WEIGHT-REDUCED AIRCRAFT TIRE

PROBLEM TO BE SOLVED: To provide an improved aircraft tire having durability to high speed and heavy load, and satisfying weight saving requirement.SOLUTION: The carcass of a pneumatic aircraft tire has: at least two inner plies 1, 2, 3, 4 which are wound around an annular bead member 14 from inside...

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Bibliographic Details
Main Author UEYOKO KIYOSHI
Format Patent
LanguageEnglish
Japanese
Published 30.06.2016
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Summary:PROBLEM TO BE SOLVED: To provide an improved aircraft tire having durability to high speed and heavy load, and satisfying weight saving requirement.SOLUTION: The carcass of a pneumatic aircraft tire has: at least two inner plies 1, 2, 3, 4 which are wound around an annular bead member 14 from inside toward outside in an axial direction and extend to outside in a radial direction toward a crown to form folding parts 10, 20, 30, 40; at least one outside carcass ply 5, 6 extending inside from the crown in the radial direction and outside the annular bead member 14 in the axial direction and partially wound around a bead to end at terminal parts 50, 60; and a barrier ply 100 positioning between an inner liner 13 and an innermost ply 1 in the axial direction. The barrier ply 100 has a first end part ending in the shoulder area of the tire and a second end part 120 having a terminal part positioning below the outside carcass ply.SELECTED DRAWING: Figure 2 【課題】高速と高負荷と軽量化とを満たす、改良された航空機タイヤを提供する。【解決手段】空気入りタイヤのカーカスが、環状ビード部材14の周りに軸方向の内側から外側に向かって巻かれ、クラウンに向かって半径方向外側に延びて、各折り返し部10,20,30,40を形成する少なくとも2つの内側プライ1,2,3,4と、クラウンから半径方向内側に、環状ビード部材14の軸方向外側に延び、ビードの周りに部分的に巻かれて、末端部50,60で終端する少なくとも1つの外側カーカスプライ5,6と、インナーライナー13と軸方向の最も内側の内側プライ1との間に位置するバリアプライ100と、を有する。バリアプライ100は、タイヤのショルダー領域内で終端する第1の端部と、外側カーカスプライの下方に位置する終端部を有する第2の端部120を有している。【選択図】図2
Bibliography:Application Number: JP20150250088