发明名称 Aircraft tire with improved bead structure
摘要 A pneumatic radial ply tire 100 for use on aircraft has a radial reinforced carcass 20 having at least one axially inner ply 2 A, 2 B, 2 C and 2 D of textile cords 21 wound around a pair of bead cores 33 . The improved bead structure 30 has a flipper 50 having an axially inner leg L<SUB>I </SUB>and axially outer leg L<SUB>E</SUB>. The ends L<SUB>I</SUB>, L<SUB>E </SUB>of the flippers 50 are above the bead core height B<SUB>h </SUB>and below the apex A of an elastomeric strip 40 satisfying the relation B<SUB>h</SUB><L<SUB>E</SUB><0.7D AND B<SUB>h</SUB><L<SUB>I</SUB><0.7D. Additionally, the tire carcass 20 has at least one axially outer ply 2 E, 2 F of textile cords 21 extending from bead 30 to bead 30 along the turn-ups 20 A, 20 B, 20 C and 20 D of the axially inner plies 2 A, 2 B, 2 C and 2 D. The plies 21 are closely spaced along the natural ply path.
申请公布号 US7100655(B2) 申请公布日期 2006.09.05
申请号 US20030637477 申请日期 2003.08.08
申请人 THE GOODYEAR TIRE & RUBBER COMPANY 发明人 UEYOKO KIYOSHI
分类号 B60C15/00;B60C9/20;B60C13/00;B60C15/06;B60C19/00 主分类号 B60C15/00
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