发明名称 航空機用タイヤのクラウン補強材
摘要 An improvement of an airplane tire to obtain a more even distribution of temperature within the crown of the tire. An airplane tire comprises a crown reinforced by a working reinforcement (3), comprising at least one layer of working reinforcement (30) comprising axially juxtaposed substantially circumferential strips (31) comprising mutually parallel textile reinforcing elements (32) coated with a polymer coating material (33). Each strip of at least one layer of working reinforcement is in contact, over at least its radially inner axial face, with a heat transfer element (34) comprising mutually parallel substantially circumferential threadlike elements (35) made of a heat-conducting material with thermal conductivity at least equal to 50 times the thermal conductivity of the polymer coating material. Heat transfer element (34) comprises substantially circumferential threadlike elements (35) that have periodic geometric oscillations parallel to the strip in contact.
申请公布号 JP6038782(B2) 申请公布日期 2016.12.07
申请号 JP20130517350 申请日期 2011.07.05
申请人 カンパニー ジェネラレ デ エスタブリシュメンツ ミシュラン;ミシュラン ルシェルシュ エ テクニーク ソシエテ アノニム 发明人 エステンヌ ヴァンサン;ブシェ ローレン
分类号 B60C9/18;B60C9/00;B60C9/22 主分类号 B60C9/18
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