that has turned-up parts that turn up around the bead cores from the tire-axial-direction inside to the outside; and at least one down ply that covers the turned-up parts and extends at least to the radial-direction inside of the bead cores. In a tire-axial-direction cross-section of the tire when the tire has been installed on a rim, is below maximum internal pressure, and is not bearing a load, when points A are the intersections between virtual circles that are centered on the centers O of the bead cores and have a radius that is twice the diameter D of the bead cores and a ply that intersects the virtual circles and is closest to the tire-axial-direction insides of the stiffeners, points B are the intersections between the virtual circles and a ply that intersects the virtual circles and is closest to the tire-axial-direction outsides of the stiffeners, and reference points C are the middle points between points A and points B, line segments OC that connect the centers O of the bead cores and reference points C have an inclination angle θ of no more than 17° toward the tire-axial-direction outside relative to tire-radial-direction lines that pass through the centers O of the bead cores.

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Inventors:
OGAWA GAKU (JP)
MATSUMOTO TAKUYA (JP)
Application Number:
PCT/JP2018/046892
Publication Date:
June 27, 2019
Filing Date:
December 19, 2018
Export Citation:
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Assignee:
BRIDGESTONE CORP (JP)
International Classes:
B60C15/06; B60C9/08; B60C15/00; B60C15/04
Foreign References:
JP2009298342A2009-12-24
JP2003291607A2003-10-15
JP2015536868A2015-12-24
JP2011509879A2011-03-31
JP2003080908A2003-03-19
US20090151843A12009-06-18
US20110186201A12011-08-04
JPH06171326A1994-06-21
Other References:
"Engineering Design Information for Aircraft Tires (EDI", 2017, TIRE AND RIM ASSOCIATION, INC., article "description of numeric values in the present description"
See also references of EP 3730318A4
Attorney, Agent or Firm:
SUGIMURA Kenji (JP)
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